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1 | /*####################################################################################### |
1 | /*####################################################################################### |
2 | Flight Control |
2 | Flight Control |
3 | #######################################################################################*/ |
3 | #######################################################################################*/ |
4 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
4 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
5 | // + Copyright (c) Holger Buss, Ingo Busker |
5 | // + Copyright (c) Holger Buss, Ingo Busker |
6 | // + Nur für den privaten Gebrauch / NON-COMMERCIAL USE ONLY |
6 | // + Nur für den privaten Gebrauch / NON-COMMERCIAL USE ONLY |
7 | // + www.MikroKopter.com |
7 | // + www.MikroKopter.com |
8 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
8 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
9 | // + Es gilt für das gesamte Projekt (Hardware, Software, Binärfiles, Sourcecode und Dokumentation), |
9 | // + Es gilt für das gesamte Projekt (Hardware, Software, Binärfiles, Sourcecode und Dokumentation), |
10 | // + dass eine Nutzung (auch auszugsweise) nur für den privaten (nicht-kommerziellen) Gebrauch zulässig ist. |
10 | // + dass eine Nutzung (auch auszugsweise) nur für den privaten (nicht-kommerziellen) Gebrauch zulässig ist. |
11 | // + Sollten direkte oder indirekte kommerzielle Absichten verfolgt werden, ist mit uns (info@mikrokopter.de) Kontakt |
11 | // + Sollten direkte oder indirekte kommerzielle Absichten verfolgt werden, ist mit uns (info@mikrokopter.de) Kontakt |
12 | // + bzgl. der Nutzungsbedingungen aufzunehmen. |
12 | // + bzgl. der Nutzungsbedingungen aufzunehmen. |
13 | // + Eine kommerzielle Nutzung ist z.B.Verkauf von MikroKoptern, Bestückung und Verkauf von Platinen oder Bausätzen, |
13 | // + Eine kommerzielle Nutzung ist z.B.Verkauf von MikroKoptern, Bestückung und Verkauf von Platinen oder Bausätzen, |
14 | // + Verkauf von Luftbildaufnahmen, usw. |
14 | // + Verkauf von Luftbildaufnahmen, usw. |
15 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
15 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
16 | // + Werden Teile des Quellcodes (mit oder ohne Modifikation) weiterverwendet oder veröffentlicht, |
16 | // + Werden Teile des Quellcodes (mit oder ohne Modifikation) weiterverwendet oder veröffentlicht, |
17 | // + unterliegen sie auch diesen Nutzungsbedingungen und diese Nutzungsbedingungen incl. Copyright müssen dann beiliegen |
17 | // + unterliegen sie auch diesen Nutzungsbedingungen und diese Nutzungsbedingungen incl. Copyright müssen dann beiliegen |
18 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
18 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
19 | // + Sollte die Software (auch auszugesweise) oder sonstige Informationen des MikroKopter-Projekts |
19 | // + Sollte die Software (auch auszugesweise) oder sonstige Informationen des MikroKopter-Projekts |
20 | // + auf anderen Webseiten oder sonstigen Medien veröffentlicht werden, muss unsere Webseite "http://www.mikrokopter.de" |
20 | // + auf anderen Webseiten oder sonstigen Medien veröffentlicht werden, muss unsere Webseite "http://www.mikrokopter.de" |
21 | // + eindeutig als Ursprung verlinkt werden |
21 | // + eindeutig als Ursprung verlinkt werden |
22 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
22 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
23 | // + Keine Gewähr auf Fehlerfreiheit, Vollständigkeit oder Funktion |
23 | // + Keine Gewähr auf Fehlerfreiheit, Vollständigkeit oder Funktion |
24 | // + Benutzung auf eigene Gefahr |
24 | // + Benutzung auf eigene Gefahr |
25 | // + Wir übernehmen keinerlei Haftung für direkte oder indirekte Personen- oder Sachschäden |
25 | // + Wir übernehmen keinerlei Haftung für direkte oder indirekte Personen- oder Sachschäden |
26 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
26 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
27 | // + Die Portierung oder Nutzung der Software (oder Teile davon) auf andere Systeme (ausser der Hardware von www.mikrokopter.de) ist nur |
27 | // + Die Portierung oder Nutzung der Software (oder Teile davon) auf andere Systeme (ausser der Hardware von www.mikrokopter.de) ist nur |
28 | // + mit unserer Zustimmung zulässig |
28 | // + mit unserer Zustimmung zulässig |
29 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
29 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
30 | // + Die Funktion printf_P() unterliegt ihrer eigenen Lizenz und ist hiervon nicht betroffen |
30 | // + Die Funktion printf_P() unterliegt ihrer eigenen Lizenz und ist hiervon nicht betroffen |
31 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
31 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
32 | // + Redistributions of source code (with or without modifications) must retain the above copyright notice, |
32 | // + Redistributions of source code (with or without modifications) must retain the above copyright notice, |
33 | // + this list of conditions and the following disclaimer. |
33 | // + this list of conditions and the following disclaimer. |
34 | // + * Neither the name of the copyright holders nor the names of contributors may be used to endorse or promote products derived |
34 | // + * Neither the name of the copyright holders nor the names of contributors may be used to endorse or promote products derived |
35 | // + from this software without specific prior written permission. |
35 | // + from this software without specific prior written permission. |
36 | // + * The use of this project (hardware, software, binary files, sources and documentation) is only permittet |
36 | // + * The use of this project (hardware, software, binary files, sources and documentation) is only permittet |
37 | // + for non-commercial use (directly or indirectly) |
37 | // + for non-commercial use (directly or indirectly) |
38 | // + Commercial use (for excample: selling of MikroKopters, selling of PCBs, assembly, ...) is only permitted |
38 | // + Commercial use (for excample: selling of MikroKopters, selling of PCBs, assembly, ...) is only permitted |
39 | // + with our written permission |
39 | // + with our written permission |
40 | // + * If sources or documentations are redistributet on other webpages, out webpage (http://www.MikroKopter.de) must be |
40 | // + * If sources or documentations are redistributet on other webpages, out webpage (http://www.MikroKopter.de) must be |
41 | // + clearly linked as origin |
41 | // + clearly linked as origin |
42 | // + * porting the sources to other systems or using the software on other systems (except hardware from www.mikrokopter.de) is not allowed |
42 | // + * porting the sources to other systems or using the software on other systems (except hardware from www.mikrokopter.de) is not allowed |
43 | // + THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" |
43 | // + THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" |
44 | // + AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE |
44 | // + AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE |
45 | // + IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE |
45 | // + IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE |
46 | // + ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER OR CONTRIBUTORS BE |
46 | // + ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER OR CONTRIBUTORS BE |
47 | // + LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR |
47 | // + LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR |
48 | // + CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF |
48 | // + CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF |
49 | // + SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS |
49 | // + SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS |
50 | // + INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN |
50 | // + INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN |
51 | // + CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) |
51 | // + CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) |
52 | // + ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
52 | // + ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
53 | // + POSSIBILITY OF SUCH DAMAGE. |
53 | // + POSSIBILITY OF SUCH DAMAGE. |
54 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
54 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
55 | 55 | ||
56 | #include "main.h" |
56 | #include "main.h" |
57 | #include "mymath.h" |
57 | #include "mymath.h" |
58 | #include "isqrt.h" |
58 | #include "isqrt.h" |
- | 59 | ||
- | 60 | //MartinW; added vars |
|
- | 61 | unsigned char loop1, loop2, loop3; |
|
- | 62 | unsigned char settingdest = 5; |
|
- | 63 | int keynumber=-7; |
|
- | 64 | ||
- | 65 | unsigned short CurrentOffset = 0;/// |
|
- | 66 | ||
- | 67 | unsigned char pos1, pos2, pos3, pos4=0; |
|
- | 68 | unsigned char Motors0,Motors1,Motors2,Motors3,Motors4,Motors5,Motors6,Motors7; |
|
- | 69 | unsigned char Motors0max,Motors1max,Motors2max,Motors3max,Motors4max,Motors5max,Motors6max,Motors7max; |
|
- | 70 | unsigned short MotorsTmax; |
|
- | 71 | unsigned char updatemotors=5; |
|
- | 72 | //MartinW; added vars |
|
- | 73 | ||
59 | 74 | ||
60 | unsigned char h,m,s; |
75 | unsigned char h,m,s; |
61 | unsigned int BaroExpandActive = 0; |
76 | unsigned int BaroExpandActive = 0; |
62 | int MesswertNick,MesswertRoll,MesswertGier,MesswertGierBias, RohMesswertNick,RohMesswertRoll; |
77 | int MesswertNick,MesswertRoll,MesswertGier,MesswertGierBias, RohMesswertNick,RohMesswertRoll; |
63 | int TrimNick, TrimRoll; |
78 | int TrimNick, TrimRoll; |
64 | int AdNeutralNick = 0,AdNeutralRoll = 0,AdNeutralGier = 0,StartNeutralRoll = 0,StartNeutralNick = 0; |
79 | int AdNeutralNick = 0,AdNeutralRoll = 0,AdNeutralGier = 0,StartNeutralRoll = 0,StartNeutralNick = 0; |
65 | int Mittelwert_AccNick, Mittelwert_AccRoll; |
80 | int Mittelwert_AccNick, Mittelwert_AccRoll; |
66 | unsigned int NeutralAccX=0, NeutralAccY=0; |
81 | unsigned int NeutralAccX=0, NeutralAccY=0; |
67 | int NaviAccNick, NaviAccRoll,NaviCntAcc = 0; |
82 | int NaviAccNick, NaviAccRoll,NaviCntAcc = 0; |
68 | int NeutralAccZ = 0; |
83 | int NeutralAccZ = 0; |
69 | unsigned char ControlHeading = 0;// in 2° |
84 | unsigned char ControlHeading = 0;// in 2° |
70 | long IntegralNick = 0,IntegralNick2 = 0; |
85 | long IntegralNick = 0,IntegralNick2 = 0; |
71 | long IntegralRoll = 0,IntegralRoll2 = 0; |
86 | long IntegralRoll = 0,IntegralRoll2 = 0; |
72 | long IntegralAccNick = 0,IntegralAccRoll = 0,IntegralAccZ = 0; |
87 | long IntegralAccNick = 0,IntegralAccRoll = 0,IntegralAccZ = 0; |
73 | long Integral_Gier = 0; |
88 | long Integral_Gier = 0; |
74 | long Mess_IntegralNick = 0,Mess_IntegralNick2 = 0; |
89 | long Mess_IntegralNick = 0,Mess_IntegralNick2 = 0; |
75 | long Mess_IntegralRoll = 0,Mess_IntegralRoll2 = 0; |
90 | long Mess_IntegralRoll = 0,Mess_IntegralRoll2 = 0; |
76 | long Mess_Integral_Gier = 0,Mess_Integral_Gier2 = 0; |
91 | long Mess_Integral_Gier = 0,Mess_Integral_Gier2 = 0; |
77 | long MittelIntegralNick,MittelIntegralRoll,MittelIntegralNick2,MittelIntegralRoll2; |
92 | long MittelIntegralNick,MittelIntegralRoll,MittelIntegralNick2,MittelIntegralRoll2; |
78 | long SummeNick=0,SummeRoll=0; |
93 | long SummeNick=0,SummeRoll=0; |
79 | volatile long Mess_Integral_Hoch = 0; |
94 | volatile long Mess_Integral_Hoch = 0; |
80 | int KompassValue = 0; |
95 | int KompassValue = 0; |
81 | int KompassStartwert = 0; |
96 | int KompassStartwert = 0; |
82 | int KompassRichtung = 0; |
97 | int KompassRichtung = 0; |
83 | unsigned int KompassSignalSchlecht = 500; |
98 | unsigned int KompassSignalSchlecht = 500; |
84 | unsigned char MAX_GAS,MIN_GAS; |
99 | unsigned char MAX_GAS,MIN_GAS; |
85 | unsigned char HoehenReglerAktiv = 0; |
100 | unsigned char HoehenReglerAktiv = 0; |
86 | unsigned char TrichterFlug = 0; |
101 | unsigned char TrichterFlug = 0; |
87 | long Umschlag180Nick = 250000L, Umschlag180Roll = 250000L; |
102 | long Umschlag180Nick = 250000L, Umschlag180Roll = 250000L; |
88 | long ErsatzKompass; |
103 | long ErsatzKompass; |
89 | int ErsatzKompassInGrad; // Kompasswert in Grad |
104 | int ErsatzKompassInGrad; // Kompasswert in Grad |
90 | int GierGyroFehler = 0; |
105 | int GierGyroFehler = 0; |
91 | char GyroFaktor,GyroFaktorGier; |
106 | char GyroFaktor,GyroFaktorGier; |
92 | char IntegralFaktor,IntegralFaktorGier; |
107 | char IntegralFaktor,IntegralFaktorGier; |
93 | int DiffNick,DiffRoll; |
108 | int DiffNick,DiffRoll; |
94 | //int Poti1 = 0, Poti2 = 0, Poti3 = 0, Poti4 = 0, Poti5 = 0, Poti6 = 0, Poti7 = 0, Poti8 = 0; |
109 | //int Poti1 = 0, Poti2 = 0, Poti3 = 0, Poti4 = 0, Poti5 = 0, Poti6 = 0, Poti7 = 0, Poti8 = 0; |
95 | unsigned char Poti[9] = {0,0,0,0,0,0,0,0}; |
110 | unsigned char Poti[9] = {0,0,0,0,0,0,0,0}; |
96 | volatile unsigned char SenderOkay = 0; |
111 | volatile unsigned char SenderOkay = 0; |
97 | int StickNick = 0,StickRoll = 0,StickGier = 0,StickGas = 0; |
112 | int StickNick = 0,StickRoll = 0,StickGier = 0,StickGas = 0; |
98 | char MotorenEin = 0,StartTrigger = 0; |
113 | char MotorenEin = 0,StartTrigger = 0; |
99 | long HoehenWert = 0; |
114 | long HoehenWert = 0; |
100 | long SollHoehe = 0; |
115 | long SollHoehe = 0; |
101 | int LageKorrekturRoll = 0,LageKorrekturNick = 0, HoverGas = 0; |
116 | int LageKorrekturRoll = 0,LageKorrekturNick = 0, HoverGas = 0; |
102 | //float Ki = FAKTOR_I; |
117 | //float Ki = FAKTOR_I; |
103 | int Ki = 10300 / 33; |
118 | int Ki = 10300 / 33; |
104 | unsigned char Looping_Nick = 0,Looping_Roll = 0; |
119 | unsigned char Looping_Nick = 0,Looping_Roll = 0; |
105 | unsigned char Looping_Links = 0, Looping_Rechts = 0, Looping_Unten = 0, Looping_Oben = 0; |
120 | unsigned char Looping_Links = 0, Looping_Rechts = 0, Looping_Unten = 0, Looping_Oben = 0; |
106 | 121 | ||
107 | unsigned char Parameter_Luftdruck_D = 48; // Wert : 0-250 |
122 | unsigned char Parameter_Luftdruck_D = 48; // Wert : 0-250 |
108 | unsigned char Parameter_MaxHoehe = 251; // Wert : 0-250 |
123 | unsigned char Parameter_MaxHoehe = 251; // Wert : 0-250 |
109 | unsigned char Parameter_Hoehe_P = 16; // Wert : 0-32 |
124 | unsigned char Parameter_Hoehe_P = 16; // Wert : 0-32 |
110 | unsigned char Parameter_Hoehe_ACC_Wirkung = 58; // Wert : 0-250 |
125 | unsigned char Parameter_Hoehe_ACC_Wirkung = 58; // Wert : 0-250 |
111 | unsigned char Parameter_KompassWirkung = 64; // Wert : 0-250 |
126 | unsigned char Parameter_KompassWirkung = 64; // Wert : 0-250 |
112 | unsigned char Parameter_Hoehe_GPS_Z = 64; // Wert : 0-250 |
127 | unsigned char Parameter_Hoehe_GPS_Z = 64; // Wert : 0-250 |
113 | unsigned char Parameter_Gyro_D = 8; // Wert : 0-250 |
128 | unsigned char Parameter_Gyro_D = 8; // Wert : 0-250 |
114 | unsigned char Parameter_Gyro_P = 150; // Wert : 10-250 |
129 | unsigned char Parameter_Gyro_P = 150; // Wert : 10-250 |
115 | unsigned char Parameter_Gyro_I = 150; // Wert : 0-250 |
130 | unsigned char Parameter_Gyro_I = 150; // Wert : 0-250 |
116 | unsigned char Parameter_Gyro_Gier_P = 150; // Wert : 10-250 |
131 | unsigned char Parameter_Gyro_Gier_P = 150; // Wert : 10-250 |
117 | unsigned char Parameter_Gyro_Gier_I = 150; // Wert : 10-250 |
132 | unsigned char Parameter_Gyro_Gier_I = 150; // Wert : 10-250 |
118 | unsigned char Parameter_Gier_P = 2; // Wert : 1-20 |
133 | unsigned char Parameter_Gier_P = 2; // Wert : 1-20 |
119 | unsigned char Parameter_I_Faktor = 10; // Wert : 1-20 |
134 | unsigned char Parameter_I_Faktor = 10; // Wert : 1-20 |
120 | unsigned char Parameter_UserParam1 = 0; |
135 | unsigned char Parameter_UserParam1 = 0; |
121 | unsigned char Parameter_UserParam2 = 0; |
136 | unsigned char Parameter_UserParam2 = 0; |
122 | unsigned char Parameter_UserParam3 = 0; |
137 | unsigned char Parameter_UserParam3 = 0; |
123 | unsigned char Parameter_UserParam4 = 0; |
138 | unsigned char Parameter_UserParam4 = 0; |
124 | unsigned char Parameter_UserParam5 = 0; |
139 | unsigned char Parameter_UserParam5 = 0; |
125 | unsigned char Parameter_UserParam6 = 0; |
140 | unsigned char Parameter_UserParam6 = 0; |
126 | unsigned char Parameter_UserParam7 = 0; |
141 | unsigned char Parameter_UserParam7 = 0; |
127 | unsigned char Parameter_UserParam8 = 0; |
142 | unsigned char Parameter_UserParam8 = 0; |
128 | unsigned char Parameter_ServoNickControl = 100; |
143 | unsigned char Parameter_ServoNickControl = 100; |
129 | unsigned char Parameter_ServoRollControl = 100; |
144 | unsigned char Parameter_ServoRollControl = 100; |
130 | unsigned char Parameter_LoopGasLimit = 70; |
145 | unsigned char Parameter_LoopGasLimit = 70; |
131 | unsigned char Parameter_AchsKopplung1 = 90; |
146 | unsigned char Parameter_AchsKopplung1 = 90; |
132 | unsigned char Parameter_AchsKopplung2 = 65; |
147 | unsigned char Parameter_AchsKopplung2 = 65; |
133 | unsigned char Parameter_CouplingYawCorrection = 64; |
148 | unsigned char Parameter_CouplingYawCorrection = 64; |
134 | //unsigned char Parameter_AchsGegenKopplung1 = 0; |
149 | //unsigned char Parameter_AchsGegenKopplung1 = 0; |
135 | unsigned char Parameter_DynamicStability = 100; |
150 | unsigned char Parameter_DynamicStability = 100; |
136 | unsigned char Parameter_J16Bitmask; // for the J16 Output |
151 | unsigned char Parameter_J16Bitmask; // for the J16 Output |
137 | unsigned char Parameter_J16Timing; // for the J16 Output |
152 | unsigned char Parameter_J16Timing; // for the J16 Output |
138 | unsigned char Parameter_J17Bitmask; // for the J17 Output |
153 | unsigned char Parameter_J17Bitmask; // for the J17 Output |
139 | unsigned char Parameter_J17Timing; // for the J17 Output |
154 | unsigned char Parameter_J17Timing; // for the J17 Output |
140 | unsigned char Parameter_NaviGpsModeControl; // Parameters for the Naviboard |
155 | unsigned char Parameter_NaviGpsModeControl; // Parameters for the Naviboard |
141 | unsigned char Parameter_NaviGpsGain; |
156 | unsigned char Parameter_NaviGpsGain; |
142 | unsigned char Parameter_NaviGpsP; |
157 | unsigned char Parameter_NaviGpsP; |
143 | unsigned char Parameter_NaviGpsI; |
158 | unsigned char Parameter_NaviGpsI; |
144 | unsigned char Parameter_NaviGpsD; |
159 | unsigned char Parameter_NaviGpsD; |
145 | unsigned char Parameter_NaviGpsACC; |
160 | unsigned char Parameter_NaviGpsACC; |
146 | unsigned char Parameter_NaviOperatingRadius; |
161 | unsigned char Parameter_NaviOperatingRadius; |
147 | unsigned char Parameter_NaviWindCorrection; |
162 | unsigned char Parameter_NaviWindCorrection; |
148 | unsigned char Parameter_NaviSpeedCompensation; |
163 | unsigned char Parameter_NaviSpeedCompensation; |
149 | unsigned char Parameter_ExternalControl; |
164 | unsigned char Parameter_ExternalControl; |
150 | unsigned char Parameter_Servo3,Parameter_Servo4,Parameter_Servo5; |
165 | unsigned char Parameter_Servo3,Parameter_Servo4,Parameter_Servo5; |
151 | unsigned char CareFree = 0; |
166 | unsigned char CareFree = 0; |
152 | const signed char sintab[31] = { 0, 2, 4, 6, 7, 8, 8, 8, 7, 6, 4, 2, 0, -2, -4, -6, -7, -8, -8, -8, -7, -6, -4, -2, 0, 2, 4, 6, 7, 8, 8}; |
167 | const signed char sintab[31] = { 0, 2, 4, 6, 7, 8, 8, 8, 7, 6, 4, 2, 0, -2, -4, -6, -7, -8, -8, -8, -7, -6, -4, -2, 0, 2, 4, 6, 7, 8, 8}; |
153 | 168 | ||
154 | signed int ExternStickNick = 0,ExternStickRoll = 0,ExternStickGier = 0, ExternHoehenValue = -20; |
169 | signed int ExternStickNick = 0,ExternStickRoll = 0,ExternStickGier = 0, ExternHoehenValue = -20; |
155 | int MaxStickNick = 0,MaxStickRoll = 0; |
170 | int MaxStickNick = 0,MaxStickRoll = 0; |
156 | unsigned int modell_fliegt = 0; |
171 | unsigned int modell_fliegt = 0; |
157 | volatile unsigned char FC_StatusFlags = 0; |
172 | volatile unsigned char FC_StatusFlags = 0; |
158 | long GIER_GRAD_FAKTOR = 1291; |
173 | long GIER_GRAD_FAKTOR = 1291; |
159 | signed int KopplungsteilNickRoll,KopplungsteilRollNick; |
174 | signed int KopplungsteilNickRoll,KopplungsteilRollNick; |
160 | signed int tmp_motorwert[MAX_MOTORS]; |
175 | signed int tmp_motorwert[MAX_MOTORS]; |
161 | char VarioCharacter = ' '; |
176 | char VarioCharacter = ' '; |
162 | 177 | ||
163 | #define LIMIT_MIN(value, min) {if(value <= min) value = min;} |
178 | #define LIMIT_MIN(value, min) {if(value <= min) value = min;} |
164 | #define LIMIT_MAX(value, max) {if(value >= max) value = max;} |
179 | #define LIMIT_MAX(value, max) {if(value >= max) value = max;} |
165 | #define LIMIT_MIN_MAX(value, min, max) {if(value <= min) value = min; else if(value >= max) value = max;} |
180 | #define LIMIT_MIN_MAX(value, min, max) {if(value <= min) value = min; else if(value >= max) value = max;} |
166 | 181 | ||
167 | 182 | ||
168 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
183 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
169 | // Debugwerte zuordnen |
184 | // Debugwerte zuordnen |
170 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
185 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
171 | void CopyDebugValues(void) |
186 | void CopyDebugValues(void) |
172 | { |
187 | { |
173 | DebugOut.Analog[0] = IntegralNick / (EE_Parameter.GyroAccFaktor * 4); |
188 | DebugOut.Analog[0] = IntegralNick / (EE_Parameter.GyroAccFaktor * 4); |
174 | DebugOut.Analog[1] = IntegralRoll / (EE_Parameter.GyroAccFaktor * 4); |
189 | DebugOut.Analog[1] = IntegralRoll / (EE_Parameter.GyroAccFaktor * 4); |
175 | DebugOut.Analog[2] = Mittelwert_AccNick / 4; |
190 | DebugOut.Analog[2] = Mittelwert_AccNick / 4; |
176 | DebugOut.Analog[3] = Mittelwert_AccRoll / 4; |
191 | DebugOut.Analog[3] = Mittelwert_AccRoll / 4; |
177 | DebugOut.Analog[4] = (signed int) AdNeutralGier - AdWertGier; |
192 | DebugOut.Analog[4] = (signed int) AdNeutralGier - AdWertGier; |
178 | DebugOut.Analog[5] = HoehenWert/5; |
193 | DebugOut.Analog[5] = HoehenWert/5; |
179 | DebugOut.Analog[6] = AdWertAccHoch;//(Mess_Integral_Hoch / 512);// Aktuell_az; |
194 | DebugOut.Analog[6] = AdWertAccHoch;//(Mess_Integral_Hoch / 512);// Aktuell_az; |
180 | DebugOut.Analog[8] = KompassValue; |
195 | DebugOut.Analog[8] = KompassValue; |
181 | DebugOut.Analog[9] = UBat; |
196 | DebugOut.Analog[9] = UBat; |
182 | DebugOut.Analog[10] = SenderOkay; |
197 | DebugOut.Analog[10] = SenderOkay; |
183 | DebugOut.Analog[11] = ErsatzKompass / GIER_GRAD_FAKTOR; |
198 | DebugOut.Analog[11] = ErsatzKompass / GIER_GRAD_FAKTOR; |
184 | DebugOut.Analog[12] = Motor[0].SetPoint; |
199 | DebugOut.Analog[12] = Motor[0].SetPoint; |
185 | DebugOut.Analog[13] = Motor[1].SetPoint; |
200 | DebugOut.Analog[13] = Motor[1].SetPoint; |
186 | DebugOut.Analog[14] = Motor[2].SetPoint; |
201 | DebugOut.Analog[14] = Motor[2].SetPoint; |
187 | DebugOut.Analog[15] = Motor[3].SetPoint; |
202 | DebugOut.Analog[15] = Motor[3].SetPoint; |
- | 203 | ||
- | 204 | //MartinW added Debug ouputs |
|
- | 205 | DebugOut.Analog[16] = Motor[4].SetPoint; |
|
- | 206 | DebugOut.Analog[17] = Motor[5].SetPoint; |
|
- | 207 | DebugOut.Analog[24] = Motor[6].SetPoint; |
|
- | 208 | DebugOut.Analog[25] = Motor[7].SetPoint; |
|
- | 209 | DebugOut.Analog[26] = Motor[8].SetPoint; |
|
- | 210 | DebugOut.Analog[27] = Motor[9].SetPoint; |
|
- | 211 | //MartinW added Debug ouputs |
|
- | 212 | ||
188 | DebugOut.Analog[20] = ServoNickValue; |
213 | DebugOut.Analog[20] = ServoNickValue; |
189 | DebugOut.Analog[22] = Capacity.ActualCurrent; |
214 | DebugOut.Analog[22] = Capacity.ActualCurrent; |
190 | DebugOut.Analog[23] = Capacity.UsedCapacity; |
215 | DebugOut.Analog[23] = Capacity.UsedCapacity; |
191 | // DebugOut.Analog[22] = FromNaviCtrl_Value.GpsZ; |
216 | // DebugOut.Analog[22] = FromNaviCtrl_Value.GpsZ; |
192 | // DebugOut.Analog[29] = FromNaviCtrl_Value.SerialDataOkay; |
217 | // DebugOut.Analog[29] = FromNaviCtrl_Value.SerialDataOkay; |
193 | DebugOut.Analog[29] = Capacity.MinOfMaxPWM; |
218 | DebugOut.Analog[29] = Capacity.MinOfMaxPWM; |
194 | DebugOut.Analog[30] = GPS_Nick; |
219 | DebugOut.Analog[30] = GPS_Nick; |
195 | DebugOut.Analog[31] = GPS_Roll; |
220 | DebugOut.Analog[31] = GPS_Roll; |
196 | if(VersionInfo.HardwareError[0] || VersionInfo.HardwareError[1]) DebugOut.Status[1] |= 1; else DebugOut.Status[1] &= 0xfe; |
221 | if(VersionInfo.HardwareError[0] || VersionInfo.HardwareError[1]) DebugOut.Status[1] |= 1; else DebugOut.Status[1] &= 0xfe; |
197 | 222 | ||
198 | //if(Capacity.MinOfMaxPWM < 250/* && modell_fliegt > 500*/) { beeptime = 1000; DebugOut.Analog[25]++; } |
223 | //if(Capacity.MinOfMaxPWM < 250/* && modell_fliegt > 500*/) { beeptime = 1000; DebugOut.Analog[25]++; } |
199 | } |
224 | } |
200 | 225 | ||
201 | 226 | ||
202 | 227 | ||
203 | void Piep(unsigned char Anzahl, unsigned int dauer) |
228 | void Piep(unsigned char Anzahl, unsigned int dauer) |
204 | { |
229 | { |
205 | if(MotorenEin) return; //auf keinen Fall im Flug! |
230 | if(MotorenEin) return; //auf keinen Fall im Flug! |
206 | while(Anzahl--) |
231 | while(Anzahl--) |
207 | { |
232 | { |
208 | beeptime = dauer; |
233 | beeptime = dauer; |
209 | while(beeptime); |
234 | while(beeptime); |
210 | Delay_ms(dauer * 2); |
235 | Delay_ms(dauer * 2); |
211 | } |
236 | } |
212 | } |
237 | } |
213 | 238 | ||
214 | //############################################################################ |
239 | //############################################################################ |
215 | // Messwerte beim Ermitteln der Nullage |
240 | // Messwerte beim Ermitteln der Nullage |
216 | void CalibrierMittelwert(void) |
241 | void CalibrierMittelwert(void) |
217 | //############################################################################ |
242 | //############################################################################ |
218 | { |
243 | { |
219 | unsigned char i; |
244 | unsigned char i; |
220 | if(PlatinenVersion == 13) SucheGyroOffset(); |
245 | if(PlatinenVersion == 13) SucheGyroOffset(); |
221 | // ADC auschalten, damit die Werte sich nicht während der Berechnung ändern |
246 | // ADC auschalten, damit die Werte sich nicht während der Berechnung ändern |
222 | ANALOG_OFF; |
247 | ANALOG_OFF; |
223 | MesswertNick = AdWertNick; |
248 | MesswertNick = AdWertNick; |
224 | MesswertRoll = AdWertRoll; |
249 | MesswertRoll = AdWertRoll; |
225 | MesswertGier = AdWertGier; |
250 | MesswertGier = AdWertGier; |
226 | Mittelwert_AccNick = ACC_AMPLIFY * AdWertAccNick; |
251 | Mittelwert_AccNick = ACC_AMPLIFY * AdWertAccNick; |
227 | Mittelwert_AccRoll = ACC_AMPLIFY * AdWertAccRoll; |
252 | Mittelwert_AccRoll = ACC_AMPLIFY * AdWertAccRoll; |
228 | // ADC einschalten |
253 | // ADC einschalten |
229 | ANALOG_ON; |
254 | ANALOG_ON; |
230 | for(i=0;i<8;i++) |
255 | for(i=0;i<8;i++) |
231 | { |
256 | { |
232 | int tmp; |
257 | int tmp; |
233 | tmp = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
258 | tmp = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
234 | LIMIT_MIN_MAX(tmp, 0, 255); |
259 | LIMIT_MIN_MAX(tmp, 0, 255); |
235 | if(Poti[i] > tmp) Poti[i]--; else if(Poti[i] < tmp) Poti[i]++; |
260 | if(Poti[i] > tmp) Poti[i]--; else if(Poti[i] < tmp) Poti[i]++; |
236 | } |
261 | } |
237 | Umschlag180Nick = (long) EE_Parameter.WinkelUmschlagNick * 2500L; |
262 | Umschlag180Nick = (long) EE_Parameter.WinkelUmschlagNick * 2500L; |
238 | Umschlag180Roll = (long) EE_Parameter.WinkelUmschlagRoll * 2500L; |
263 | Umschlag180Roll = (long) EE_Parameter.WinkelUmschlagRoll * 2500L; |
239 | } |
264 | } |
240 | 265 | ||
241 | //############################################################################ |
266 | //############################################################################ |
242 | // Nullwerte ermitteln |
267 | // Nullwerte ermitteln |
243 | void SetNeutral(unsigned char AccAdjustment) |
268 | void SetNeutral(unsigned char AccAdjustment) |
244 | //############################################################################ |
269 | //############################################################################ |
245 | { |
270 | { |
246 | unsigned char i; |
271 | unsigned char i; |
247 | unsigned int gier_neutral=0, nick_neutral=0, roll_neutral=0; |
272 | unsigned int gier_neutral=0, nick_neutral=0, roll_neutral=0; |
248 | VersionInfo.HardwareError[0] = 0; |
273 | VersionInfo.HardwareError[0] = 0; |
249 | HEF4017R_ON; |
274 | HEF4017R_ON; |
250 | NeutralAccX = 0; |
275 | NeutralAccX = 0; |
251 | NeutralAccY = 0; |
276 | NeutralAccY = 0; |
252 | NeutralAccZ = 0; |
277 | NeutralAccZ = 0; |
253 | 278 | ||
254 | AdNeutralNick = 0; |
279 | AdNeutralNick = 0; |
255 | AdNeutralRoll = 0; |
280 | AdNeutralRoll = 0; |
256 | AdNeutralGier = 0; |
281 | AdNeutralGier = 0; |
257 | 282 | ||
258 | Parameter_AchsKopplung1 = 0; |
283 | Parameter_AchsKopplung1 = 0; |
259 | Parameter_AchsKopplung2 = 0; |
284 | Parameter_AchsKopplung2 = 0; |
260 | 285 | ||
261 | ExpandBaro = 0; |
286 | ExpandBaro = 0; |
262 | 287 | ||
263 | CalibrierMittelwert(); |
288 | CalibrierMittelwert(); |
264 | Delay_ms_Mess(100); |
289 | Delay_ms_Mess(100); |
265 | 290 | ||
266 | CalibrierMittelwert(); |
291 | CalibrierMittelwert(); |
267 | 292 | ||
268 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
293 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
269 | { |
294 | { |
270 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
295 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
271 | } |
296 | } |
272 | #define NEUTRAL_FILTER 32 |
297 | #define NEUTRAL_FILTER 32 |
273 | for(i=0; i<NEUTRAL_FILTER; i++) |
298 | for(i=0; i<NEUTRAL_FILTER; i++) |
274 | { |
299 | { |
275 | Delay_ms_Mess(10); |
300 | Delay_ms_Mess(10); |
276 | gier_neutral += AdWertGier; |
301 | gier_neutral += AdWertGier; |
277 | nick_neutral += AdWertNick; |
302 | nick_neutral += AdWertNick; |
278 | roll_neutral += AdWertRoll; |
303 | roll_neutral += AdWertRoll; |
279 | } |
304 | } |
280 | AdNeutralNick= (nick_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
305 | AdNeutralNick= (nick_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
281 | AdNeutralRoll= (roll_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
306 | AdNeutralRoll= (roll_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
282 | AdNeutralGier= (gier_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER); |
307 | AdNeutralGier= (gier_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER); |
283 | 308 | ||
284 | StartNeutralRoll = AdNeutralRoll; |
309 | StartNeutralRoll = AdNeutralRoll; |
285 | StartNeutralNick = AdNeutralNick; |
310 | StartNeutralNick = AdNeutralNick; |
286 | 311 | ||
287 | if(AccAdjustment) |
312 | if(AccAdjustment) |
288 | { |
313 | { |
289 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
314 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
290 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
315 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
291 | NeutralAccZ = Aktuell_az; |
316 | NeutralAccZ = Aktuell_az; |
292 | 317 | ||
293 | // Save ACC neutral settings to eeprom |
318 | // Save ACC neutral settings to eeprom |
294 | SetParamWord(PID_ACC_NICK, (uint16_t)NeutralAccX); |
319 | SetParamWord(PID_ACC_NICK, (uint16_t)NeutralAccX); |
295 | SetParamWord(PID_ACC_ROLL, (uint16_t)NeutralAccY); |
320 | SetParamWord(PID_ACC_ROLL, (uint16_t)NeutralAccY); |
296 | SetParamWord(PID_ACC_TOP, (uint16_t)NeutralAccZ); |
321 | SetParamWord(PID_ACC_TOP, (uint16_t)NeutralAccZ); |
297 | } |
322 | } |
298 | else |
323 | else |
299 | { |
324 | { |
300 | // restore from eeprom |
325 | // restore from eeprom |
301 | NeutralAccX = (int16_t)GetParamWord(PID_ACC_NICK); |
326 | NeutralAccX = (int16_t)GetParamWord(PID_ACC_NICK); |
302 | NeutralAccY = (int16_t)GetParamWord(PID_ACC_ROLL); |
327 | NeutralAccY = (int16_t)GetParamWord(PID_ACC_ROLL); |
303 | NeutralAccZ = (int16_t)GetParamWord(PID_ACC_TOP); |
328 | NeutralAccZ = (int16_t)GetParamWord(PID_ACC_TOP); |
304 | // strange settings? |
329 | // strange settings? |
305 | if(((unsigned int) NeutralAccX > 2048) || ((unsigned int) NeutralAccY > 2048) || ((unsigned int) NeutralAccZ > 1024)) |
330 | if(((unsigned int) NeutralAccX > 2048) || ((unsigned int) NeutralAccY > 2048) || ((unsigned int) NeutralAccZ > 1024)) |
306 | { |
331 | { |
307 | printf("\n\rACC not calibrated!\r\n"); |
332 | printf("\n\rACC not calibrated!\r\n"); |
308 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
333 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
309 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
334 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
310 | NeutralAccZ = Aktuell_az; |
335 | NeutralAccZ = Aktuell_az; |
311 | } |
336 | } |
312 | } |
337 | } |
313 | 338 | ||
314 | MesswertNick = 0; |
339 | MesswertNick = 0; |
315 | MesswertRoll = 0; |
340 | MesswertRoll = 0; |
316 | MesswertGier = 0; |
341 | MesswertGier = 0; |
317 | Delay_ms_Mess(100); |
342 | Delay_ms_Mess(100); |
318 | Mittelwert_AccNick = ACC_AMPLIFY * AdWertAccNick; |
343 | Mittelwert_AccNick = ACC_AMPLIFY * AdWertAccNick; |
319 | Mittelwert_AccRoll = ACC_AMPLIFY * AdWertAccRoll; |
344 | Mittelwert_AccRoll = ACC_AMPLIFY * AdWertAccRoll; |
320 | IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
345 | IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
321 | IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
346 | IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
322 | Mess_IntegralNick2 = IntegralNick; |
347 | Mess_IntegralNick2 = IntegralNick; |
323 | Mess_IntegralRoll2 = IntegralRoll; |
348 | Mess_IntegralRoll2 = IntegralRoll; |
324 | Mess_Integral_Gier = 0; |
349 | Mess_Integral_Gier = 0; |
325 | StartLuftdruck = Luftdruck; |
350 | StartLuftdruck = Luftdruck; |
326 | VarioMeter = 0; |
351 | VarioMeter = 0; |
327 | Mess_Integral_Hoch = 0; |
352 | Mess_Integral_Hoch = 0; |
328 | KompassStartwert = KompassValue; |
353 | KompassStartwert = KompassValue; |
329 | GPS_Neutral(); |
354 | GPS_Neutral(); |
330 | beeptime = 50; |
355 | beeptime = 50; |
331 | Umschlag180Nick = ((long) EE_Parameter.WinkelUmschlagNick * 2500L) + 15000L; |
356 | Umschlag180Nick = ((long) EE_Parameter.WinkelUmschlagNick * 2500L) + 15000L; |
332 | Umschlag180Roll = ((long) EE_Parameter.WinkelUmschlagRoll * 2500L) + 15000L; |
357 | Umschlag180Roll = ((long) EE_Parameter.WinkelUmschlagRoll * 2500L) + 15000L; |
333 | ExternHoehenValue = 0; |
358 | ExternHoehenValue = 0; |
334 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
359 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
335 | GierGyroFehler = 0; |
360 | GierGyroFehler = 0; |
336 | SendVersionToNavi = 1; |
361 | SendVersionToNavi = 1; |
337 | LED_Init(); |
362 | LED_Init(); |
338 | FC_StatusFlags |= FC_STATUS_CALIBRATE; |
363 | FC_StatusFlags |= FC_STATUS_CALIBRATE; |
339 | FromNaviCtrl_Value.Kalman_K = -1; |
364 | FromNaviCtrl_Value.Kalman_K = -1; |
340 | FromNaviCtrl_Value.Kalman_MaxDrift = 0; |
365 | FromNaviCtrl_Value.Kalman_MaxDrift = 0; |
341 | FromNaviCtrl_Value.Kalman_MaxFusion = 32; |
366 | FromNaviCtrl_Value.Kalman_MaxFusion = 32; |
342 | 367 | ||
343 | for(i=0;i<8;i++) |
368 | for(i=0;i<8;i++) |
344 | { |
369 | { |
345 | Poti[i] = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
370 | Poti[i] = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
346 | } |
371 | } |
347 | SenderOkay = 100; |
372 | SenderOkay = 100; |
348 | if(ServoActive) |
373 | if(ServoActive) |
349 | { |
374 | { |
350 | HEF4017R_ON; |
375 | HEF4017R_ON; |
351 | DDRD |=0x80; // enable J7 -> Servo signal |
376 | DDRD |=0x80; // enable J7 -> Servo signal |
352 | } |
377 | } |
353 | 378 | ||
354 | if((AdNeutralNick < 150 * 16) || (AdNeutralNick > 850 * 16)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_NICK; }; |
379 | if((AdNeutralNick < 150 * 16) || (AdNeutralNick > 850 * 16)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_NICK; }; |
355 | if((AdNeutralRoll < 150 * 16) || (AdNeutralRoll > 850 * 16)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_ROLL; }; |
380 | if((AdNeutralRoll < 150 * 16) || (AdNeutralRoll > 850 * 16)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_ROLL; }; |
356 | if((AdNeutralGier < 150 * 2) || (AdNeutralGier > 850 * 2)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_YAW; }; |
381 | if((AdNeutralGier < 150 * 2) || (AdNeutralGier > 850 * 2)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_YAW; }; |
357 | if((NeutralAccX < 300) || (NeutralAccX > 750)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_NICK; }; |
382 | if((NeutralAccX < 300) || (NeutralAccX > 750)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_NICK; }; |
358 | if((NeutralAccY < 300) || (NeutralAccY > 750)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_ROLL; }; |
383 | if((NeutralAccY < 300) || (NeutralAccY > 750)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_ROLL; }; |
359 | if((NeutralAccZ < 512) || (NeutralAccZ > 850)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_TOP; }; |
384 | if((NeutralAccZ < 512) || (NeutralAccZ > 850)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_TOP; }; |
360 | } |
385 | } |
361 | 386 | ||
362 | 387 | ||
363 | //############################################################################ |
388 | //############################################################################ |
364 | // Bearbeitet die Messwerte |
389 | // Bearbeitet die Messwerte |
365 | void Mittelwert(void) |
390 | void Mittelwert(void) |
366 | //############################################################################ |
391 | //############################################################################ |
367 | { |
392 | { |
368 | static signed long tmpl,tmpl2,tmpl3,tmpl4; |
393 | static signed long tmpl,tmpl2,tmpl3,tmpl4; |
369 | static signed int oldNick, oldRoll, d2Roll, d2Nick; |
394 | static signed int oldNick, oldRoll, d2Roll, d2Nick; |
370 | signed long winkel_nick, winkel_roll; |
395 | signed long winkel_nick, winkel_roll; |
371 | unsigned char i; |
396 | unsigned char i; |
372 | MesswertGier = (signed int) AdNeutralGier - AdWertGier; |
397 | MesswertGier = (signed int) AdNeutralGier - AdWertGier; |
373 | MesswertNick = (signed int) AdWertNickFilter / 8; |
398 | MesswertNick = (signed int) AdWertNickFilter / 8; |
374 | MesswertRoll = (signed int) AdWertRollFilter / 8; |
399 | MesswertRoll = (signed int) AdWertRollFilter / 8; |
375 | RohMesswertNick = MesswertNick; |
400 | RohMesswertNick = MesswertNick; |
376 | RohMesswertRoll = MesswertRoll; |
401 | RohMesswertRoll = MesswertRoll; |
377 | 402 | ||
378 | // Beschleunigungssensor ++++++++++++++++++++++++++++++++++++++++++++++++ |
403 | // Beschleunigungssensor ++++++++++++++++++++++++++++++++++++++++++++++++ |
379 | Mittelwert_AccNick = (Mittelwert_AccNick * 3 + ((ACC_AMPLIFY * AdWertAccNick))) / 4L; |
404 | Mittelwert_AccNick = (Mittelwert_AccNick * 3 + ((ACC_AMPLIFY * AdWertAccNick))) / 4L; |
380 | Mittelwert_AccRoll = (Mittelwert_AccRoll * 3 + ((ACC_AMPLIFY * AdWertAccRoll))) / 4L; |
405 | Mittelwert_AccRoll = (Mittelwert_AccRoll * 3 + ((ACC_AMPLIFY * AdWertAccRoll))) / 4L; |
381 | IntegralAccNick += ACC_AMPLIFY * AdWertAccNick; |
406 | IntegralAccNick += ACC_AMPLIFY * AdWertAccNick; |
382 | IntegralAccRoll += ACC_AMPLIFY * AdWertAccRoll; |
407 | IntegralAccRoll += ACC_AMPLIFY * AdWertAccRoll; |
383 | NaviAccNick += AdWertAccNick; |
408 | NaviAccNick += AdWertAccNick; |
384 | NaviAccRoll += AdWertAccRoll; |
409 | NaviAccRoll += AdWertAccRoll; |
385 | NaviCntAcc++; |
410 | NaviCntAcc++; |
386 | IntegralAccZ += Aktuell_az - NeutralAccZ; |
411 | IntegralAccZ += Aktuell_az - NeutralAccZ; |
387 | 412 | ||
388 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
413 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
389 | // ADC einschalten |
414 | // ADC einschalten |
390 | ANALOG_ON; |
415 | ANALOG_ON; |
391 | AdReady = 0; |
416 | AdReady = 0; |
392 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
417 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
393 | 418 | ||
394 | if(Mess_IntegralRoll > 93000L) winkel_roll = 93000L; |
419 | if(Mess_IntegralRoll > 93000L) winkel_roll = 93000L; |
395 | else if(Mess_IntegralRoll <-93000L) winkel_roll = -93000L; |
420 | else if(Mess_IntegralRoll <-93000L) winkel_roll = -93000L; |
396 | else winkel_roll = Mess_IntegralRoll; |
421 | else winkel_roll = Mess_IntegralRoll; |
397 | 422 | ||
398 | if(Mess_IntegralNick > 93000L) winkel_nick = 93000L; |
423 | if(Mess_IntegralNick > 93000L) winkel_nick = 93000L; |
399 | else if(Mess_IntegralNick <-93000L) winkel_nick = -93000L; |
424 | else if(Mess_IntegralNick <-93000L) winkel_nick = -93000L; |
400 | else winkel_nick = Mess_IntegralNick; |
425 | else winkel_nick = Mess_IntegralNick; |
401 | 426 | ||
402 | // Gier ++++++++++++++++++++++++++++++++++++++++++++++++ |
427 | // Gier ++++++++++++++++++++++++++++++++++++++++++++++++ |
403 | Mess_Integral_Gier += MesswertGier; |
428 | Mess_Integral_Gier += MesswertGier; |
404 | ErsatzKompass += MesswertGier; |
429 | ErsatzKompass += MesswertGier; |
405 | // Kopplungsanteil +++++++++++++++++++++++++++++++++++++ |
430 | // Kopplungsanteil +++++++++++++++++++++++++++++++++++++ |
406 | if(!Looping_Nick && !Looping_Roll && (EE_Parameter.GlobalConfig & CFG_ACHSENKOPPLUNG_AKTIV)) |
431 | if(!Looping_Nick && !Looping_Roll && (EE_Parameter.GlobalConfig & CFG_ACHSENKOPPLUNG_AKTIV)) |
407 | { |
432 | { |
408 | tmpl3 = (MesswertRoll * winkel_nick) / 2048L; |
433 | tmpl3 = (MesswertRoll * winkel_nick) / 2048L; |
409 | tmpl3 *= Parameter_AchsKopplung2; //65 |
434 | tmpl3 *= Parameter_AchsKopplung2; //65 |
410 | tmpl3 /= 4096L; |
435 | tmpl3 /= 4096L; |
411 | tmpl4 = (MesswertNick * winkel_roll) / 2048L; |
436 | tmpl4 = (MesswertNick * winkel_roll) / 2048L; |
412 | tmpl4 *= Parameter_AchsKopplung2; //65 |
437 | tmpl4 *= Parameter_AchsKopplung2; //65 |
413 | tmpl4 /= 4096L; |
438 | tmpl4 /= 4096L; |
414 | KopplungsteilNickRoll = tmpl3; |
439 | KopplungsteilNickRoll = tmpl3; |
415 | KopplungsteilRollNick = tmpl4; |
440 | KopplungsteilRollNick = tmpl4; |
416 | tmpl4 -= tmpl3; |
441 | tmpl4 -= tmpl3; |
417 | ErsatzKompass += tmpl4; |
442 | ErsatzKompass += tmpl4; |
418 | if(!Parameter_CouplingYawCorrection) Mess_Integral_Gier -= tmpl4/2; // Gier nachhelfen |
443 | if(!Parameter_CouplingYawCorrection) Mess_Integral_Gier -= tmpl4/2; // Gier nachhelfen |
419 | 444 | ||
420 | tmpl = ((MesswertGier + tmpl4) * winkel_nick) / 2048L; |
445 | tmpl = ((MesswertGier + tmpl4) * winkel_nick) / 2048L; |
421 | tmpl *= Parameter_AchsKopplung1; // 90 |
446 | tmpl *= Parameter_AchsKopplung1; // 90 |
422 | tmpl /= 4096L; |
447 | tmpl /= 4096L; |
423 | tmpl2 = ((MesswertGier + tmpl4) * winkel_roll) / 2048L; |
448 | tmpl2 = ((MesswertGier + tmpl4) * winkel_roll) / 2048L; |
424 | tmpl2 *= Parameter_AchsKopplung1; |
449 | tmpl2 *= Parameter_AchsKopplung1; |
425 | tmpl2 /= 4096L; |
450 | tmpl2 /= 4096L; |
426 | if(abs(MesswertGier) > 64) if(labs(tmpl) > 128 || labs(tmpl2) > 128) TrichterFlug = 1; |
451 | if(abs(MesswertGier) > 64) if(labs(tmpl) > 128 || labs(tmpl2) > 128) TrichterFlug = 1; |
427 | //MesswertGier += (Parameter_CouplingYawCorrection * tmpl4) / 256; |
452 | //MesswertGier += (Parameter_CouplingYawCorrection * tmpl4) / 256; |
428 | } |
453 | } |
429 | else tmpl = tmpl2 = KopplungsteilNickRoll = KopplungsteilRollNick = 0; |
454 | else tmpl = tmpl2 = KopplungsteilNickRoll = KopplungsteilRollNick = 0; |
430 | TrimRoll = tmpl - tmpl2 / 100L; |
455 | TrimRoll = tmpl - tmpl2 / 100L; |
431 | TrimNick = -tmpl2 + tmpl / 100L; |
456 | TrimNick = -tmpl2 + tmpl / 100L; |
432 | // Kompasswert begrenzen ++++++++++++++++++++++++++++++++++++++++++++++++ |
457 | // Kompasswert begrenzen ++++++++++++++++++++++++++++++++++++++++++++++++ |
433 | if(ErsatzKompass >= (360L * GIER_GRAD_FAKTOR)) ErsatzKompass -= 360L * GIER_GRAD_FAKTOR; // 360° Umschlag |
458 | if(ErsatzKompass >= (360L * GIER_GRAD_FAKTOR)) ErsatzKompass -= 360L * GIER_GRAD_FAKTOR; // 360° Umschlag |
434 | if(ErsatzKompass < 0) ErsatzKompass += 360L * GIER_GRAD_FAKTOR; |
459 | if(ErsatzKompass < 0) ErsatzKompass += 360L * GIER_GRAD_FAKTOR; |
435 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
460 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
436 | Mess_IntegralRoll2 += MesswertRoll + TrimRoll; |
461 | Mess_IntegralRoll2 += MesswertRoll + TrimRoll; |
437 | Mess_IntegralRoll += MesswertRoll + TrimRoll - LageKorrekturRoll; |
462 | Mess_IntegralRoll += MesswertRoll + TrimRoll - LageKorrekturRoll; |
438 | if(Mess_IntegralRoll > Umschlag180Roll) |
463 | if(Mess_IntegralRoll > Umschlag180Roll) |
439 | { |
464 | { |
440 | Mess_IntegralRoll = -(Umschlag180Roll - 25000L); |
465 | Mess_IntegralRoll = -(Umschlag180Roll - 25000L); |
441 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
466 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
442 | } |
467 | } |
443 | if(Mess_IntegralRoll <-Umschlag180Roll) |
468 | if(Mess_IntegralRoll <-Umschlag180Roll) |
444 | { |
469 | { |
445 | Mess_IntegralRoll = (Umschlag180Roll - 25000L); |
470 | Mess_IntegralRoll = (Umschlag180Roll - 25000L); |
446 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
471 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
447 | } |
472 | } |
448 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
473 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
449 | Mess_IntegralNick2 += MesswertNick + TrimNick; |
474 | Mess_IntegralNick2 += MesswertNick + TrimNick; |
450 | Mess_IntegralNick += MesswertNick + TrimNick - LageKorrekturNick; |
475 | Mess_IntegralNick += MesswertNick + TrimNick - LageKorrekturNick; |
451 | if(Mess_IntegralNick > Umschlag180Nick) |
476 | if(Mess_IntegralNick > Umschlag180Nick) |
452 | { |
477 | { |
453 | Mess_IntegralNick = -(Umschlag180Nick - 25000L); |
478 | Mess_IntegralNick = -(Umschlag180Nick - 25000L); |
454 | Mess_IntegralNick2 = Mess_IntegralNick; |
479 | Mess_IntegralNick2 = Mess_IntegralNick; |
455 | } |
480 | } |
456 | if(Mess_IntegralNick <-Umschlag180Nick) |
481 | if(Mess_IntegralNick <-Umschlag180Nick) |
457 | { |
482 | { |
458 | Mess_IntegralNick = (Umschlag180Nick - 25000L); |
483 | Mess_IntegralNick = (Umschlag180Nick - 25000L); |
459 | Mess_IntegralNick2 = Mess_IntegralNick; |
484 | Mess_IntegralNick2 = Mess_IntegralNick; |
460 | } |
485 | } |
461 | 486 | ||
462 | Integral_Gier = Mess_Integral_Gier; |
487 | Integral_Gier = Mess_Integral_Gier; |
463 | IntegralNick = Mess_IntegralNick; |
488 | IntegralNick = Mess_IntegralNick; |
464 | IntegralRoll = Mess_IntegralRoll; |
489 | IntegralRoll = Mess_IntegralRoll; |
465 | IntegralNick2 = Mess_IntegralNick2; |
490 | IntegralNick2 = Mess_IntegralNick2; |
466 | IntegralRoll2 = Mess_IntegralRoll2; |
491 | IntegralRoll2 = Mess_IntegralRoll2; |
467 | 492 | ||
468 | #define D_LIMIT 128 |
493 | #define D_LIMIT 128 |
469 | 494 | ||
470 | MesswertNick = HiResNick / 8; |
495 | MesswertNick = HiResNick / 8; |
471 | MesswertRoll = HiResRoll / 8; |
496 | MesswertRoll = HiResRoll / 8; |
472 | 497 | ||
473 | if(AdWertNick < 15) MesswertNick = -1000; if(AdWertNick < 7) MesswertNick = -2000; |
498 | if(AdWertNick < 15) MesswertNick = -1000; if(AdWertNick < 7) MesswertNick = -2000; |
474 | if(PlatinenVersion == 10) { if(AdWertNick > 1010) MesswertNick = +1000; if(AdWertNick > 1017) MesswertNick = +2000; } |
499 | if(PlatinenVersion == 10) { if(AdWertNick > 1010) MesswertNick = +1000; if(AdWertNick > 1017) MesswertNick = +2000; } |
475 | else { if(AdWertNick > 2000) MesswertNick = +1000; if(AdWertNick > 2015) MesswertNick = +2000; } |
500 | else { if(AdWertNick > 2000) MesswertNick = +1000; if(AdWertNick > 2015) MesswertNick = +2000; } |
476 | if(AdWertRoll < 15) MesswertRoll = -1000; if(AdWertRoll < 7) MesswertRoll = -2000; |
501 | if(AdWertRoll < 15) MesswertRoll = -1000; if(AdWertRoll < 7) MesswertRoll = -2000; |
477 | if(PlatinenVersion == 10) { if(AdWertRoll > 1010) MesswertRoll = +1000; if(AdWertRoll > 1017) MesswertRoll = +2000; } |
502 | if(PlatinenVersion == 10) { if(AdWertRoll > 1010) MesswertRoll = +1000; if(AdWertRoll > 1017) MesswertRoll = +2000; } |
478 | else { if(AdWertRoll > 2000) MesswertRoll = +1000; if(AdWertRoll > 2015) MesswertRoll = +2000; } |
503 | else { if(AdWertRoll > 2000) MesswertRoll = +1000; if(AdWertRoll > 2015) MesswertRoll = +2000; } |
479 | 504 | ||
480 | if(Parameter_Gyro_D) |
505 | if(Parameter_Gyro_D) |
481 | { |
506 | { |
482 | d2Nick = HiResNick - oldNick; |
507 | d2Nick = HiResNick - oldNick; |
483 | oldNick = (oldNick + HiResNick)/2; |
508 | oldNick = (oldNick + HiResNick)/2; |
484 | if(d2Nick > D_LIMIT) d2Nick = D_LIMIT; |
509 | if(d2Nick > D_LIMIT) d2Nick = D_LIMIT; |
485 | else if(d2Nick < -D_LIMIT) d2Nick = -D_LIMIT; |
510 | else if(d2Nick < -D_LIMIT) d2Nick = -D_LIMIT; |
486 | 511 | ||
487 | d2Roll = HiResRoll - oldRoll; |
512 | d2Roll = HiResRoll - oldRoll; |
488 | oldRoll = (oldRoll + HiResRoll)/2; |
513 | oldRoll = (oldRoll + HiResRoll)/2; |
489 | if(d2Roll > D_LIMIT) d2Roll = D_LIMIT; |
514 | if(d2Roll > D_LIMIT) d2Roll = D_LIMIT; |
490 | else if(d2Roll < -D_LIMIT) d2Roll = -D_LIMIT; |
515 | else if(d2Roll < -D_LIMIT) d2Roll = -D_LIMIT; |
491 | 516 | ||
492 | MesswertNick += (d2Nick * (signed int) Parameter_Gyro_D) / 16; |
517 | MesswertNick += (d2Nick * (signed int) Parameter_Gyro_D) / 16; |
493 | MesswertRoll += (d2Roll * (signed int) Parameter_Gyro_D) / 16; |
518 | MesswertRoll += (d2Roll * (signed int) Parameter_Gyro_D) / 16; |
494 | HiResNick += (d2Nick * (signed int) Parameter_Gyro_D); |
519 | HiResNick += (d2Nick * (signed int) Parameter_Gyro_D); |
495 | HiResRoll += (d2Roll * (signed int) Parameter_Gyro_D); |
520 | HiResRoll += (d2Roll * (signed int) Parameter_Gyro_D); |
496 | } |
521 | } |
497 | 522 | ||
498 | if(RohMesswertRoll > 0) TrimRoll += ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
523 | if(RohMesswertRoll > 0) TrimRoll += ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
499 | else TrimRoll -= ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
524 | else TrimRoll -= ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
500 | if(RohMesswertNick > 0) TrimNick += ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
525 | if(RohMesswertNick > 0) TrimNick += ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
501 | else TrimNick -= ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
526 | else TrimNick -= ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
502 | 527 | ||
503 | if(EE_Parameter.GlobalConfig & CFG_DREHRATEN_BEGRENZER && !Looping_Nick && !Looping_Roll) |
528 | if(EE_Parameter.GlobalConfig & CFG_DREHRATEN_BEGRENZER && !Looping_Nick && !Looping_Roll) |
504 | { |
529 | { |
505 | if(RohMesswertNick > 256) MesswertNick += 1 * (RohMesswertNick - 256); |
530 | if(RohMesswertNick > 256) MesswertNick += 1 * (RohMesswertNick - 256); |
506 | else if(RohMesswertNick < -256) MesswertNick += 1 * (RohMesswertNick + 256); |
531 | else if(RohMesswertNick < -256) MesswertNick += 1 * (RohMesswertNick + 256); |
507 | if(RohMesswertRoll > 256) MesswertRoll += 1 * (RohMesswertRoll - 256); |
532 | if(RohMesswertRoll > 256) MesswertRoll += 1 * (RohMesswertRoll - 256); |
508 | else if(RohMesswertRoll < -256) MesswertRoll += 1 * (RohMesswertRoll + 256); |
533 | else if(RohMesswertRoll < -256) MesswertRoll += 1 * (RohMesswertRoll + 256); |
509 | } |
534 | } |
510 | } |
535 | } |
511 | 536 | ||
512 | //############################################################################ |
537 | //############################################################################ |
513 | // Senden der Motorwerte per I2C-Bus |
538 | // Senden der Motorwerte per I2C-Bus |
514 | void SendMotorData(void) |
539 | void SendMotorData(void) |
515 | //############################################################################ |
540 | //############################################################################ |
516 | { |
541 | { |
517 | unsigned char i; |
542 | unsigned char i; |
518 | if(!MotorenEin) |
543 | if(!MotorenEin) |
519 | { |
544 | { |
520 | FC_StatusFlags &= ~(FC_STATUS_MOTOR_RUN | FC_STATUS_FLY); |
545 | FC_StatusFlags &= ~(FC_STATUS_MOTOR_RUN | FC_STATUS_FLY); |
521 | for(i=0;i<MAX_MOTORS;i++) |
546 | for(i=0;i<MAX_MOTORS;i++) |
522 | { |
547 | { |
523 | if(!PC_MotortestActive) MotorTest[i] = 0; |
548 | if(!PC_MotortestActive) MotorTest[i] = 0; |
524 | Motor[i].SetPoint = MotorTest[i]; |
549 | Motor[i].SetPoint = MotorTest[i]; |
525 | Motor[i].SetPointLowerBits = 0; |
550 | Motor[i].SetPointLowerBits = 0; |
526 | /* |
551 | /* |
527 | Motor[i].SetPoint = MotorTest[i] / 4; // testing the high resolution |
552 | Motor[i].SetPoint = MotorTest[i] / 4; // testing the high resolution |
528 | Motor[i].SetPointLowerBits = MotorTest[i] % 4; |
553 | Motor[i].SetPointLowerBits = MotorTest[i] % 4; |
529 | */ |
554 | */ |
530 | } |
555 | } |
531 | if(PC_MotortestActive) PC_MotortestActive--; |
556 | if(PC_MotortestActive) PC_MotortestActive--; |
532 | } |
557 | } |
533 | else FC_StatusFlags |= FC_STATUS_MOTOR_RUN; |
558 | else FC_StatusFlags |= FC_STATUS_MOTOR_RUN; |
534 | 559 | ||
535 | if(I2C_TransferActive) |
560 | if(I2C_TransferActive) |
536 | { |
561 | { |
537 | I2C_TransferActive = 0; // enable for the next time |
562 | I2C_TransferActive = 0; // enable for the next time |
538 | } |
563 | } |
539 | else |
564 | else |
540 | { |
565 | { |
541 | motor_write = 0; |
566 | motor_write = 0; |
542 | I2C_Start(TWI_STATE_MOTOR_TX); //Start I2C Interrupt Mode |
567 | I2C_Start(TWI_STATE_MOTOR_TX); //Start I2C Interrupt Mode |
543 | } |
568 | } |
544 | } |
569 | } |
545 | 570 | ||
546 | 571 | ||
547 | 572 | ||
548 | //############################################################################ |
573 | //############################################################################ |
549 | // Trägt ggf. das Poti als Parameter ein |
574 | // Trägt ggf. das Poti als Parameter ein |
550 | void ParameterZuordnung(void) |
575 | void ParameterZuordnung(void) |
551 | //############################################################################ |
576 | //############################################################################ |
552 | { |
577 | { |
553 | unsigned char tmp,i; |
578 | unsigned char tmp,i; |
554 | #define CHK_POTI(b,a) {if(a < 248) b = a; else b = Poti[255 - a];} |
579 | #define CHK_POTI(b,a) {if(a < 248) b = a; else b = Poti[255 - a];} |
555 | #define CHK_POTI_MM(b,a,min,max) {CHK_POTI(b,a); LIMIT_MIN_MAX(b, min, max);} |
580 | #define CHK_POTI_MM(b,a,min,max) {CHK_POTI(b,a); LIMIT_MIN_MAX(b, min, max);} |
556 | for(i=0;i<8;i++) |
581 | for(i=0;i<8;i++) |
557 | { |
582 | { |
558 | int tmp2; |
583 | int tmp2; |
559 | tmp2 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
584 | tmp2 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
560 | if(tmp2 > 255) tmp2 = 255; else if(tmp2 < 0) tmp2 = 0; |
585 | if(tmp2 > 255) tmp2 = 255; else if(tmp2 < 0) tmp2 = 0; |
561 | if(tmp2 != Poti[i]) |
586 | if(tmp2 != Poti[i]) |
562 | { |
587 | { |
563 | Poti[i] += (tmp2 - Poti[i]) / 4; |
588 | Poti[i] += (tmp2 - Poti[i]) / 4; |
564 | if(Poti[i] > tmp2) Poti[i]--; |
589 | if(Poti[i] > tmp2) Poti[i]--; |
565 | else Poti[i]++; |
590 | else Poti[i]++; |
566 | } |
591 | } |
567 | } |
592 | } |
568 | CHK_POTI_MM(Parameter_Luftdruck_D,EE_Parameter.Luftdruck_D,0,100); |
593 | CHK_POTI_MM(Parameter_Luftdruck_D,EE_Parameter.Luftdruck_D,0,100); |
569 | CHK_POTI_MM(Parameter_Hoehe_P,EE_Parameter.Hoehe_P,0,100); |
594 | CHK_POTI_MM(Parameter_Hoehe_P,EE_Parameter.Hoehe_P,0,100); |
570 | CHK_POTI_MM(Parameter_Gyro_P,EE_Parameter.Gyro_P,10,255); |
595 | CHK_POTI_MM(Parameter_Gyro_P,EE_Parameter.Gyro_P,10,255); |
571 | CHK_POTI_MM(Parameter_J16Timing,EE_Parameter.J16Timing,1,255); |
596 | CHK_POTI_MM(Parameter_J16Timing,EE_Parameter.J16Timing,1,255); |
572 | CHK_POTI_MM(Parameter_J17Timing,EE_Parameter.J17Timing,1,255); |
597 | CHK_POTI_MM(Parameter_J17Timing,EE_Parameter.J17Timing,1,255); |
573 | CHK_POTI(Parameter_Servo3,EE_Parameter.Servo3); |
598 | CHK_POTI(Parameter_Servo3,EE_Parameter.Servo3); |
574 | CHK_POTI(Parameter_Servo4,EE_Parameter.Servo4); |
599 | CHK_POTI(Parameter_Servo4,EE_Parameter.Servo4); |
575 | CHK_POTI(Parameter_Servo5,EE_Parameter.Servo5); |
600 | CHK_POTI(Parameter_Servo5,EE_Parameter.Servo5); |
576 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
601 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
577 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
602 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
578 | CHK_POTI(Parameter_Hoehe_ACC_Wirkung,EE_Parameter.Hoehe_ACC_Wirkung); |
603 | CHK_POTI(Parameter_Hoehe_ACC_Wirkung,EE_Parameter.Hoehe_ACC_Wirkung); |
579 | CHK_POTI(Parameter_Hoehe_GPS_Z,EE_Parameter.Hoehe_GPS_Z); |
604 | CHK_POTI(Parameter_Hoehe_GPS_Z,EE_Parameter.Hoehe_GPS_Z); |
580 | CHK_POTI(Parameter_KompassWirkung,EE_Parameter.KompassWirkung); |
605 | CHK_POTI(Parameter_KompassWirkung,EE_Parameter.KompassWirkung); |
581 | CHK_POTI(Parameter_Gyro_I,EE_Parameter.Gyro_I); |
606 | CHK_POTI(Parameter_Gyro_I,EE_Parameter.Gyro_I); |
582 | CHK_POTI(Parameter_Gyro_D,EE_Parameter.Gyro_D); |
607 | CHK_POTI(Parameter_Gyro_D,EE_Parameter.Gyro_D); |
583 | CHK_POTI(Parameter_Gyro_Gier_P,EE_Parameter.Gyro_Gier_P); |
608 | CHK_POTI(Parameter_Gyro_Gier_P,EE_Parameter.Gyro_Gier_P); |
584 | CHK_POTI(Parameter_Gyro_Gier_I,EE_Parameter.Gyro_Gier_I); |
609 | CHK_POTI(Parameter_Gyro_Gier_I,EE_Parameter.Gyro_Gier_I); |
585 | CHK_POTI(Parameter_I_Faktor,EE_Parameter.I_Faktor); |
610 | CHK_POTI(Parameter_I_Faktor,EE_Parameter.I_Faktor); |
586 | CHK_POTI(Parameter_UserParam1,EE_Parameter.UserParam1); |
611 | CHK_POTI(Parameter_UserParam1,EE_Parameter.UserParam1); |
587 | CHK_POTI(Parameter_UserParam2,EE_Parameter.UserParam2); |
612 | CHK_POTI(Parameter_UserParam2,EE_Parameter.UserParam2); |
588 | CHK_POTI(Parameter_UserParam3,EE_Parameter.UserParam3); |
613 | CHK_POTI(Parameter_UserParam3,EE_Parameter.UserParam3); |
589 | CHK_POTI(Parameter_UserParam4,EE_Parameter.UserParam4); |
614 | CHK_POTI(Parameter_UserParam4,EE_Parameter.UserParam4); |
590 | CHK_POTI(Parameter_UserParam5,EE_Parameter.UserParam5); |
615 | CHK_POTI(Parameter_UserParam5,EE_Parameter.UserParam5); |
591 | CHK_POTI(Parameter_UserParam6,EE_Parameter.UserParam6); |
616 | CHK_POTI(Parameter_UserParam6,EE_Parameter.UserParam6); |
592 | CHK_POTI(Parameter_UserParam7,EE_Parameter.UserParam7); |
617 | CHK_POTI(Parameter_UserParam7,EE_Parameter.UserParam7); |
593 | CHK_POTI(Parameter_UserParam8,EE_Parameter.UserParam8); |
618 | CHK_POTI(Parameter_UserParam8,EE_Parameter.UserParam8); |
594 | CHK_POTI(Parameter_ServoNickControl,EE_Parameter.ServoNickControl); |
619 | CHK_POTI(Parameter_ServoNickControl,EE_Parameter.ServoNickControl); |
595 | CHK_POTI(Parameter_ServoRollControl,EE_Parameter.ServoRollControl); |
620 | CHK_POTI(Parameter_ServoRollControl,EE_Parameter.ServoRollControl); |
596 | CHK_POTI(Parameter_LoopGasLimit,EE_Parameter.LoopGasLimit); |
621 | CHK_POTI(Parameter_LoopGasLimit,EE_Parameter.LoopGasLimit); |
597 | CHK_POTI(Parameter_AchsKopplung1,EE_Parameter.AchsKopplung1); |
622 | CHK_POTI(Parameter_AchsKopplung1,EE_Parameter.AchsKopplung1); |
598 | CHK_POTI(Parameter_AchsKopplung2,EE_Parameter.AchsKopplung2); |
623 | CHK_POTI(Parameter_AchsKopplung2,EE_Parameter.AchsKopplung2); |
599 | CHK_POTI(Parameter_CouplingYawCorrection,EE_Parameter.CouplingYawCorrection); |
624 | CHK_POTI(Parameter_CouplingYawCorrection,EE_Parameter.CouplingYawCorrection); |
600 | // CHK_POTI(Parameter_AchsGegenKopplung1,EE_Parameter.AchsGegenKopplung1,0,255); |
625 | // CHK_POTI(Parameter_AchsGegenKopplung1,EE_Parameter.AchsGegenKopplung1,0,255); |
601 | CHK_POTI(Parameter_DynamicStability,EE_Parameter.DynamicStability); |
626 | CHK_POTI(Parameter_DynamicStability,EE_Parameter.DynamicStability); |
602 | CHK_POTI(Parameter_ExternalControl,EE_Parameter.ExternalControl); |
627 | CHK_POTI(Parameter_ExternalControl,EE_Parameter.ExternalControl); |
603 | Ki = 10300 / (Parameter_I_Faktor + 1); |
628 | Ki = 10300 / (Parameter_I_Faktor + 1); |
604 | MAX_GAS = EE_Parameter.Gas_Max; |
629 | MAX_GAS = EE_Parameter.Gas_Max; |
605 | MIN_GAS = EE_Parameter.Gas_Min; |
630 | MIN_GAS = EE_Parameter.Gas_Min; |
606 | 631 | ||
607 | tmp = EE_Parameter.OrientationModeControl; |
632 | tmp = EE_Parameter.OrientationModeControl; |
608 | if(tmp > 50) |
633 | if(tmp > 50) |
609 | { |
634 | { |
610 | #ifdef SWITCH_LEARNS_CAREFREE |
635 | #ifdef SWITCH_LEARNS_CAREFREE |
611 | if(!CareFree) ControlHeading = (((int) EE_Parameter.OrientationAngle * 15 + KompassValue) % 360) / 2; |
636 | if(!CareFree) ControlHeading = (((int) EE_Parameter.OrientationAngle * 15 + KompassValue) % 360) / 2; |
612 | #endif |
637 | #endif |
613 | CareFree = 1; |
638 | CareFree = 1; |
614 | if(tmp >= 248 && Poti[255 - tmp] < 50) CareFree = 0; |
639 | if(tmp >= 248 && Poti[255 - tmp] < 50) CareFree = 0; |
615 | if(FromNaviCtrl.CompassValue < 0 && CareFree) VersionInfo.HardwareError[0] |= FC_ERROR0_CAREFREE; else VersionInfo.HardwareError[0] &= ~FC_ERROR0_CAREFREE; |
640 | if(FromNaviCtrl.CompassValue < 0 && CareFree) VersionInfo.HardwareError[0] |= FC_ERROR0_CAREFREE; else VersionInfo.HardwareError[0] &= ~FC_ERROR0_CAREFREE; |
616 | } |
641 | } |
617 | else CareFree = 0; |
642 | else CareFree = 0; |
618 | 643 | ||
619 | if(FromNaviCtrl.CompassValue < 0 && MotorenEin && CareFree && BeepMuster == 0xffff) // ungültiger Kompasswert |
644 | if(FromNaviCtrl.CompassValue < 0 && MotorenEin && CareFree && BeepMuster == 0xffff) // ungültiger Kompasswert |
620 | { |
645 | { |
621 | beeptime = 15000; |
646 | beeptime = 15000; |
622 | BeepMuster = 0xA400; |
647 | BeepMuster = 0xA400; |
623 | CareFree = 0; |
648 | CareFree = 0; |
624 | } |
649 | } |
625 | 650 | ||
626 | if(CareFree) {if(Parameter_AchsKopplung1 < 210) Parameter_AchsKopplung1 += 30;} |
651 | if(CareFree) {if(Parameter_AchsKopplung1 < 210) Parameter_AchsKopplung1 += 30;} |
627 | } |
652 | } |
628 | 653 | ||
629 | //############################################################################ |
654 | //############################################################################ |
630 | // |
655 | // |
631 | void MotorRegler(void) |
656 | void MotorRegler(void) |
632 | //############################################################################ |
657 | //############################################################################ |
633 | { |
658 | { |
634 | int pd_ergebnis_nick,pd_ergebnis_roll,tmp_int, tmp_int2; |
659 | int pd_ergebnis_nick,pd_ergebnis_roll,tmp_int, tmp_int2; |
635 | int GierMischanteil,GasMischanteil; |
660 | int GierMischanteil,GasMischanteil; |
636 | static long sollGier = 0,tmp_long,tmp_long2; |
661 | static long sollGier = 0,tmp_long,tmp_long2; |
637 | static long IntegralFehlerNick = 0; |
662 | static long IntegralFehlerNick = 0; |
638 | static long IntegralFehlerRoll = 0; |
663 | static long IntegralFehlerRoll = 0; |
639 | static unsigned int RcLostTimer; |
664 | static unsigned int RcLostTimer; |
640 | static unsigned char delay_neutral = 0; |
665 | static unsigned char delay_neutral = 0; |
641 | static unsigned char delay_einschalten = 0,delay_ausschalten = 0; |
666 | static unsigned char delay_einschalten = 0,delay_ausschalten = 0; |
642 | static unsigned char calibration_done = 0; |
667 | static unsigned char calibration_done = 0; |
643 | static char NeueKompassRichtungMerken = 0; |
668 | static char NeueKompassRichtungMerken = 0; |
644 | static long ausgleichNick, ausgleichRoll; |
669 | static long ausgleichNick, ausgleichRoll; |
645 | int IntegralNickMalFaktor,IntegralRollMalFaktor; |
670 | int IntegralNickMalFaktor,IntegralRollMalFaktor; |
646 | unsigned char i; |
671 | unsigned char i; |
647 | Mittelwert(); |
672 | Mittelwert(); |
648 | GRN_ON; |
673 | GRN_ON; |
649 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
674 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
650 | // Gaswert ermitteln |
675 | // Gaswert ermitteln |
651 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
676 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
652 | GasMischanteil = StickGas; |
677 | GasMischanteil = StickGas; |
653 | if(GasMischanteil < MIN_GAS + 10) GasMischanteil = MIN_GAS + 10; |
678 | if(GasMischanteil < MIN_GAS + 10) GasMischanteil = MIN_GAS + 10; |
654 | 679 | ||
655 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
680 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
656 | // Empfang schlecht |
681 | // Empfang schlecht |
657 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
682 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
658 | if(SenderOkay < 100) |
683 | if(SenderOkay < 100) |
659 | { |
684 | { |
660 | if(RcLostTimer) RcLostTimer--; |
685 | if(RcLostTimer) RcLostTimer--; |
661 | else |
686 | else |
662 | { |
687 | { |
663 | MotorenEin = 0; |
688 | MotorenEin = 0; |
664 | FC_StatusFlags &= ~FC_STATUS_EMERGENCY_LANDING; |
689 | FC_StatusFlags &= ~FC_STATUS_EMERGENCY_LANDING; |
665 | } |
690 | } |
666 | ROT_ON; |
691 | ROT_ON; |
667 | if(modell_fliegt > 1000) // wahrscheinlich in der Luft --> langsam absenken |
692 | if(modell_fliegt > 1000) // wahrscheinlich in der Luft --> langsam absenken |
668 | { |
693 | { |
669 | GasMischanteil = EE_Parameter.NotGas; |
694 | GasMischanteil = EE_Parameter.NotGas; |
670 | FC_StatusFlags |= FC_STATUS_EMERGENCY_LANDING; |
695 | FC_StatusFlags |= FC_STATUS_EMERGENCY_LANDING; |
671 | PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
696 | PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
672 | PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
697 | PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
673 | PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
698 | PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
674 | PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
699 | PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
675 | PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] = 0; |
700 | PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] = 0; |
676 | } |
701 | } |
677 | else MotorenEin = 0; |
702 | else MotorenEin = 0; |
678 | } |
703 | } |
679 | else |
704 | else |
680 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
705 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
681 | // Emfang gut |
706 | // Emfang gut |
682 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
707 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
683 | if(SenderOkay > 140) |
708 | if(SenderOkay > 140) |
684 | { |
709 | { |
685 | FC_StatusFlags &= ~FC_STATUS_EMERGENCY_LANDING; |
710 | FC_StatusFlags &= ~FC_STATUS_EMERGENCY_LANDING; |
686 | RcLostTimer = EE_Parameter.NotGasZeit * 50; |
711 | RcLostTimer = EE_Parameter.NotGasZeit * 50; |
687 | if(GasMischanteil > 40 && MotorenEin) |
712 | if(GasMischanteil > 40 && MotorenEin) |
688 | { |
713 | { |
689 | if(modell_fliegt < 0xffff) modell_fliegt++; |
714 | if(modell_fliegt < 0xffff) modell_fliegt++; |
690 | } |
715 | } |
691 | if((modell_fliegt < 256)) |
716 | if((modell_fliegt < 256)) |
692 | { |
717 | { |
693 | SummeNick = 0; |
718 | SummeNick = 0; |
694 | SummeRoll = 0; |
719 | SummeRoll = 0; |
695 | sollGier = 0; |
720 | sollGier = 0; |
696 | Mess_Integral_Gier = 0; |
721 | Mess_Integral_Gier = 0; |
697 | if(modell_fliegt == 250) |
722 | if(modell_fliegt == 250) |
698 | { |
723 | { |
699 | NeueKompassRichtungMerken = 1; |
724 | NeueKompassRichtungMerken = 1; |
700 | } |
725 | } |
701 | } else FC_StatusFlags |= FC_STATUS_FLY; |
726 | } else FC_StatusFlags |= FC_STATUS_FLY; |
702 | 727 | ||
703 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] > 80) && MotorenEin == 0) |
728 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] > 80) && MotorenEin == 0) |
704 | { |
729 | { |
705 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
730 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
706 | // auf Nullwerte kalibrieren |
731 | // auf Nullwerte kalibrieren |
707 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
732 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
708 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) // Neutralwerte |
733 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) // Neutralwerte |
709 | { |
734 | { |
710 | if(++delay_neutral > 200) // nicht sofort |
735 | if(++delay_neutral > 200) // nicht sofort |
711 | { |
736 | { |
712 | GRN_OFF; |
737 | GRN_OFF; |
713 | MotorenEin = 0; |
738 | MotorenEin = 0; |
714 | delay_neutral = 0; |
739 | delay_neutral = 0; |
715 | modell_fliegt = 0; |
740 | modell_fliegt = 0; |
716 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) > 70) |
741 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) > 70) |
717 | { |
742 | { |
718 | unsigned char setting=1; |
743 | unsigned char setting=1; |
719 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 1; |
744 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 1; |
720 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 2; |
745 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 2; |
721 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 3; |
746 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 3; |
722 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 4; |
747 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 4; |
723 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 5; |
748 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 5; |
724 | SetActiveParamSet(setting); // aktiven Datensatz merken |
749 | SetActiveParamSet(setting); // aktiven Datensatz merken |
725 | } |
750 | } |
726 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 30 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -70) |
751 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 30 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -70) |
727 | { |
752 | { |
728 | WinkelOut.CalcState = 1; |
753 | WinkelOut.CalcState = 1; |
729 | beeptime = 1000; |
754 | beeptime = 1000; |
730 | } |
755 | } |
731 | else |
756 | else |
732 | { |
757 | { |
733 | ParamSet_ReadFromEEProm(GetActiveParamSet()); |
758 | ParamSet_ReadFromEEProm(GetActiveParamSet()); |
734 | LipoDetection(0); |
759 | LipoDetection(0); |
735 | LIBFC_ReceiverInit(EE_Parameter.Receiver); |
760 | LIBFC_ReceiverInit(EE_Parameter.Receiver); |
736 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
761 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
737 | { |
762 | { |
738 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
763 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
739 | } |
764 | } |
740 | ServoActive = 0; |
765 | ServoActive = 0; |
741 | SetNeutral(0); |
766 | SetNeutral(0); |
742 | calibration_done = 1; |
767 | calibration_done = 1; |
743 | ServoActive = 1; |
768 | ServoActive = 1; |
744 | DDRD |=0x80; // enable J7 -> Servo signal |
769 | DDRD |=0x80; // enable J7 -> Servo signal |
745 | Piep(GetActiveParamSet(),120); |
770 | Piep(GetActiveParamSet(),120); |
746 | } |
771 | } |
747 | } |
772 | } |
748 | } |
773 | } |
749 | else |
774 | else |
750 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) // ACC Neutralwerte speichern |
775 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) // ACC Neutralwerte speichern |
751 | { |
776 | { |
752 | if(++delay_neutral > 200) // nicht sofort |
777 | if(++delay_neutral > 200) // nicht sofort |
753 | { |
778 | { |
754 | GRN_OFF; |
779 | GRN_OFF; |
755 | MotorenEin = 0; |
780 | MotorenEin = 0; |
756 | delay_neutral = 0; |
781 | delay_neutral = 0; |
757 | modell_fliegt = 0; |
782 | modell_fliegt = 0; |
758 | SetNeutral(1); |
783 | SetNeutral(1); |
759 | calibration_done = 1; |
784 | calibration_done = 1; |
760 | Piep(GetActiveParamSet(),120); |
785 | Piep(GetActiveParamSet(),120); |
761 | } |
786 | } |
762 | } |
787 | } |
763 | else delay_neutral = 0; |
788 | else delay_neutral = 0; |
764 | } |
789 | } |
765 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
790 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
766 | // Gas ist unten |
791 | // Gas ist unten |
767 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
792 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
768 | 793 | ||
769 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] < 35-120) |
794 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] < 35-120) |
770 | { |
795 | { |
771 | // Motoren Starten |
796 | // Motoren Starten |
772 | if(!MotorenEin) |
797 | if(!MotorenEin) |
773 | { |
798 | { |
774 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) && (PPM_in[EE_Parameter.MotorSafetySwitch] < -75 || EE_Parameter.MotorSafetySwitch == 0)) |
799 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) && (PPM_in[EE_Parameter.MotorSafetySwitch] < -75 || EE_Parameter.MotorSafetySwitch == 0)) |
775 | { |
800 | { |
776 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
801 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
777 | // Einschalten |
802 | // Einschalten |
778 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
803 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
779 | if(++delay_einschalten > 200) |
804 | if(++delay_einschalten > 200) |
780 | { |
805 | { |
781 | delay_einschalten = 0; |
806 | delay_einschalten = 0; |
782 | if(!VersionInfo.HardwareError[0] && calibration_done) |
807 | if(!VersionInfo.HardwareError[0] && calibration_done) |
783 | { |
808 | { |
784 | modell_fliegt = 1; |
809 | modell_fliegt = 1; |
785 | MotorenEin = 1; |
810 | MotorenEin = 1; |
786 | sollGier = 0; |
811 | sollGier = 0; |
787 | Mess_Integral_Gier = 0; |
812 | Mess_Integral_Gier = 0; |
788 | Mess_Integral_Gier2 = 0; |
813 | Mess_Integral_Gier2 = 0; |
789 | Mess_IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
814 | Mess_IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
790 | Mess_IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
815 | Mess_IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
791 | Mess_IntegralNick2 = IntegralNick; |
816 | Mess_IntegralNick2 = IntegralNick; |
792 | Mess_IntegralRoll2 = IntegralRoll; |
817 | Mess_IntegralRoll2 = IntegralRoll; |
793 | SummeNick = 0; |
818 | SummeNick = 0; |
794 | SummeRoll = 0; |
819 | SummeRoll = 0; |
795 | FC_StatusFlags |= FC_STATUS_START; |
820 | FC_StatusFlags |= FC_STATUS_START; |
796 | ControlHeading = (((int) EE_Parameter.OrientationAngle * 15 + KompassValue) % 360) / 2; |
821 | ControlHeading = (((int) EE_Parameter.OrientationAngle * 15 + KompassValue) % 360) / 2; |
797 | } |
822 | } |
798 | else |
823 | else |
799 | { |
824 | { |
800 | beeptime = 1500; // indicate missing calibration |
825 | beeptime = 1500; // indicate missing calibration |
801 | } |
826 | } |
802 | } |
827 | } |
803 | } |
828 | } |
804 | else delay_einschalten = 0; |
829 | else delay_einschalten = 0; |
805 | } |
830 | } |
806 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
831 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
807 | // Auschalten |
832 | // Auschalten |
808 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
833 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
809 | else // only if motors are running |
834 | else // only if motors are running |
810 | { |
835 | { |
811 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) && (PPM_in[EE_Parameter.MotorSafetySwitch] < -75 || EE_Parameter.MotorSafetySwitch == 0)) |
836 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) && (PPM_in[EE_Parameter.MotorSafetySwitch] < -75 || EE_Parameter.MotorSafetySwitch == 0)) |
812 | { |
837 | { |
813 | if(++delay_ausschalten > 200) // nicht sofort |
838 | if(++delay_ausschalten > 200) // nicht sofort |
814 | { |
839 | { |
815 | MotorenEin = 0; |
840 | MotorenEin = 0; |
816 | delay_ausschalten = 0; |
841 | delay_ausschalten = 0; |
817 | modell_fliegt = 0; |
842 | modell_fliegt = 0; |
818 | } |
843 | } |
819 | } |
844 | } |
820 | else delay_ausschalten = 0; |
845 | else delay_ausschalten = 0; |
821 | } |
846 | } |
822 | } |
847 | } |
823 | } |
848 | } |
824 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
849 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
825 | // neue Werte von der Funke |
850 | // neue Werte von der Funke |
826 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
851 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
827 | 852 | ||
828 | if(!NewPpmData-- || (FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
853 | if(!NewPpmData-- || (FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
829 | { |
854 | { |
830 | static int stick_nick,stick_roll; |
855 | static int stick_nick,stick_roll; |
831 | ParameterZuordnung(); |
856 | ParameterZuordnung(); |
832 | stick_nick = (stick_nick * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_P) / 4; |
857 | stick_nick = (stick_nick * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_P) / 4; |
833 | stick_nick += PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_D; |
858 | stick_nick += PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_D; |
834 | stick_roll = (stick_roll * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_P) / 4; |
859 | stick_roll = (stick_roll * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_P) / 4; |
835 | stick_roll += PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_D; |
860 | stick_roll += PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_D; |
836 | 861 | ||
837 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
862 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
838 | // CareFree und freie Wahl der vorderen Richtung |
863 | // CareFree und freie Wahl der vorderen Richtung |
839 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
864 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
840 | if(CareFree) |
865 | if(CareFree) |
841 | { |
866 | { |
842 | signed int nick, roll; |
867 | signed int nick, roll; |
843 | nick = stick_nick / 4; |
868 | nick = stick_nick / 4; |
844 | roll = stick_roll / 4; |
869 | roll = stick_roll / 4; |
845 | StickNick = ((FromNC_Rotate_C * nick) + (FromNC_Rotate_S * roll)) / (32 / 4); |
870 | StickNick = ((FromNC_Rotate_C * nick) + (FromNC_Rotate_S * roll)) / (32 / 4); |
846 | StickRoll = ((FromNC_Rotate_C * roll) - (FromNC_Rotate_S * nick)) / (32 / 4); |
871 | StickRoll = ((FromNC_Rotate_C * roll) - (FromNC_Rotate_S * nick)) / (32 / 4); |
847 | } |
872 | } |
848 | else |
873 | else |
849 | { |
874 | { |
850 | FromNC_Rotate_C = sintab[EE_Parameter.OrientationAngle + 6]; |
875 | FromNC_Rotate_C = sintab[EE_Parameter.OrientationAngle + 6]; |
851 | FromNC_Rotate_S = sintab[EE_Parameter.OrientationAngle]; |
876 | FromNC_Rotate_S = sintab[EE_Parameter.OrientationAngle]; |
852 | StickNick = ((FromNC_Rotate_C * stick_nick) + (FromNC_Rotate_S * stick_roll)) / 8; |
877 | StickNick = ((FromNC_Rotate_C * stick_nick) + (FromNC_Rotate_S * stick_roll)) / 8; |
853 | StickRoll = ((FromNC_Rotate_C * stick_roll) - (FromNC_Rotate_S * stick_nick)) / 8; |
878 | StickRoll = ((FromNC_Rotate_C * stick_roll) - (FromNC_Rotate_S * stick_nick)) / 8; |
854 | } |
879 | } |
855 | 880 | ||
856 | StickGier = -PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]; |
881 | StickGier = -PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]; |
857 | if(StickGier > 2) StickGier -= 2; else |
882 | if(StickGier > 2) StickGier -= 2; else |
858 | if(StickGier < -2) StickGier += 2; else StickGier = 0; |
883 | if(StickGier < -2) StickGier += 2; else StickGier = 0; |
859 | 884 | ||
860 | StickNick -= (GPS_Nick + GPS_Nick2); |
885 | StickNick -= (GPS_Nick + GPS_Nick2); |
861 | StickRoll -= (GPS_Roll + GPS_Roll2); |
886 | StickRoll -= (GPS_Roll + GPS_Roll2); |
862 | StickGas = PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] + 120; |
887 | StickGas = PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] + 120; |
863 | 888 | ||
864 | GyroFaktor = (Parameter_Gyro_P + 10.0); |
889 | GyroFaktor = (Parameter_Gyro_P + 10.0); |
865 | IntegralFaktor = Parameter_Gyro_I; |
890 | IntegralFaktor = Parameter_Gyro_I; |
866 | GyroFaktorGier = (Parameter_Gyro_Gier_P + 10.0); |
891 | GyroFaktorGier = (Parameter_Gyro_Gier_P + 10.0); |
867 | IntegralFaktorGier = Parameter_Gyro_Gier_I; |
892 | IntegralFaktorGier = Parameter_Gyro_Gier_I; |
868 | 893 | ||
869 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
894 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
870 | //+ Analoge Steuerung per Seriell |
895 | //+ Analoge Steuerung per Seriell |
871 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
896 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
872 | if(ExternControl.Config & 0x01 && Parameter_ExternalControl > 128) |
897 | if(ExternControl.Config & 0x01 && Parameter_ExternalControl > 128) |
873 | { |
898 | { |
874 | StickNick += (int) ExternControl.Nick * (int) EE_Parameter.Stick_P; |
899 | StickNick += (int) ExternControl.Nick * (int) EE_Parameter.Stick_P; |
875 | StickRoll += (int) ExternControl.Roll * (int) EE_Parameter.Stick_P; |
900 | StickRoll += (int) ExternControl.Roll * (int) EE_Parameter.Stick_P; |
876 | StickGier += ExternControl.Gier; |
901 | StickGier += ExternControl.Gier; |
877 | ExternHoehenValue = (int) ExternControl.Hight * (int)EE_Parameter.Hoehe_Verstaerkung; |
902 | ExternHoehenValue = (int) ExternControl.Hight * (int)EE_Parameter.Hoehe_Verstaerkung; |
878 | if(ExternControl.Gas < StickGas) StickGas = ExternControl.Gas; |
903 | if(ExternControl.Gas < StickGas) StickGas = ExternControl.Gas; |
879 | } |
904 | } |
880 | if(StickGas < 0) StickGas = 0; |
905 | if(StickGas < 0) StickGas = 0; |
881 | 906 | ||
882 | if(EE_Parameter.GlobalConfig & CFG_HEADING_HOLD) IntegralFaktor = 0; |
907 | if(EE_Parameter.GlobalConfig & CFG_HEADING_HOLD) IntegralFaktor = 0; |
883 | 908 | ||
884 | if(abs(StickNick/STICK_GAIN) > MaxStickNick) |
909 | if(abs(StickNick/STICK_GAIN) > MaxStickNick) |
885 | { |
910 | { |
886 | MaxStickNick = abs(StickNick)/STICK_GAIN; |
911 | MaxStickNick = abs(StickNick)/STICK_GAIN; |
887 | if(MaxStickNick > 100) MaxStickNick = 100; |
912 | if(MaxStickNick > 100) MaxStickNick = 100; |
888 | } |
913 | } |
889 | else MaxStickNick--; |
914 | else MaxStickNick--; |
890 | if(abs(StickRoll/STICK_GAIN) > MaxStickRoll) |
915 | if(abs(StickRoll/STICK_GAIN) > MaxStickRoll) |
891 | { |
916 | { |
892 | MaxStickRoll = abs(StickRoll)/STICK_GAIN; |
917 | MaxStickRoll = abs(StickRoll)/STICK_GAIN; |
893 | if(MaxStickRoll > 100) MaxStickRoll = 100; |
918 | if(MaxStickRoll > 100) MaxStickRoll = 100; |
894 | } |
919 | } |
895 | else MaxStickRoll--; |
920 | else MaxStickRoll--; |
896 | if(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING) {MaxStickNick = 0; MaxStickRoll = 0;} |
921 | if(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING) {MaxStickNick = 0; MaxStickRoll = 0;} |
897 | 922 | ||
898 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
923 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
899 | // Looping? |
924 | // Looping? |
900 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
925 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
901 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_LINKS) Looping_Links = 1; |
926 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_LINKS) Looping_Links = 1; |
902 | else |
927 | else |
903 | { |
928 | { |
904 | { |
929 | { |
905 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Links = 0; |
930 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Links = 0; |
906 | } |
931 | } |
907 | } |
932 | } |
908 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_RECHTS) Looping_Rechts = 1; |
933 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_RECHTS) Looping_Rechts = 1; |
909 | else |
934 | else |
910 | { |
935 | { |
911 | if(Looping_Rechts) // Hysterese |
936 | if(Looping_Rechts) // Hysterese |
912 | { |
937 | { |
913 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Rechts = 0; |
938 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Rechts = 0; |
914 | } |
939 | } |
915 | } |
940 | } |
916 | 941 | ||
917 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_OBEN) Looping_Oben = 1; |
942 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_OBEN) Looping_Oben = 1; |
918 | else |
943 | else |
919 | { |
944 | { |
920 | if(Looping_Oben) // Hysterese |
945 | if(Looping_Oben) // Hysterese |
921 | { |
946 | { |
922 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Oben = 0; |
947 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Oben = 0; |
923 | } |
948 | } |
924 | } |
949 | } |
925 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_UNTEN) Looping_Unten = 1; |
950 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_UNTEN) Looping_Unten = 1; |
926 | else |
951 | else |
927 | { |
952 | { |
928 | if(Looping_Unten) // Hysterese |
953 | if(Looping_Unten) // Hysterese |
929 | { |
954 | { |
930 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Unten = 0; |
955 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Unten = 0; |
931 | } |
956 | } |
932 | } |
957 | } |
933 | 958 | ||
934 | if(Looping_Links || Looping_Rechts) Looping_Roll = 1; else Looping_Roll = 0; |
959 | if(Looping_Links || Looping_Rechts) Looping_Roll = 1; else Looping_Roll = 0; |
935 | if(Looping_Oben || Looping_Unten) { Looping_Nick = 1; Looping_Roll = 0; Looping_Links = 0; Looping_Rechts = 0;} else Looping_Nick = 0; |
960 | if(Looping_Oben || Looping_Unten) { Looping_Nick = 1; Looping_Roll = 0; Looping_Links = 0; Looping_Rechts = 0;} else Looping_Nick = 0; |
936 | } // Ende neue Funken-Werte |
961 | } // Ende neue Funken-Werte |
937 | 962 | ||
938 | if(Looping_Roll || Looping_Nick) |
963 | if(Looping_Roll || Looping_Nick) |
939 | { |
964 | { |
940 | if(GasMischanteil > EE_Parameter.LoopGasLimit) GasMischanteil = EE_Parameter.LoopGasLimit; |
965 | if(GasMischanteil > EE_Parameter.LoopGasLimit) GasMischanteil = EE_Parameter.LoopGasLimit; |
941 | TrichterFlug = 1; |
966 | TrichterFlug = 1; |
942 | } |
967 | } |
943 | 968 | ||
944 | 969 | ||
945 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
970 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
946 | // Bei Empfangsausfall im Flug |
971 | // Bei Empfangsausfall im Flug |
947 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
972 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
948 | if(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING) |
973 | if(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING) |
949 | { |
974 | { |
950 | StickGier = 0; |
975 | StickGier = 0; |
951 | StickNick = 0; |
976 | StickNick = 0; |
952 | StickRoll = 0; |
977 | StickRoll = 0; |
953 | GyroFaktor = 90; |
978 | GyroFaktor = 90; |
954 | IntegralFaktor = 120; |
979 | IntegralFaktor = 120; |
955 | GyroFaktorGier = 90; |
980 | GyroFaktorGier = 90; |
956 | IntegralFaktorGier = 120; |
981 | IntegralFaktorGier = 120; |
957 | Looping_Roll = 0; |
982 | Looping_Roll = 0; |
958 | Looping_Nick = 0; |
983 | Looping_Nick = 0; |
959 | } |
984 | } |
960 | 985 | ||
961 | 986 | ||
962 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
987 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
963 | // Integrale auf ACC-Signal abgleichen |
988 | // Integrale auf ACC-Signal abgleichen |
964 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
989 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
965 | #define ABGLEICH_ANZAHL 256L |
990 | #define ABGLEICH_ANZAHL 256L |
966 | 991 | ||
967 | MittelIntegralNick += IntegralNick; // Für die Mittelwertbildung aufsummieren |
992 | MittelIntegralNick += IntegralNick; // Für die Mittelwertbildung aufsummieren |
968 | MittelIntegralRoll += IntegralRoll; |
993 | MittelIntegralRoll += IntegralRoll; |
969 | MittelIntegralNick2 += IntegralNick2; |
994 | MittelIntegralNick2 += IntegralNick2; |
970 | MittelIntegralRoll2 += IntegralRoll2; |
995 | MittelIntegralRoll2 += IntegralRoll2; |
971 | 996 | ||
972 | if(Looping_Nick || Looping_Roll) |
997 | if(Looping_Nick || Looping_Roll) |
973 | { |
998 | { |
974 | IntegralAccNick = 0; |
999 | IntegralAccNick = 0; |
975 | IntegralAccRoll = 0; |
1000 | IntegralAccRoll = 0; |
976 | MittelIntegralNick = 0; |
1001 | MittelIntegralNick = 0; |
977 | MittelIntegralRoll = 0; |
1002 | MittelIntegralRoll = 0; |
978 | MittelIntegralNick2 = 0; |
1003 | MittelIntegralNick2 = 0; |
979 | MittelIntegralRoll2 = 0; |
1004 | MittelIntegralRoll2 = 0; |
980 | Mess_IntegralNick2 = Mess_IntegralNick; |
1005 | Mess_IntegralNick2 = Mess_IntegralNick; |
981 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
1006 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
982 | ZaehlMessungen = 0; |
1007 | ZaehlMessungen = 0; |
983 | LageKorrekturNick = 0; |
1008 | LageKorrekturNick = 0; |
984 | LageKorrekturRoll = 0; |
1009 | LageKorrekturRoll = 0; |
985 | } |
1010 | } |
986 | 1011 | ||
987 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1012 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
988 | if(!Looping_Nick && !Looping_Roll && (Aktuell_az > 512 || MotorenEin)) |
1013 | if(!Looping_Nick && !Looping_Roll && (Aktuell_az > 512 || MotorenEin)) |
989 | { |
1014 | { |
990 | long tmp_long, tmp_long2; |
1015 | long tmp_long, tmp_long2; |
991 | if(FromNaviCtrl_Value.Kalman_K != -1 /*&& !TrichterFlug*/) |
1016 | if(FromNaviCtrl_Value.Kalman_K != -1 /*&& !TrichterFlug*/) |
992 | { |
1017 | { |
993 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
1018 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
994 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
1019 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
995 | tmp_long = (tmp_long * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
1020 | tmp_long = (tmp_long * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
996 | tmp_long2 = (tmp_long2 * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
1021 | tmp_long2 = (tmp_long2 * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
997 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
1022 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
998 | { |
1023 | { |
999 | tmp_long /= 2; |
1024 | tmp_long /= 2; |
1000 | tmp_long2 /= 2; |
1025 | tmp_long2 /= 2; |
1001 | } |
1026 | } |
1002 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
1027 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
1003 | { |
1028 | { |
1004 | tmp_long /= 3; |
1029 | tmp_long /= 3; |
1005 | tmp_long2 /= 3; |
1030 | tmp_long2 /= 3; |
1006 | } |
1031 | } |
1007 | if(tmp_long > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
1032 | if(tmp_long > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
1008 | if(tmp_long < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
1033 | if(tmp_long < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
1009 | if(tmp_long2 > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
1034 | if(tmp_long2 > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
1010 | if(tmp_long2 < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
1035 | if(tmp_long2 < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
1011 | } |
1036 | } |
1012 | else |
1037 | else |
1013 | { |
1038 | { |
1014 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
1039 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
1015 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
1040 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
1016 | tmp_long /= 16; |
1041 | tmp_long /= 16; |
1017 | tmp_long2 /= 16; |
1042 | tmp_long2 /= 16; |
1018 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
1043 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
1019 | { |
1044 | { |
1020 | tmp_long /= 3; |
1045 | tmp_long /= 3; |
1021 | tmp_long2 /= 3; |
1046 | tmp_long2 /= 3; |
1022 | } |
1047 | } |
1023 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
1048 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
1024 | { |
1049 | { |
1025 | tmp_long /= 3; |
1050 | tmp_long /= 3; |
1026 | tmp_long2 /= 3; |
1051 | tmp_long2 /= 3; |
1027 | } |
1052 | } |
1028 | 1053 | ||
1029 | #define AUSGLEICH 32 |
1054 | #define AUSGLEICH 32 |
1030 | if(tmp_long > AUSGLEICH) tmp_long = AUSGLEICH; |
1055 | if(tmp_long > AUSGLEICH) tmp_long = AUSGLEICH; |
1031 | if(tmp_long < -AUSGLEICH) tmp_long =-AUSGLEICH; |
1056 | if(tmp_long < -AUSGLEICH) tmp_long =-AUSGLEICH; |
1032 | if(tmp_long2 > AUSGLEICH) tmp_long2 = AUSGLEICH; |
1057 | if(tmp_long2 > AUSGLEICH) tmp_long2 = AUSGLEICH; |
1033 | if(tmp_long2 <-AUSGLEICH) tmp_long2 =-AUSGLEICH; |
1058 | if(tmp_long2 <-AUSGLEICH) tmp_long2 =-AUSGLEICH; |
1034 | } |
1059 | } |
1035 | 1060 | ||
1036 | Mess_IntegralNick -= tmp_long; |
1061 | Mess_IntegralNick -= tmp_long; |
1037 | Mess_IntegralRoll -= tmp_long2; |
1062 | Mess_IntegralRoll -= tmp_long2; |
1038 | } |
1063 | } |
1039 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1064 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1040 | if(ZaehlMessungen >= ABGLEICH_ANZAHL) |
1065 | if(ZaehlMessungen >= ABGLEICH_ANZAHL) |
1041 | { |
1066 | { |
1042 | static int cnt = 0; |
1067 | static int cnt = 0; |
1043 | static char last_n_p,last_n_n,last_r_p,last_r_n; |
1068 | static char last_n_p,last_n_n,last_r_p,last_r_n; |
1044 | static long MittelIntegralNick_Alt,MittelIntegralRoll_Alt; |
1069 | static long MittelIntegralNick_Alt,MittelIntegralRoll_Alt; |
1045 | if(!Looping_Nick && !Looping_Roll && !TrichterFlug && EE_Parameter.Driftkomp) |
1070 | if(!Looping_Nick && !Looping_Roll && !TrichterFlug && EE_Parameter.Driftkomp) |
1046 | { |
1071 | { |
1047 | MittelIntegralNick /= ABGLEICH_ANZAHL; |
1072 | MittelIntegralNick /= ABGLEICH_ANZAHL; |
1048 | MittelIntegralRoll /= ABGLEICH_ANZAHL; |
1073 | MittelIntegralRoll /= ABGLEICH_ANZAHL; |
1049 | IntegralAccNick = (EE_Parameter.GyroAccFaktor * IntegralAccNick) / ABGLEICH_ANZAHL; |
1074 | IntegralAccNick = (EE_Parameter.GyroAccFaktor * IntegralAccNick) / ABGLEICH_ANZAHL; |
1050 | IntegralAccRoll = (EE_Parameter.GyroAccFaktor * IntegralAccRoll) / ABGLEICH_ANZAHL; |
1075 | IntegralAccRoll = (EE_Parameter.GyroAccFaktor * IntegralAccRoll) / ABGLEICH_ANZAHL; |
1051 | IntegralAccZ = IntegralAccZ / ABGLEICH_ANZAHL; |
1076 | IntegralAccZ = IntegralAccZ / ABGLEICH_ANZAHL; |
1052 | #define MAX_I 0 |
1077 | #define MAX_I 0 |
1053 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
1078 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
1054 | IntegralFehlerNick = (long)(MittelIntegralNick - (long)IntegralAccNick); |
1079 | IntegralFehlerNick = (long)(MittelIntegralNick - (long)IntegralAccNick); |
1055 | ausgleichNick = IntegralFehlerNick / EE_Parameter.GyroAccAbgleich; |
1080 | ausgleichNick = IntegralFehlerNick / EE_Parameter.GyroAccAbgleich; |
1056 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
1081 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
1057 | IntegralFehlerRoll = (long)(MittelIntegralRoll - (long)IntegralAccRoll); |
1082 | IntegralFehlerRoll = (long)(MittelIntegralRoll - (long)IntegralAccRoll); |
1058 | ausgleichRoll = IntegralFehlerRoll / EE_Parameter.GyroAccAbgleich; |
1083 | ausgleichRoll = IntegralFehlerRoll / EE_Parameter.GyroAccAbgleich; |
1059 | 1084 | ||
1060 | LageKorrekturNick = ausgleichNick / ABGLEICH_ANZAHL; |
1085 | LageKorrekturNick = ausgleichNick / ABGLEICH_ANZAHL; |
1061 | LageKorrekturRoll = ausgleichRoll / ABGLEICH_ANZAHL; |
1086 | LageKorrekturRoll = ausgleichRoll / ABGLEICH_ANZAHL; |
1062 | 1087 | ||
1063 | if(((MaxStickNick > 64) || (MaxStickRoll > 64) || (abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25)) && (FromNaviCtrl_Value.Kalman_K == -1)) |
1088 | if(((MaxStickNick > 64) || (MaxStickRoll > 64) || (abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25)) && (FromNaviCtrl_Value.Kalman_K == -1)) |
1064 | { |
1089 | { |
1065 | LageKorrekturNick /= 2; |
1090 | LageKorrekturNick /= 2; |
1066 | LageKorrekturRoll /= 2; |
1091 | LageKorrekturRoll /= 2; |
1067 | } |
1092 | } |
1068 | 1093 | ||
1069 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1094 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1070 | // Gyro-Drift ermitteln |
1095 | // Gyro-Drift ermitteln |
1071 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1096 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1072 | MittelIntegralNick2 /= ABGLEICH_ANZAHL; |
1097 | MittelIntegralNick2 /= ABGLEICH_ANZAHL; |
1073 | MittelIntegralRoll2 /= ABGLEICH_ANZAHL; |
1098 | MittelIntegralRoll2 /= ABGLEICH_ANZAHL; |
1074 | tmp_long = IntegralNick2 - IntegralNick; |
1099 | tmp_long = IntegralNick2 - IntegralNick; |
1075 | tmp_long2 = IntegralRoll2 - IntegralRoll; |
1100 | tmp_long2 = IntegralRoll2 - IntegralRoll; |
1076 | 1101 | ||
1077 | IntegralFehlerNick = tmp_long; |
1102 | IntegralFehlerNick = tmp_long; |
1078 | IntegralFehlerRoll = tmp_long2; |
1103 | IntegralFehlerRoll = tmp_long2; |
1079 | Mess_IntegralNick2 -= IntegralFehlerNick; |
1104 | Mess_IntegralNick2 -= IntegralFehlerNick; |
1080 | Mess_IntegralRoll2 -= IntegralFehlerRoll; |
1105 | Mess_IntegralRoll2 -= IntegralFehlerRoll; |
1081 | 1106 | ||
1082 | if(EE_Parameter.Driftkomp) |
1107 | if(EE_Parameter.Driftkomp) |
1083 | { |
1108 | { |
1084 | if(GierGyroFehler > ABGLEICH_ANZAHL/2) { AdNeutralGier++; } |
1109 | if(GierGyroFehler > ABGLEICH_ANZAHL/2) { AdNeutralGier++; } |
1085 | if(GierGyroFehler <-ABGLEICH_ANZAHL/2) { AdNeutralGier--; } |
1110 | if(GierGyroFehler <-ABGLEICH_ANZAHL/2) { AdNeutralGier--; } |
1086 | } |
1111 | } |
1087 | GierGyroFehler = 0; |
1112 | GierGyroFehler = 0; |
1088 | 1113 | ||
1089 | #define FEHLER_LIMIT (ABGLEICH_ANZAHL / 2) |
1114 | #define FEHLER_LIMIT (ABGLEICH_ANZAHL / 2) |
1090 | #define FEHLER_LIMIT1 (ABGLEICH_ANZAHL * 2) //4 |
1115 | #define FEHLER_LIMIT1 (ABGLEICH_ANZAHL * 2) //4 |
1091 | #define FEHLER_LIMIT2 (ABGLEICH_ANZAHL * 16) //16 |
1116 | #define FEHLER_LIMIT2 (ABGLEICH_ANZAHL * 16) //16 |
1092 | #define BEWEGUNGS_LIMIT 20000 |
1117 | #define BEWEGUNGS_LIMIT 20000 |
1093 | // Nick +++++++++++++++++++++++++++++++++++++++++++++++++ |
1118 | // Nick +++++++++++++++++++++++++++++++++++++++++++++++++ |
1094 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
1119 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
1095 | if(labs(IntegralFehlerNick) > FEHLER_LIMIT1) cnt = 4; |
1120 | if(labs(IntegralFehlerNick) > FEHLER_LIMIT1) cnt = 4; |
1096 | if(labs(MittelIntegralNick_Alt - MittelIntegralNick) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
1121 | if(labs(MittelIntegralNick_Alt - MittelIntegralNick) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
1097 | { |
1122 | { |
1098 | if(IntegralFehlerNick > FEHLER_LIMIT2) |
1123 | if(IntegralFehlerNick > FEHLER_LIMIT2) |
1099 | { |
1124 | { |
1100 | if(last_n_p) |
1125 | if(last_n_p) |
1101 | { |
1126 | { |
1102 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
1127 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
1103 | ausgleichNick = IntegralFehlerNick / 8; |
1128 | ausgleichNick = IntegralFehlerNick / 8; |
1104 | if(ausgleichNick > 5000) ausgleichNick = 5000; |
1129 | if(ausgleichNick > 5000) ausgleichNick = 5000; |
1105 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1130 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1106 | } |
1131 | } |
1107 | else last_n_p = 1; |
1132 | else last_n_p = 1; |
1108 | } else last_n_p = 0; |
1133 | } else last_n_p = 0; |
1109 | if(IntegralFehlerNick < -FEHLER_LIMIT2) |
1134 | if(IntegralFehlerNick < -FEHLER_LIMIT2) |
1110 | { |
1135 | { |
1111 | if(last_n_n) |
1136 | if(last_n_n) |
1112 | { |
1137 | { |
1113 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
1138 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
1114 | ausgleichNick = IntegralFehlerNick / 8; |
1139 | ausgleichNick = IntegralFehlerNick / 8; |
1115 | if(ausgleichNick < -5000) ausgleichNick = -5000; |
1140 | if(ausgleichNick < -5000) ausgleichNick = -5000; |
1116 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1141 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1117 | } |
1142 | } |
1118 | else last_n_n = 1; |
1143 | else last_n_n = 1; |
1119 | } else last_n_n = 0; |
1144 | } else last_n_n = 0; |
1120 | } |
1145 | } |
1121 | else |
1146 | else |
1122 | { |
1147 | { |
1123 | cnt = 0; |
1148 | cnt = 0; |
1124 | KompassSignalSchlecht = 1000; |
1149 | KompassSignalSchlecht = 1000; |
1125 | } |
1150 | } |
1126 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1151 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1127 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
1152 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
1128 | if(IntegralFehlerNick > FEHLER_LIMIT) AdNeutralNick += cnt; |
1153 | if(IntegralFehlerNick > FEHLER_LIMIT) AdNeutralNick += cnt; |
1129 | if(IntegralFehlerNick < -FEHLER_LIMIT) AdNeutralNick -= cnt; |
1154 | if(IntegralFehlerNick < -FEHLER_LIMIT) AdNeutralNick -= cnt; |
1130 | 1155 | ||
1131 | // Roll +++++++++++++++++++++++++++++++++++++++++++++++++ |
1156 | // Roll +++++++++++++++++++++++++++++++++++++++++++++++++ |
1132 | cnt = 1;// + labs(IntegralFehlerRoll) / 4096; |
1157 | cnt = 1;// + labs(IntegralFehlerRoll) / 4096; |
1133 | if(labs(IntegralFehlerRoll) > FEHLER_LIMIT1) cnt = 4; |
1158 | if(labs(IntegralFehlerRoll) > FEHLER_LIMIT1) cnt = 4; |
1134 | if(labs(MittelIntegralRoll_Alt - MittelIntegralRoll) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
1159 | if(labs(MittelIntegralRoll_Alt - MittelIntegralRoll) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
1135 | { |
1160 | { |
1136 | if(IntegralFehlerRoll > FEHLER_LIMIT2) |
1161 | if(IntegralFehlerRoll > FEHLER_LIMIT2) |
1137 | { |
1162 | { |
1138 | if(last_r_p) |
1163 | if(last_r_p) |
1139 | { |
1164 | { |
1140 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
1165 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
1141 | ausgleichRoll = IntegralFehlerRoll / 8; |
1166 | ausgleichRoll = IntegralFehlerRoll / 8; |
1142 | if(ausgleichRoll > 5000) ausgleichRoll = 5000; |
1167 | if(ausgleichRoll > 5000) ausgleichRoll = 5000; |
1143 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
1168 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
1144 | } |
1169 | } |
1145 | else last_r_p = 1; |
1170 | else last_r_p = 1; |
1146 | } else last_r_p = 0; |
1171 | } else last_r_p = 0; |
1147 | if(IntegralFehlerRoll < -FEHLER_LIMIT2) |
1172 | if(IntegralFehlerRoll < -FEHLER_LIMIT2) |
1148 | { |
1173 | { |
1149 | if(last_r_n) |
1174 | if(last_r_n) |
1150 | { |
1175 | { |
1151 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
1176 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
1152 | ausgleichRoll = IntegralFehlerRoll / 8; |
1177 | ausgleichRoll = IntegralFehlerRoll / 8; |
1153 | if(ausgleichRoll < -5000) ausgleichRoll = -5000; |
1178 | if(ausgleichRoll < -5000) ausgleichRoll = -5000; |
1154 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
1179 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
1155 | } |
1180 | } |
1156 | else last_r_n = 1; |
1181 | else last_r_n = 1; |
1157 | } else last_r_n = 0; |
1182 | } else last_r_n = 0; |
1158 | } else |
1183 | } else |
1159 | { |
1184 | { |
1160 | cnt = 0; |
1185 | cnt = 0; |
1161 | KompassSignalSchlecht = 1000; |
1186 | KompassSignalSchlecht = 1000; |
1162 | } |
1187 | } |
1163 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1188 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1164 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
1189 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
1165 | if(IntegralFehlerRoll > FEHLER_LIMIT) AdNeutralRoll += cnt; |
1190 | if(IntegralFehlerRoll > FEHLER_LIMIT) AdNeutralRoll += cnt; |
1166 | if(IntegralFehlerRoll < -FEHLER_LIMIT) AdNeutralRoll -= cnt; |
1191 | if(IntegralFehlerRoll < -FEHLER_LIMIT) AdNeutralRoll -= cnt; |
1167 | } |
1192 | } |
1168 | else |
1193 | else |
1169 | { |
1194 | { |
1170 | LageKorrekturRoll = 0; |
1195 | LageKorrekturRoll = 0; |
1171 | LageKorrekturNick = 0; |
1196 | LageKorrekturNick = 0; |
1172 | TrichterFlug = 0; |
1197 | TrichterFlug = 0; |
1173 | } |
1198 | } |
1174 | 1199 | ||
1175 | if(!IntegralFaktor) { LageKorrekturRoll = 0; LageKorrekturNick = 0;} // z.B. bei HH |
1200 | if(!IntegralFaktor) { LageKorrekturRoll = 0; LageKorrekturNick = 0;} // z.B. bei HH |
1176 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1201 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1177 | MittelIntegralNick_Alt = MittelIntegralNick; |
1202 | MittelIntegralNick_Alt = MittelIntegralNick; |
1178 | MittelIntegralRoll_Alt = MittelIntegralRoll; |
1203 | MittelIntegralRoll_Alt = MittelIntegralRoll; |
1179 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1204 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1180 | IntegralAccNick = 0; |
1205 | IntegralAccNick = 0; |
1181 | IntegralAccRoll = 0; |
1206 | IntegralAccRoll = 0; |
1182 | IntegralAccZ = 0; |
1207 | IntegralAccZ = 0; |
1183 | MittelIntegralNick = 0; |
1208 | MittelIntegralNick = 0; |
1184 | MittelIntegralRoll = 0; |
1209 | MittelIntegralRoll = 0; |
1185 | MittelIntegralNick2 = 0; |
1210 | MittelIntegralNick2 = 0; |
1186 | MittelIntegralRoll2 = 0; |
1211 | MittelIntegralRoll2 = 0; |
1187 | ZaehlMessungen = 0; |
1212 | ZaehlMessungen = 0; |
1188 | } // ZaehlMessungen >= ABGLEICH_ANZAHL |
1213 | } // ZaehlMessungen >= ABGLEICH_ANZAHL |
1189 | 1214 | ||
1190 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1215 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1191 | // Gieren |
1216 | // Gieren |
1192 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1217 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1193 | if(abs(StickGier) > 15) // war 35 |
1218 | if(abs(StickGier) > 15) // war 35 |
1194 | { |
1219 | { |
1195 | KompassSignalSchlecht = 1000; |
1220 | KompassSignalSchlecht = 1000; |
1196 | if(!(EE_Parameter.GlobalConfig & CFG_KOMPASS_FIX)) |
1221 | if(!(EE_Parameter.GlobalConfig & CFG_KOMPASS_FIX)) |
1197 | { |
1222 | { |
1198 | NeueKompassRichtungMerken = 1; |
1223 | NeueKompassRichtungMerken = 1; |
1199 | }; |
1224 | }; |
1200 | } |
1225 | } |
1201 | tmp_int = (long) EE_Parameter.Gier_P * ((long)StickGier * abs(StickGier)) / 512L; // expo y = ax + bx² |
1226 | tmp_int = (long) EE_Parameter.Gier_P * ((long)StickGier * abs(StickGier)) / 512L; // expo y = ax + bx² |
1202 | tmp_int += (EE_Parameter.Gier_P * StickGier) / 4; |
1227 | tmp_int += (EE_Parameter.Gier_P * StickGier) / 4; |
1203 | sollGier = tmp_int; |
1228 | sollGier = tmp_int; |
1204 | Mess_Integral_Gier -= tmp_int; |
1229 | Mess_Integral_Gier -= tmp_int; |
1205 | if(Mess_Integral_Gier > 50000) Mess_Integral_Gier = 50000; // begrenzen |
1230 | if(Mess_Integral_Gier > 50000) Mess_Integral_Gier = 50000; // begrenzen |
1206 | if(Mess_Integral_Gier <-50000) Mess_Integral_Gier =-50000; |
1231 | if(Mess_Integral_Gier <-50000) Mess_Integral_Gier =-50000; |
1207 | 1232 | ||
1208 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1233 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1209 | // Kompass |
1234 | // Kompass |
1210 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1235 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1211 | if(KompassValue && (EE_Parameter.GlobalConfig & CFG_KOMPASS_AKTIV)) |
1236 | if(KompassValue && (EE_Parameter.GlobalConfig & CFG_KOMPASS_AKTIV)) |
1212 | { |
1237 | { |
1213 | int w,v,r,fehler,korrektur; |
1238 | int w,v,r,fehler,korrektur; |
1214 | w = abs(IntegralNick /512); // mit zunehmender Neigung den Einfluss drosseln |
1239 | w = abs(IntegralNick /512); // mit zunehmender Neigung den Einfluss drosseln |
1215 | v = abs(IntegralRoll /512); |
1240 | v = abs(IntegralRoll /512); |
1216 | if(v > w) w = v; // grösste Neigung ermitteln |
1241 | if(v > w) w = v; // grösste Neigung ermitteln |
1217 | korrektur = w / 8 + 2; |
1242 | korrektur = w / 8 + 2; |
1218 | fehler = ((540 + KompassValue - (ErsatzKompass/GIER_GRAD_FAKTOR)) % 360) - 180; |
1243 | fehler = ((540 + KompassValue - (ErsatzKompass/GIER_GRAD_FAKTOR)) % 360) - 180; |
1219 | //fehler += MesswertGier / 12; |
1244 | //fehler += MesswertGier / 12; |
1220 | 1245 | ||
1221 | if(!KompassSignalSchlecht && w < 25) |
1246 | if(!KompassSignalSchlecht && w < 25) |
1222 | { |
1247 | { |
1223 | GierGyroFehler += fehler; |
1248 | GierGyroFehler += fehler; |
1224 | if(NeueKompassRichtungMerken) |
1249 | if(NeueKompassRichtungMerken) |
1225 | { |
1250 | { |
1226 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
1251 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
1227 | KompassStartwert = (ErsatzKompass/GIER_GRAD_FAKTOR); |
1252 | KompassStartwert = (ErsatzKompass/GIER_GRAD_FAKTOR); |
1228 | NeueKompassRichtungMerken = 0; |
1253 | NeueKompassRichtungMerken = 0; |
1229 | } |
1254 | } |
1230 | } |
1255 | } |
1231 | ErsatzKompass += (fehler * 16) / korrektur; |
1256 | ErsatzKompass += (fehler * 16) / korrektur; |
1232 | w = (w * Parameter_KompassWirkung) / 32; // auf die Wirkung normieren |
1257 | w = (w * Parameter_KompassWirkung) / 32; // auf die Wirkung normieren |
1233 | w = Parameter_KompassWirkung - w; // Wirkung ggf drosseln |
1258 | w = Parameter_KompassWirkung - w; // Wirkung ggf drosseln |
1234 | if(w >= 0) |
1259 | if(w >= 0) |
1235 | { |
1260 | { |
1236 | if(!KompassSignalSchlecht) |
1261 | if(!KompassSignalSchlecht) |
1237 | { |
1262 | { |
1238 | v = 64 + ((MaxStickNick + MaxStickRoll)) / 8; |
1263 | v = 64 + ((MaxStickNick + MaxStickRoll)) / 8; |
1239 | r = ((540 + (ErsatzKompass/GIER_GRAD_FAKTOR) - KompassStartwert) % 360) - 180; |
1264 | r = ((540 + (ErsatzKompass/GIER_GRAD_FAKTOR) - KompassStartwert) % 360) - 180; |
1240 | v = (r * w) / v; // nach Kompass ausrichten |
1265 | v = (r * w) / v; // nach Kompass ausrichten |
1241 | w = 3 * Parameter_KompassWirkung; |
1266 | w = 3 * Parameter_KompassWirkung; |
1242 | if(v > w) v = w; // Begrenzen |
1267 | if(v > w) v = w; // Begrenzen |
1243 | else |
1268 | else |
1244 | if(v < -w) v = -w; |
1269 | if(v < -w) v = -w; |
1245 | Mess_Integral_Gier += v; |
1270 | Mess_Integral_Gier += v; |
1246 | } |
1271 | } |
1247 | if(KompassSignalSchlecht) KompassSignalSchlecht--; |
1272 | if(KompassSignalSchlecht) KompassSignalSchlecht--; |
1248 | } |
1273 | } |
1249 | else KompassSignalSchlecht = 500; // so lange das Signal taub stellen --> ca. 1 sek |
1274 | else KompassSignalSchlecht = 500; // so lange das Signal taub stellen --> ca. 1 sek |
1250 | } |
1275 | } |
1251 | 1276 | ||
1252 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1277 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1253 | // Drehgeschwindigkeit und -winkel zu einem Istwert zusammenfassen |
1278 | // Drehgeschwindigkeit und -winkel zu einem Istwert zusammenfassen |
1254 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1279 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1255 | if(TrichterFlug) { SummeRoll = 0; SummeNick = 0;}; |
1280 | if(TrichterFlug) { SummeRoll = 0; SummeNick = 0;}; |
1256 | 1281 | ||
1257 | if(!Looping_Nick) IntegralNickMalFaktor = (IntegralNick * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralNickMalFaktor = 0; |
1282 | if(!Looping_Nick) IntegralNickMalFaktor = (IntegralNick * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralNickMalFaktor = 0; |
1258 | if(!Looping_Roll) IntegralRollMalFaktor = (IntegralRoll * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralRollMalFaktor = 0; |
1283 | if(!Looping_Roll) IntegralRollMalFaktor = (IntegralRoll * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralRollMalFaktor = 0; |
1259 | 1284 | ||
1260 | #define TRIM_MAX 200 |
1285 | #define TRIM_MAX 200 |
1261 | if(TrimNick > TRIM_MAX) TrimNick = TRIM_MAX; else if(TrimNick <-TRIM_MAX) TrimNick =-TRIM_MAX; |
1286 | if(TrimNick > TRIM_MAX) TrimNick = TRIM_MAX; else if(TrimNick <-TRIM_MAX) TrimNick =-TRIM_MAX; |
1262 | if(TrimRoll > TRIM_MAX) TrimRoll = TRIM_MAX; else if(TrimRoll <-TRIM_MAX) TrimRoll =-TRIM_MAX; |
1287 | if(TrimRoll > TRIM_MAX) TrimRoll = TRIM_MAX; else if(TrimRoll <-TRIM_MAX) TrimRoll =-TRIM_MAX; |
1263 | 1288 | ||
1264 | MesswertNick = IntegralNickMalFaktor + (long)((long)MesswertNick * GyroFaktor + (long)TrimNick * 128L) / (256L / STICK_GAIN); |
1289 | MesswertNick = IntegralNickMalFaktor + (long)((long)MesswertNick * GyroFaktor + (long)TrimNick * 128L) / (256L / STICK_GAIN); |
1265 | MesswertRoll = IntegralRollMalFaktor + (long)((long)MesswertRoll * GyroFaktor + (long)TrimRoll * 128L) / (256L / STICK_GAIN); |
1290 | MesswertRoll = IntegralRollMalFaktor + (long)((long)MesswertRoll * GyroFaktor + (long)TrimRoll * 128L) / (256L / STICK_GAIN); |
1266 | MesswertGier = (long)(MesswertGier * 2 * (long)GyroFaktorGier) / (256L / STICK_GAIN) + (long)(Integral_Gier * IntegralFaktorGier) / (2 * (44000 / STICK_GAIN)); |
1291 | MesswertGier = (long)(MesswertGier * 2 * (long)GyroFaktorGier) / (256L / STICK_GAIN) + (long)(Integral_Gier * IntegralFaktorGier) / (2 * (44000 / STICK_GAIN)); |
1267 | 1292 | ||
1268 | // Maximalwerte abfangen |
1293 | // Maximalwerte abfangen |
1269 | // #define MAX_SENSOR (4096*STICK_GAIN) |
1294 | // #define MAX_SENSOR (4096*STICK_GAIN) |
1270 | #define MAX_SENSOR (4096) |
1295 | #define MAX_SENSOR (4096) |
1271 | if(MesswertNick > MAX_SENSOR) MesswertNick = MAX_SENSOR; |
1296 | if(MesswertNick > MAX_SENSOR) MesswertNick = MAX_SENSOR; |
1272 | if(MesswertNick < -MAX_SENSOR) MesswertNick = -MAX_SENSOR; |
1297 | if(MesswertNick < -MAX_SENSOR) MesswertNick = -MAX_SENSOR; |
1273 | if(MesswertRoll > MAX_SENSOR) MesswertRoll = MAX_SENSOR; |
1298 | if(MesswertRoll > MAX_SENSOR) MesswertRoll = MAX_SENSOR; |
1274 | if(MesswertRoll < -MAX_SENSOR) MesswertRoll = -MAX_SENSOR; |
1299 | if(MesswertRoll < -MAX_SENSOR) MesswertRoll = -MAX_SENSOR; |
1275 | if(MesswertGier > MAX_SENSOR) MesswertGier = MAX_SENSOR; |
1300 | if(MesswertGier > MAX_SENSOR) MesswertGier = MAX_SENSOR; |
1276 | if(MesswertGier < -MAX_SENSOR) MesswertGier = -MAX_SENSOR; |
1301 | if(MesswertGier < -MAX_SENSOR) MesswertGier = -MAX_SENSOR; |
1277 | 1302 | ||
1278 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1303 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1279 | // Höhenregelung |
1304 | // Höhenregelung |
1280 | // Die Höhenregelung schwächt lediglich das Gas ab, erhöht es allerdings nicht |
1305 | // Die Höhenregelung schwächt lediglich das Gas ab, erhöht es allerdings nicht |
1281 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1306 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1282 | if(UBat > BattLowVoltageWarning) GasMischanteil = ((unsigned int)GasMischanteil * BattLowVoltageWarning) / UBat; // Gas auf das aktuelle Spannungvieveau beziehen |
1307 | if(UBat > BattLowVoltageWarning) GasMischanteil = ((unsigned int)GasMischanteil * BattLowVoltageWarning) / UBat; // Gas auf das aktuelle Spannungvieveau beziehen |
1283 | GasMischanteil *= STICK_GAIN; |
1308 | GasMischanteil *= STICK_GAIN; |
1284 | // if height control is activated |
1309 | // if height control is activated |
1285 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG) && !(Looping_Roll || Looping_Nick)) // Höhenregelung |
1310 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG) && !(Looping_Roll || Looping_Nick)) // Höhenregelung |
1286 | { |
1311 | { |
1287 | #define HOVER_GAS_AVERAGE 16384L // 16384 * 2ms = 32s averaging |
1312 | #define HOVER_GAS_AVERAGE 16384L // 16384 * 2ms = 32s averaging |
1288 | #define HC_GAS_AVERAGE 4 // 4 * 2ms= 8ms averaging |
1313 | #define HC_GAS_AVERAGE 4 // 4 * 2ms= 8ms averaging |
1289 | 1314 | ||
1290 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
1315 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
1291 | #define OPA_OFFSET_STEP 15 |
1316 | #define OPA_OFFSET_STEP 15 |
1292 | #else |
1317 | #else |
1293 | #define OPA_OFFSET_STEP 10 |
1318 | #define OPA_OFFSET_STEP 10 |
1294 | #endif |
1319 | #endif |
1295 | int HCGas, HeightDeviation = 0,GasReduction = 0; |
1320 | int HCGas, HeightDeviation = 0,GasReduction = 0; |
1296 | static int HeightTrimming = 0; // rate for change of height setpoint |
1321 | static int HeightTrimming = 0; // rate for change of height setpoint |
1297 | static int FilterHCGas = 0; |
1322 | static int FilterHCGas = 0; |
1298 | static int StickGasHover = 120, HoverGasMin = 0, HoverGasMax = 1023; |
1323 | static int StickGasHover = 120, HoverGasMin = 0, HoverGasMax = 1023; |
1299 | static unsigned long HoverGasFilter = 0; |
1324 | static unsigned long HoverGasFilter = 0; |
1300 | static unsigned char delay = 100, BaroAtUpperLimit = 0, BaroAtLowerLimit = 0; |
1325 | static unsigned char delay = 100, BaroAtUpperLimit = 0, BaroAtLowerLimit = 0; |
1301 | int CosAttitude; // for projection of hoover gas |
1326 | int CosAttitude; // for projection of hoover gas |
1302 | 1327 | ||
1303 | // get the current hooverpoint |
1328 | // get the current hooverpoint |
1304 | DebugOut.Analog[21] = HoverGas; |
1329 | DebugOut.Analog[21] = HoverGas; |
1305 | 1330 | ||
1306 | // Expand the measurement |
1331 | // Expand the measurement |
1307 | // measurement of air pressure close to upper limit and no overflow in correction of the new OCR0A value occurs |
1332 | // measurement of air pressure close to upper limit and no overflow in correction of the new OCR0A value occurs |
1308 | if(!BaroExpandActive) |
1333 | if(!BaroExpandActive) |
1309 | { |
1334 | { |
1310 | if(MessLuftdruck > 920) |
1335 | if(MessLuftdruck > 920) |
1311 | { // increase offset |
1336 | { // increase offset |
1312 | if(OCR0A < (255 - OPA_OFFSET_STEP)) |
1337 | if(OCR0A < (255 - OPA_OFFSET_STEP)) |
1313 | { |
1338 | { |
1314 | ExpandBaro -= 1; |
1339 | ExpandBaro -= 1; |
1315 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // increase offset to shift ADC down |
1340 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // increase offset to shift ADC down |
1316 | beeptime = 300; |
1341 | beeptime = 300; |
1317 | BaroExpandActive = 350; |
1342 | BaroExpandActive = 350; |
1318 | } |
1343 | } |
1319 | else |
1344 | else |
1320 | { |
1345 | { |
1321 | BaroAtLowerLimit = 1; |
1346 | BaroAtLowerLimit = 1; |
1322 | } |
1347 | } |
1323 | } |
1348 | } |
1324 | // measurement of air pressure close to lower limit and |
1349 | // measurement of air pressure close to lower limit and |
1325 | else |
1350 | else |
1326 | if(MessLuftdruck < 100) |
1351 | if(MessLuftdruck < 100) |
1327 | { // decrease offset |
1352 | { // decrease offset |
1328 | if(OCR0A > OPA_OFFSET_STEP) |
1353 | if(OCR0A > OPA_OFFSET_STEP) |
1329 | { |
1354 | { |
1330 | ExpandBaro += 1; |
1355 | ExpandBaro += 1; |
1331 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // decrease offset to shift ADC up |
1356 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // decrease offset to shift ADC up |
1332 | beeptime = 300; |
1357 | beeptime = 300; |
1333 | BaroExpandActive = 350; |
1358 | BaroExpandActive = 350; |
1334 | } |
1359 | } |
1335 | else |
1360 | else |
1336 | { |
1361 | { |
1337 | BaroAtUpperLimit = 1; |
1362 | BaroAtUpperLimit = 1; |
1338 | } |
1363 | } |
1339 | } |
1364 | } |
1340 | else |
1365 | else |
1341 | { |
1366 | { |
1342 | BaroAtUpperLimit = 0; |
1367 | BaroAtUpperLimit = 0; |
1343 | BaroAtLowerLimit = 0; |
1368 | BaroAtLowerLimit = 0; |
1344 | } |
1369 | } |
1345 | } |
1370 | } |
1346 | else // delay, because of expanding the Baro-Range |
1371 | else // delay, because of expanding the Baro-Range |
1347 | { |
1372 | { |
1348 | // now clear the D-values |
1373 | // now clear the D-values |
1349 | SummenHoehe = HoehenWert * SM_FILTER; |
1374 | SummenHoehe = HoehenWert * SM_FILTER; |
1350 | VarioMeter = 0; |
1375 | VarioMeter = 0; |
1351 | BaroExpandActive--; |
1376 | BaroExpandActive--; |
1352 | } |
1377 | } |
1353 | 1378 | ||
1354 | // if height control is activated by an rc channel |
1379 | // if height control is activated by an rc channel |
1355 | if(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER) // Regler wird über Schalter gesteuert |
1380 | if(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER) // Regler wird über Schalter gesteuert |
1356 | { // check if parameter is less than activation threshold |
1381 | { // check if parameter is less than activation threshold |
1357 | if(Parameter_MaxHoehe < 50) // for 3 or 2-state switch height control is disabled in lowest position |
1382 | if(Parameter_MaxHoehe < 50) // for 3 or 2-state switch height control is disabled in lowest position |
1358 | { //height control not active |
1383 | { //height control not active |
1359 | if(!delay--) |
1384 | if(!delay--) |
1360 | { |
1385 | { |
1361 | HoehenReglerAktiv = 0; // disable height control |
1386 | HoehenReglerAktiv = 0; // disable height control |
1362 | SollHoehe = HoehenWert; // update SetPoint with current reading |
1387 | SollHoehe = HoehenWert; // update SetPoint with current reading |
1363 | delay = 1; |
1388 | delay = 1; |
1364 | } |
1389 | } |
1365 | } |
1390 | } |
1366 | else |
1391 | else |
1367 | { //height control is activated |
1392 | { //height control is activated |
1368 | HoehenReglerAktiv = 1; // enable height control |
1393 | HoehenReglerAktiv = 1; // enable height control |
1369 | delay = 200; |
1394 | delay = 200; |
1370 | } |
1395 | } |
1371 | } |
1396 | } |
1372 | else // no switchable height control |
1397 | else // no switchable height control |
1373 | { |
1398 | { |
1374 | SollHoehe = ((int16_t) ExternHoehenValue + (int16_t) Parameter_MaxHoehe) * (int)EE_Parameter.Hoehe_Verstaerkung; |
1399 | SollHoehe = ((int16_t) ExternHoehenValue + (int16_t) Parameter_MaxHoehe) * (int)EE_Parameter.Hoehe_Verstaerkung; |
1375 | HoehenReglerAktiv = 1; |
1400 | HoehenReglerAktiv = 1; |
1376 | } |
1401 | } |
1377 | 1402 | ||
1378 | // calculate cos of nick and roll angle used for projection of the vertical hoover gas |
1403 | // calculate cos of nick and roll angle used for projection of the vertical hoover gas |
1379 | tmp_int = (int)(IntegralNick/GIER_GRAD_FAKTOR); // nick angle in deg |
1404 | tmp_int = (int)(IntegralNick/GIER_GRAD_FAKTOR); // nick angle in deg |
1380 | tmp_int2 = (int)(IntegralRoll/GIER_GRAD_FAKTOR); // roll angle in deg |
1405 | tmp_int2 = (int)(IntegralRoll/GIER_GRAD_FAKTOR); // roll angle in deg |
1381 | CosAttitude = (int16_t)ihypot(tmp_int, tmp_int2); // phytagoras gives effective attitude angle in deg |
1406 | CosAttitude = (int16_t)ihypot(tmp_int, tmp_int2); // phytagoras gives effective attitude angle in deg |
1382 | LIMIT_MAX(CosAttitude, 60); // limit effective attitude angle |
1407 | LIMIT_MAX(CosAttitude, 60); // limit effective attitude angle |
1383 | CosAttitude = c_cos_8192(CosAttitude); // cos of actual attitude |
1408 | CosAttitude = c_cos_8192(CosAttitude); // cos of actual attitude |
1384 | VarioCharacter = ' '; |
1409 | VarioCharacter = ' '; |
1385 | if(HoehenReglerAktiv && !(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
1410 | if(HoehenReglerAktiv && !(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
1386 | { |
1411 | { |
1387 | #define HEIGHT_CONTROL_STICKTHRESHOLD 15 |
1412 | #define HEIGHT_CONTROL_STICKTHRESHOLD 15 |
1388 | // Holger original version |
1413 | // Holger original version |
1389 | // start of height control algorithm |
1414 | // start of height control algorithm |
1390 | // the height control is only an attenuation of the actual gas stick. |
1415 | // the height control is only an attenuation of the actual gas stick. |
1391 | // I.e. it will work only if the gas stick is higher than the hover gas |
1416 | // I.e. it will work only if the gas stick is higher than the hover gas |
1392 | // and the hover height will be allways larger than height setpoint. |
1417 | // and the hover height will be allways larger than height setpoint. |
1393 | if((EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) || !(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER)) // Regler wird über Schalter gesteuert) |
1418 | if((EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) || !(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER)) // Regler wird über Schalter gesteuert) |
1394 | { // old version |
1419 | { // old version |
1395 | HCGas = GasMischanteil; // take current stick gas as neutral point for the height control |
1420 | HCGas = GasMischanteil; // take current stick gas as neutral point for the height control |
1396 | HeightTrimming = 0; |
1421 | HeightTrimming = 0; |
1397 | // set both flags to indicate no vario mode |
1422 | // set both flags to indicate no vario mode |
1398 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
1423 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
1399 | } |
1424 | } |
1400 | else |
1425 | else |
1401 | { |
1426 | { |
1402 | // alternative height control |
1427 | // alternative height control |
1403 | // PD-Control with respect to hoover point |
1428 | // PD-Control with respect to hoover point |
1404 | // the thrust loss out of horizontal attitude is compensated |
1429 | // the thrust loss out of horizontal attitude is compensated |
1405 | // the setpoint will be fine adjusted with the gas stick position |
1430 | // the setpoint will be fine adjusted with the gas stick position |
1406 | if(FC_StatusFlags & FC_STATUS_FLY) // trim setpoint only when flying |
1431 | if(FC_StatusFlags & FC_STATUS_FLY) // trim setpoint only when flying |
1407 | { // gas stick is above hoover point |
1432 | { // gas stick is above hoover point |
1408 | if(StickGas > (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtUpperLimit) |
1433 | if(StickGas > (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtUpperLimit) |
1409 | { |
1434 | { |
1410 | if(FC_StatusFlags & FC_STATUS_VARIO_TRIM_DOWN) |
1435 | if(FC_StatusFlags & FC_STATUS_VARIO_TRIM_DOWN) |
1411 | { |
1436 | { |
1412 | FC_StatusFlags &= ~FC_STATUS_VARIO_TRIM_DOWN; |
1437 | FC_StatusFlags &= ~FC_STATUS_VARIO_TRIM_DOWN; |
1413 | SollHoehe = HoehenWert; // update setpoint to current heigth |
1438 | SollHoehe = HoehenWert; // update setpoint to current heigth |
1414 | } |
1439 | } |
1415 | FC_StatusFlags |= FC_STATUS_VARIO_TRIM_UP; |
1440 | FC_StatusFlags |= FC_STATUS_VARIO_TRIM_UP; |
1416 | HeightTrimming += abs(StickGas - (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD)); |
1441 | HeightTrimming += abs(StickGas - (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD)); |
1417 | VarioCharacter = '+'; |
1442 | VarioCharacter = '+'; |
1418 | } // gas stick is below hoover point |
1443 | } // gas stick is below hoover point |
1419 | else if(StickGas < (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtLowerLimit ) |
1444 | else if(StickGas < (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtLowerLimit ) |
1420 | { |
1445 | { |
1421 | if(FC_StatusFlags & FC_STATUS_VARIO_TRIM_UP) |
1446 | if(FC_StatusFlags & FC_STATUS_VARIO_TRIM_UP) |
1422 | { |
1447 | { |
1423 | FC_StatusFlags &= ~FC_STATUS_VARIO_TRIM_UP; |
1448 | FC_StatusFlags &= ~FC_STATUS_VARIO_TRIM_UP; |
1424 | SollHoehe = HoehenWert; // update setpoint to current heigth |
1449 | SollHoehe = HoehenWert; // update setpoint to current heigth |
1425 | } |
1450 | } |
1426 | FC_StatusFlags |= FC_STATUS_VARIO_TRIM_DOWN; |
1451 | FC_StatusFlags |= FC_STATUS_VARIO_TRIM_DOWN; |
1427 | HeightTrimming -= abs(StickGas - (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD)); |
1452 | HeightTrimming -= abs(StickGas - (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD)); |
1428 | VarioCharacter = '-'; |
1453 | VarioCharacter = '-'; |
1429 | } |
1454 | } |
1430 | else // Gas Stick in Hover Range |
1455 | else // Gas Stick in Hover Range |
1431 | { |
1456 | { |
1432 | if(FC_StatusFlags & (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN)) |
1457 | if(FC_StatusFlags & (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN)) |
1433 | { |
1458 | { |
1434 | FC_StatusFlags &= ~(FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
1459 | FC_StatusFlags &= ~(FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
1435 | HeightTrimming = 0; |
1460 | HeightTrimming = 0; |
1436 | SollHoehe = HoehenWert; // update setpoint to current height |
1461 | SollHoehe = HoehenWert; // update setpoint to current height |
1437 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 500; |
1462 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 500; |
1438 | if(!StartTrigger && HoehenWert > 50) |
1463 | if(!StartTrigger && HoehenWert > 50) |
1439 | { |
1464 | { |
1440 | StartTrigger = 1; |
1465 | StartTrigger = 1; |
1441 | } |
1466 | } |
1442 | } |
1467 | } |
1443 | VarioCharacter = '='; |
1468 | VarioCharacter = '='; |
1444 | } |
1469 | } |
1445 | // Trim height set point |
1470 | // Trim height set point |
1446 | if(abs(HeightTrimming) > 512) |
1471 | if(abs(HeightTrimming) > 512) |
1447 | { |
1472 | { |
1448 | SollHoehe += (HeightTrimming * EE_Parameter.Hoehe_Verstaerkung)/(5 * 512 / 2); // move setpoint |
1473 | SollHoehe += (HeightTrimming * EE_Parameter.Hoehe_Verstaerkung)/(5 * 512 / 2); // move setpoint |
1449 | HeightTrimming = 0; |
1474 | HeightTrimming = 0; |
1450 | LIMIT_MIN_MAX(SollHoehe, (HoehenWert-1024), (HoehenWert+1024)); // max. 10m Unterschied |
1475 | LIMIT_MIN_MAX(SollHoehe, (HoehenWert-1024), (HoehenWert+1024)); // max. 10m Unterschied |
1451 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 100; |
1476 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 100; |
1452 | //update hoover gas stick value when setpoint is shifted |
1477 | //update hoover gas stick value when setpoint is shifted |
1453 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
1478 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
1454 | { |
1479 | { |
1455 | StickGasHover = HoverGas/STICK_GAIN; //rescale back to stick value |
1480 | StickGasHover = HoverGas/STICK_GAIN; //rescale back to stick value |
1456 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
1481 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
1457 | if(StickGasHover < 70) StickGasHover = 70; |
1482 | if(StickGasHover < 70) StickGasHover = 70; |
1458 | else if(StickGasHover > 150) StickGasHover = 150; |
1483 | else if(StickGasHover > 150) StickGasHover = 150; |
1459 | } |
1484 | } |
1460 | } |
1485 | } |
1461 | if(BaroExpandActive) SollHoehe = HoehenWert; // update setpoint to current altitude if Expanding is active |
1486 | if(BaroExpandActive) SollHoehe = HoehenWert; // update setpoint to current altitude if Expanding is active |
1462 | } //if FCFlags & MKFCFLAG_FLY |
1487 | } //if FCFlags & MKFCFLAG_FLY |
1463 | else |
1488 | else |
1464 | { |
1489 | { |
1465 | SollHoehe = HoehenWert - 400; |
1490 | SollHoehe = HoehenWert - 400; |
1466 | if(EE_Parameter.Hoehe_StickNeutralPoint) StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
1491 | if(EE_Parameter.Hoehe_StickNeutralPoint) StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
1467 | else StickGasHover = 120; |
1492 | else StickGasHover = 120; |
1468 | HoverGas = GasMischanteil; |
1493 | HoverGas = GasMischanteil; |
1469 | } |
1494 | } |
1470 | HCGas = HoverGas; // take hover gas (neutral point) |
1495 | HCGas = HoverGas; // take hover gas (neutral point) |
1471 | } |
1496 | } |
1472 | if(HoehenWert > SollHoehe || !(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT)) |
1497 | if(HoehenWert > SollHoehe || !(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT)) |
1473 | { |
1498 | { |
1474 | // from this point the Heigth Control Algorithm is identical for both versions |
1499 | // from this point the Heigth Control Algorithm is identical for both versions |
1475 | if(BaroExpandActive) // baro range expanding active |
1500 | if(BaroExpandActive) // baro range expanding active |
1476 | { |
1501 | { |
1477 | HCGas = HoverGas; // hover while expanding baro adc range |
1502 | HCGas = HoverGas; // hover while expanding baro adc range |
1478 | HeightDeviation = 0; |
1503 | HeightDeviation = 0; |
1479 | } // EOF // baro range expanding active |
1504 | } // EOF // baro range expanding active |
1480 | else // valid data from air pressure sensor |
1505 | else // valid data from air pressure sensor |
1481 | { |
1506 | { |
1482 | // ------------------------- P-Part ---------------------------- |
1507 | // ------------------------- P-Part ---------------------------- |
1483 | tmp_long = (HoehenWert - SollHoehe); // positive when too high |
1508 | tmp_long = (HoehenWert - SollHoehe); // positive when too high |
1484 | LIMIT_MIN_MAX(tmp_long, -32767L, 32767L); // avoid overflov when casting to int16_t |
1509 | LIMIT_MIN_MAX(tmp_long, -32767L, 32767L); // avoid overflov when casting to int16_t |
1485 | HeightDeviation = (int)(tmp_long); // positive when too high |
1510 | HeightDeviation = (int)(tmp_long); // positive when too high |
1486 | tmp_long = (tmp_long * (long)Parameter_Hoehe_P) / 32L; // p-part |
1511 | tmp_long = (tmp_long * (long)Parameter_Hoehe_P) / 32L; // p-part |
1487 | LIMIT_MIN_MAX(tmp_long, -127 * STICK_GAIN, 256 * STICK_GAIN); // more than the full range makes no sense |
1512 | LIMIT_MIN_MAX(tmp_long, -127 * STICK_GAIN, 256 * STICK_GAIN); // more than the full range makes no sense |
1488 | GasReduction = tmp_long; |
1513 | GasReduction = tmp_long; |
1489 | // ------------------------- D-Part 1: Vario Meter ---------------------------- |
1514 | // ------------------------- D-Part 1: Vario Meter ---------------------------- |
1490 | tmp_int = VarioMeter / 8; |
1515 | tmp_int = VarioMeter / 8; |
1491 | LIMIT_MIN_MAX(tmp_int, -127, 128); |
1516 | LIMIT_MIN_MAX(tmp_int, -127, 128); |
1492 | tmp_int = (tmp_int * (long)Parameter_Luftdruck_D) / 4L; // scale to d-gain parameter |
1517 | tmp_int = (tmp_int * (long)Parameter_Luftdruck_D) / 4L; // scale to d-gain parameter |
1493 | LIMIT_MIN_MAX(tmp_int,-64 * STICK_GAIN, 64 * STICK_GAIN); |
1518 | LIMIT_MIN_MAX(tmp_int,-64 * STICK_GAIN, 64 * STICK_GAIN); |
1494 | if(FC_StatusFlags & (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN)) tmp_int /= 4; // reduce d-part while trimming setpoint |
1519 | if(FC_StatusFlags & (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN)) tmp_int /= 4; // reduce d-part while trimming setpoint |
1495 | else |
1520 | else |
1496 | if(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) tmp_int /= 8; // reduce d-part in "Deckel" mode |
1521 | if(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) tmp_int /= 8; // reduce d-part in "Deckel" mode |
1497 | GasReduction += tmp_int; |
1522 | GasReduction += tmp_int; |
1498 | } // EOF no baro range expanding |
1523 | } // EOF no baro range expanding |
1499 | // ------------------------ D-Part 2: ACC-Z Integral ------------------------ |
1524 | // ------------------------ D-Part 2: ACC-Z Integral ------------------------ |
1500 | if(Parameter_Hoehe_ACC_Wirkung) |
1525 | if(Parameter_Hoehe_ACC_Wirkung) |
1501 | { |
1526 | { |
1502 | tmp_long = ((Mess_Integral_Hoch / 128L) * (int32_t) Parameter_Hoehe_ACC_Wirkung) / (128L / STICK_GAIN); |
1527 | tmp_long = ((Mess_Integral_Hoch / 128L) * (int32_t) Parameter_Hoehe_ACC_Wirkung) / (128L / STICK_GAIN); |
1503 | LIMIT_MIN_MAX(tmp_long, -32 * STICK_GAIN, 64 * STICK_GAIN); |
1528 | LIMIT_MIN_MAX(tmp_long, -32 * STICK_GAIN, 64 * STICK_GAIN); |
1504 | GasReduction += tmp_long; |
1529 | GasReduction += tmp_long; |
1505 | } |
1530 | } |
1506 | // ------------------------ D-Part 3: GpsZ ---------------------------------- |
1531 | // ------------------------ D-Part 3: GpsZ ---------------------------------- |
1507 | tmp_int = (Parameter_Hoehe_GPS_Z * (int)FromNaviCtrl_Value.GpsZ)/128L; |
1532 | tmp_int = (Parameter_Hoehe_GPS_Z * (int)FromNaviCtrl_Value.GpsZ)/128L; |
1508 | LIMIT_MIN_MAX(tmp_int, -32 * STICK_GAIN, 64 * STICK_GAIN); |
1533 | LIMIT_MIN_MAX(tmp_int, -32 * STICK_GAIN, 64 * STICK_GAIN); |
1509 | GasReduction += tmp_int; |
1534 | GasReduction += tmp_int; |
1510 | GasReduction = (long)((long)GasReduction * HoverGas) / 512; // scale to the gas value |
1535 | GasReduction = (long)((long)GasReduction * HoverGas) / 512; // scale to the gas value |
1511 | // ------------------------ ---------------------------------- |
1536 | // ------------------------ ---------------------------------- |
1512 | HCGas -= GasReduction; |
1537 | HCGas -= GasReduction; |
1513 | // limit deviation from hoover point within the target region |
1538 | // limit deviation from hoover point within the target region |
1514 | if(!HeightTrimming && HoverGas > 0) // height setpoint is not changed and hoover gas not zero |
1539 | if(!HeightTrimming && HoverGas > 0) // height setpoint is not changed and hoover gas not zero |
1515 | { |
1540 | { |
1516 | unsigned int tmp; |
1541 | unsigned int tmp; |
1517 | tmp = abs(HeightDeviation); |
1542 | tmp = abs(HeightDeviation); |
1518 | if(tmp <= 60) |
1543 | if(tmp <= 60) |
1519 | { |
1544 | { |
1520 | LIMIT_MIN_MAX(HCGas, HoverGasMin, HoverGasMax); // limit gas around the hoover point |
1545 | LIMIT_MIN_MAX(HCGas, HoverGasMin, HoverGasMax); // limit gas around the hoover point |
1521 | } |
1546 | } |
1522 | else |
1547 | else |
1523 | { |
1548 | { |
1524 | tmp = (tmp - 60) / 32; |
1549 | tmp = (tmp - 60) / 32; |
1525 | if(tmp > 15) tmp = 15; |
1550 | if(tmp > 15) tmp = 15; |
1526 | if(HeightDeviation > 0) |
1551 | if(HeightDeviation > 0) |
1527 | { |
1552 | { |
1528 | tmp = (HoverGasMin * (16 - tmp)) / 16; |
1553 | tmp = (HoverGasMin * (16 - tmp)) / 16; |
1529 | LIMIT_MIN_MAX(HCGas, tmp, HoverGasMax); // limit gas around the hoover point |
1554 | LIMIT_MIN_MAX(HCGas, tmp, HoverGasMax); // limit gas around the hoover point |
1530 | } |
1555 | } |
1531 | else |
1556 | else |
1532 | { |
1557 | { |
1533 | tmp = (HoverGasMax * (tmp + 16)) / 16; |
1558 | tmp = (HoverGasMax * (tmp + 16)) / 16; |
1534 | LIMIT_MIN_MAX(HCGas, HoverGasMin, tmp); // limit gas around the hoover point |
1559 | LIMIT_MIN_MAX(HCGas, HoverGasMin, tmp); // limit gas around the hoover point |
1535 | } |
1560 | } |
1536 | } |
1561 | } |
1537 | } |
1562 | } |
1538 | // strech control output by inverse attitude projection 1/cos |
1563 | // strech control output by inverse attitude projection 1/cos |
1539 | // + 1/cos(angle) ++++++++++++++++++++++++++ |
1564 | // + 1/cos(angle) ++++++++++++++++++++++++++ |
1540 | tmp_long2 = (int32_t)HCGas; |
1565 | tmp_long2 = (int32_t)HCGas; |
1541 | tmp_long2 *= 8192L; |
1566 | tmp_long2 *= 8192L; |
1542 | tmp_long2 /= CosAttitude; |
1567 | tmp_long2 /= CosAttitude; |
1543 | HCGas = (int16_t)tmp_long2; |
1568 | HCGas = (int16_t)tmp_long2; |
1544 | // update height control gas averaging |
1569 | // update height control gas averaging |
1545 | FilterHCGas = (FilterHCGas * (HC_GAS_AVERAGE - 1) + HCGas) / HC_GAS_AVERAGE; |
1570 | FilterHCGas = (FilterHCGas * (HC_GAS_AVERAGE - 1) + HCGas) / HC_GAS_AVERAGE; |
1546 | // limit height control gas pd-control output |
1571 | // limit height control gas pd-control output |
1547 | LIMIT_MIN_MAX(FilterHCGas, EE_Parameter.Hoehe_MinGas * STICK_GAIN, (MAX_GAS - 20) * STICK_GAIN); |
1572 | LIMIT_MIN_MAX(FilterHCGas, EE_Parameter.Hoehe_MinGas * STICK_GAIN, (MAX_GAS - 20) * STICK_GAIN); |
1548 | // set GasMischanteil to HeightControlGasFilter |
1573 | // set GasMischanteil to HeightControlGasFilter |
1549 | if(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) |
1574 | if(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) |
1550 | { // old version |
1575 | { // old version |
1551 | LIMIT_MAX(FilterHCGas, GasMischanteil); // nicht mehr als Gas |
1576 | LIMIT_MAX(FilterHCGas, GasMischanteil); // nicht mehr als Gas |
1552 | GasMischanteil = FilterHCGas; |
1577 | GasMischanteil = FilterHCGas; |
1553 | } |
1578 | } |
1554 | else GasMischanteil = FilterHCGas + (GasMischanteil - HoverGas) / 4; // only in Vario-Mode |
1579 | else GasMischanteil = FilterHCGas + (GasMischanteil - HoverGas) / 4; // only in Vario-Mode |
1555 | } |
1580 | } |
1556 | }// EOF height control active |
1581 | }// EOF height control active |
1557 | else // HC not active |
1582 | else // HC not active |
1558 | { |
1583 | { |
1559 | //update hoover gas stick value when HC is not active |
1584 | //update hoover gas stick value when HC is not active |
1560 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
1585 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
1561 | { |
1586 | { |
1562 | StickGasHover = HoverGas/STICK_GAIN; // rescale back to stick value |
1587 | StickGasHover = HoverGas/STICK_GAIN; // rescale back to stick value |
1563 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
1588 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
1564 | } |
1589 | } |
1565 | else StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
1590 | else StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
1566 | LIMIT_MIN_MAX(StickGasHover, 70, 150); // reserve some range for trim up and down |
1591 | LIMIT_MIN_MAX(StickGasHover, 70, 150); // reserve some range for trim up and down |
1567 | FilterHCGas = GasMischanteil; |
1592 | FilterHCGas = GasMischanteil; |
1568 | // set both flags to indicate no vario mode |
1593 | // set both flags to indicate no vario mode |
1569 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
1594 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
1570 | } |
1595 | } |
1571 | 1596 | ||
1572 | // Hover gas estimation by averaging gas control output on small z-velocities |
1597 | // Hover gas estimation by averaging gas control output on small z-velocities |
1573 | // this is done only if height contol option is selected in global config and aircraft is flying |
1598 | // this is done only if height contol option is selected in global config and aircraft is flying |
1574 | if((FC_StatusFlags & FC_STATUS_FLY))// && !(FC_SatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
1599 | if((FC_StatusFlags & FC_STATUS_FLY))// && !(FC_SatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
1575 | { |
1600 | { |
1576 | if(HoverGasFilter == 0 || StartTrigger == 1) HoverGasFilter = HOVER_GAS_AVERAGE * (unsigned long)(GasMischanteil); // init estimation |
1601 | if(HoverGasFilter == 0 || StartTrigger == 1) HoverGasFilter = HOVER_GAS_AVERAGE * (unsigned long)(GasMischanteil); // init estimation |
1577 | if(StartTrigger == 1) StartTrigger = 2; |
1602 | if(StartTrigger == 1) StartTrigger = 2; |
1578 | tmp_long2 = (int32_t)GasMischanteil; // take current thrust |
1603 | tmp_long2 = (int32_t)GasMischanteil; // take current thrust |
1579 | tmp_long2 *= CosAttitude; // apply attitude projection |
1604 | tmp_long2 *= CosAttitude; // apply attitude projection |
1580 | tmp_long2 /= 8192; |
1605 | tmp_long2 /= 8192; |
1581 | // average vertical projected thrust |
1606 | // average vertical projected thrust |
1582 | if(modell_fliegt < 4000) // the first 8 seconds |
1607 | if(modell_fliegt < 4000) // the first 8 seconds |
1583 | { // reduce the time constant of averaging by factor of 4 to get much faster a stable value |
1608 | { // reduce the time constant of averaging by factor of 4 to get much faster a stable value |
1584 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/16L); |
1609 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/16L); |
1585 | HoverGasFilter += 16L * tmp_long2; |
1610 | HoverGasFilter += 16L * tmp_long2; |
1586 | } |
1611 | } |
1587 | if(modell_fliegt < 8000) // the first 16 seconds |
1612 | if(modell_fliegt < 8000) // the first 16 seconds |
1588 | { // reduce the time constant of averaging by factor of 2 to get much faster a stable value |
1613 | { // reduce the time constant of averaging by factor of 2 to get much faster a stable value |
1589 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/4L); |
1614 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/4L); |
1590 | HoverGasFilter += 4L * tmp_long2; |
1615 | HoverGasFilter += 4L * tmp_long2; |
1591 | } |
1616 | } |
1592 | else //later |
1617 | else //later |
1593 | if(abs(VarioMeter) < 100) // only on small vertical speed |
1618 | if(abs(VarioMeter) < 100) // only on small vertical speed |
1594 | { |
1619 | { |
1595 | HoverGasFilter -= HoverGasFilter/HOVER_GAS_AVERAGE; |
1620 | HoverGasFilter -= HoverGasFilter/HOVER_GAS_AVERAGE; |
1596 | HoverGasFilter += tmp_long2; |
1621 | HoverGasFilter += tmp_long2; |
1597 | } |
1622 | } |
1598 | HoverGas = (int16_t)(HoverGasFilter/HOVER_GAS_AVERAGE); |
1623 | HoverGas = (int16_t)(HoverGasFilter/HOVER_GAS_AVERAGE); |
1599 | if(EE_Parameter.Hoehe_HoverBand) |
1624 | if(EE_Parameter.Hoehe_HoverBand) |
1600 | { |
1625 | { |
1601 | int16_t band; |
1626 | int16_t band; |
1602 | band = HoverGas / EE_Parameter.Hoehe_HoverBand; // the higher the parameter the smaller the range |
1627 | band = HoverGas / EE_Parameter.Hoehe_HoverBand; // the higher the parameter the smaller the range |
1603 | HoverGasMin = HoverGas - band; |
1628 | HoverGasMin = HoverGas - band; |
1604 | HoverGasMax = HoverGas + band; |
1629 | HoverGasMax = HoverGas + band; |
1605 | } |
1630 | } |
1606 | else |
1631 | else |
1607 | { // no limit |
1632 | { // no limit |
1608 | HoverGasMin = 0; |
1633 | HoverGasMin = 0; |
1609 | HoverGasMax = 1023; |
1634 | HoverGasMax = 1023; |
1610 | } |
1635 | } |
1611 | } |
1636 | } |
1612 | else |
1637 | else |
1613 | { |
1638 | { |
1614 | StartTrigger = 0; |
1639 | StartTrigger = 0; |
1615 | HoverGasFilter = 0; |
1640 | HoverGasFilter = 0; |
1616 | HoverGas = 0; |
1641 | HoverGas = 0; |
1617 | } |
1642 | } |
1618 | }// EOF ParamSet.GlobalConfig & CFG_HEIGHT_CONTROL |
1643 | }// EOF ParamSet.GlobalConfig & CFG_HEIGHT_CONTROL |
1619 | else |
1644 | else |
1620 | { |
1645 | { |
1621 | // set undefined state to indicate vario off |
1646 | // set undefined state to indicate vario off |
1622 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
1647 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
1623 | } // EOF no height control |
1648 | } // EOF no height control |
1624 | 1649 | ||
1625 | // limit gas to parameter setting |
1650 | // limit gas to parameter setting |
1626 | LIMIT_MIN(GasMischanteil, (MIN_GAS + 10) * STICK_GAIN); |
1651 | LIMIT_MIN(GasMischanteil, (MIN_GAS + 10) * STICK_GAIN); |
1627 | if(GasMischanteil > (MAX_GAS - 20) * STICK_GAIN) GasMischanteil = (MAX_GAS - 20) * STICK_GAIN; |
1652 | if(GasMischanteil > (MAX_GAS - 20) * STICK_GAIN) GasMischanteil = (MAX_GAS - 20) * STICK_GAIN; |
1628 | 1653 | ||
1629 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1654 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1630 | // all BL-Ctrl connected? |
1655 | // all BL-Ctrl connected? |
1631 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1656 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1632 | if(MissingMotor || Capacity.MinOfMaxPWM != 255) |
1657 | if(MissingMotor || Capacity.MinOfMaxPWM != 255) |
1633 | if(modell_fliegt > 1 && modell_fliegt < 50 && GasMischanteil > 0) |
1658 | if(modell_fliegt > 1 && modell_fliegt < 50 && GasMischanteil > 0) |
1634 | { |
1659 | { |
1635 | modell_fliegt = 1; |
1660 | modell_fliegt = 1; |
1636 | GasMischanteil = (MIN_GAS + 10) * STICK_GAIN; |
1661 | GasMischanteil = (MIN_GAS + 10) * STICK_GAIN; |
1637 | } |
1662 | } |
1638 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1663 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1639 | // + Mischer und PI-Regler |
1664 | // + Mischer und PI-Regler |
1640 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1665 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1641 | DebugOut.Analog[7] = GasMischanteil; |
1666 | DebugOut.Analog[7] = GasMischanteil; |
1642 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1667 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1643 | // Gier-Anteil |
1668 | // Gier-Anteil |
1644 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1669 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1645 | GierMischanteil = MesswertGier - sollGier * STICK_GAIN; // Regler für Gier |
1670 | GierMischanteil = MesswertGier - sollGier * STICK_GAIN; // Regler für Gier |
1646 | #define MIN_GIERGAS (40*STICK_GAIN) // unter diesem Gaswert trotzdem Gieren |
1671 | #define MIN_GIERGAS (40*STICK_GAIN) // unter diesem Gaswert trotzdem Gieren |
1647 | if(GasMischanteil > MIN_GIERGAS) |
1672 | if(GasMischanteil > MIN_GIERGAS) |
1648 | { |
1673 | { |
1649 | if(GierMischanteil > (GasMischanteil / 2)) GierMischanteil = GasMischanteil / 2; |
1674 | if(GierMischanteil > (GasMischanteil / 2)) GierMischanteil = GasMischanteil / 2; |
1650 | if(GierMischanteil < -(GasMischanteil / 2)) GierMischanteil = -(GasMischanteil / 2); |
1675 | if(GierMischanteil < -(GasMischanteil / 2)) GierMischanteil = -(GasMischanteil / 2); |
1651 | } |
1676 | } |
1652 | else |
1677 | else |
1653 | { |
1678 | { |
1654 | if(GierMischanteil > (MIN_GIERGAS / 2)) GierMischanteil = MIN_GIERGAS / 2; |
1679 | if(GierMischanteil > (MIN_GIERGAS / 2)) GierMischanteil = MIN_GIERGAS / 2; |
1655 | if(GierMischanteil < -(MIN_GIERGAS / 2)) GierMischanteil = -(MIN_GIERGAS / 2); |
1680 | if(GierMischanteil < -(MIN_GIERGAS / 2)) GierMischanteil = -(MIN_GIERGAS / 2); |
1656 | } |
1681 | } |
1657 | tmp_int = MAX_GAS*STICK_GAIN; |
1682 | tmp_int = MAX_GAS*STICK_GAIN; |
1658 | if(GierMischanteil > ((tmp_int - GasMischanteil))) GierMischanteil = ((tmp_int - GasMischanteil)); |
1683 | if(GierMischanteil > ((tmp_int - GasMischanteil))) GierMischanteil = ((tmp_int - GasMischanteil)); |
1659 | if(GierMischanteil < -((tmp_int - GasMischanteil))) GierMischanteil = -((tmp_int - GasMischanteil)); |
1684 | if(GierMischanteil < -((tmp_int - GasMischanteil))) GierMischanteil = -((tmp_int - GasMischanteil)); |
1660 | 1685 | ||
1661 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1686 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1662 | // Nick-Achse |
1687 | // Nick-Achse |
1663 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1688 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1664 | DiffNick = MesswertNick - StickNick; // Differenz bestimmen |
1689 | DiffNick = MesswertNick - StickNick; // Differenz bestimmen |
1665 | if(IntegralFaktor) SummeNick += IntegralNickMalFaktor - StickNick; // I-Anteil bei Winkelregelung |
1690 | if(IntegralFaktor) SummeNick += IntegralNickMalFaktor - StickNick; // I-Anteil bei Winkelregelung |
1666 | else SummeNick += DiffNick; // I-Anteil bei HH |
1691 | else SummeNick += DiffNick; // I-Anteil bei HH |
1667 | if(SummeNick > (STICK_GAIN * 16000L)) SummeNick = (STICK_GAIN * 16000L); |
1692 | if(SummeNick > (STICK_GAIN * 16000L)) SummeNick = (STICK_GAIN * 16000L); |
1668 | if(SummeNick < -(16000L * STICK_GAIN)) SummeNick = -(16000L * STICK_GAIN); |
1693 | if(SummeNick < -(16000L * STICK_GAIN)) SummeNick = -(16000L * STICK_GAIN); |
1669 | 1694 | ||
1670 | if(EE_Parameter.Gyro_Stability <= 8) pd_ergebnis_nick = (EE_Parameter.Gyro_Stability * DiffNick) / 8; // PI-Regler für Nick |
1695 | if(EE_Parameter.Gyro_Stability <= 8) pd_ergebnis_nick = (EE_Parameter.Gyro_Stability * DiffNick) / 8; // PI-Regler für Nick |
1671 | else pd_ergebnis_nick = ((EE_Parameter.Gyro_Stability / 2) * DiffNick) / 4; // Überlauf verhindern |
1696 | else pd_ergebnis_nick = ((EE_Parameter.Gyro_Stability / 2) * DiffNick) / 4; // Überlauf verhindern |
1672 | pd_ergebnis_nick += SummeNick / Ki; |
1697 | pd_ergebnis_nick += SummeNick / Ki; |
1673 | 1698 | ||
1674 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
1699 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
1675 | if(pd_ergebnis_nick > tmp_int) pd_ergebnis_nick = tmp_int; |
1700 | if(pd_ergebnis_nick > tmp_int) pd_ergebnis_nick = tmp_int; |
1676 | if(pd_ergebnis_nick < -tmp_int) pd_ergebnis_nick = -tmp_int; |
1701 | if(pd_ergebnis_nick < -tmp_int) pd_ergebnis_nick = -tmp_int; |
1677 | 1702 | ||
1678 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1703 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1679 | // Roll-Achse |
1704 | // Roll-Achse |
1680 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1705 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1681 | DiffRoll = MesswertRoll - StickRoll; // Differenz bestimmen |
1706 | DiffRoll = MesswertRoll - StickRoll; // Differenz bestimmen |
1682 | if(IntegralFaktor) SummeRoll += IntegralRollMalFaktor - StickRoll;// I-Anteil bei Winkelregelung |
1707 | if(IntegralFaktor) SummeRoll += IntegralRollMalFaktor - StickRoll;// I-Anteil bei Winkelregelung |
1683 | else SummeRoll += DiffRoll; // I-Anteil bei HH |
1708 | else SummeRoll += DiffRoll; // I-Anteil bei HH |
1684 | if(SummeRoll > (STICK_GAIN * 16000L)) SummeRoll = (STICK_GAIN * 16000L); |
1709 | if(SummeRoll > (STICK_GAIN * 16000L)) SummeRoll = (STICK_GAIN * 16000L); |
1685 | if(SummeRoll < -(16000L * STICK_GAIN)) SummeRoll = -(16000L * STICK_GAIN); |
1710 | if(SummeRoll < -(16000L * STICK_GAIN)) SummeRoll = -(16000L * STICK_GAIN); |
1686 | 1711 | ||
1687 | if(EE_Parameter.Gyro_Stability <= 8) pd_ergebnis_roll = (EE_Parameter.Gyro_Stability * DiffRoll) / 8; // PI-Regler für Roll |
1712 | if(EE_Parameter.Gyro_Stability <= 8) pd_ergebnis_roll = (EE_Parameter.Gyro_Stability * DiffRoll) / 8; // PI-Regler für Roll |
1688 | else pd_ergebnis_roll = ((EE_Parameter.Gyro_Stability / 2) * DiffRoll) / 4; // Überlauf verhindern |
1713 | else pd_ergebnis_roll = ((EE_Parameter.Gyro_Stability / 2) * DiffRoll) / 4; // Überlauf verhindern |
1689 | pd_ergebnis_roll += SummeRoll / Ki; |
1714 | pd_ergebnis_roll += SummeRoll / Ki; |
1690 | 1715 | ||
1691 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
1716 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
1692 | if(pd_ergebnis_roll > tmp_int) pd_ergebnis_roll = tmp_int; |
1717 | if(pd_ergebnis_roll > tmp_int) pd_ergebnis_roll = tmp_int; |
1693 | if(pd_ergebnis_roll < -tmp_int) pd_ergebnis_roll = -tmp_int; |
1718 | if(pd_ergebnis_roll < -tmp_int) pd_ergebnis_roll = -tmp_int; |
1694 | 1719 | ||
1695 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1720 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1696 | // Universal Mixer |
1721 | // Universal Mixer |
1697 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1722 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1698 | for(i=0; i<MAX_MOTORS; i++) |
1723 | for(i=0; i<MAX_MOTORS; i++) |
1699 | { |
1724 | { |
1700 | signed int tmp_int; |
1725 | signed int tmp_int; |
1701 | if(Mixer.Motor[i][0] > 0) |
1726 | if(Mixer.Motor[i][0] > 0) |
1702 | { |
1727 | { |
1703 | // Gas |
1728 | // Gas |
1704 | if(Mixer.Motor[i][0] == 64) tmp_int = GasMischanteil; else tmp_int = ((long)GasMischanteil * Mixer.Motor[i][0]) / 64L; |
1729 | if(Mixer.Motor[i][0] == 64) tmp_int = GasMischanteil; else tmp_int = ((long)GasMischanteil * Mixer.Motor[i][0]) / 64L; |
1705 | // Nick |
1730 | // Nick |
1706 | if(Mixer.Motor[i][1] == 64) tmp_int += pd_ergebnis_nick; |
1731 | if(Mixer.Motor[i][1] == 64) tmp_int += pd_ergebnis_nick; |
1707 | else if(Mixer.Motor[i][1] == -64) tmp_int -= pd_ergebnis_nick; |
1732 | else if(Mixer.Motor[i][1] == -64) tmp_int -= pd_ergebnis_nick; |
1708 | else tmp_int += ((long)pd_ergebnis_nick * Mixer.Motor[i][1]) / 64L; |
1733 | else tmp_int += ((long)pd_ergebnis_nick * Mixer.Motor[i][1]) / 64L; |
1709 | // Roll |
1734 | // Roll |
1710 | if(Mixer.Motor[i][2] == 64) tmp_int += pd_ergebnis_roll; |
1735 | if(Mixer.Motor[i][2] == 64) tmp_int += pd_ergebnis_roll; |
1711 | else if(Mixer.Motor[i][2] == -64) tmp_int -= pd_ergebnis_roll; |
1736 | else if(Mixer.Motor[i][2] == -64) tmp_int -= pd_ergebnis_roll; |
1712 | else tmp_int += ((long)pd_ergebnis_roll * Mixer.Motor[i][2]) / 64L; |
1737 | else tmp_int += ((long)pd_ergebnis_roll * Mixer.Motor[i][2]) / 64L; |
1713 | // Gier |
1738 | // Gier |
1714 | if(Mixer.Motor[i][3] == 64) tmp_int += GierMischanteil; |
1739 | if(Mixer.Motor[i][3] == 64) tmp_int += GierMischanteil; |
1715 | else if(Mixer.Motor[i][3] == -64) tmp_int -= GierMischanteil; |
1740 | else if(Mixer.Motor[i][3] == -64) tmp_int -= GierMischanteil; |
1716 | else tmp_int += ((long)GierMischanteil * Mixer.Motor[i][3]) / 64L; |
1741 | else tmp_int += ((long)GierMischanteil * Mixer.Motor[i][3]) / 64L; |
- | 1742 | ||
- | 1743 | ||
1717 | 1744 | /* //MartinW original Motorsmoothing |
|
1718 | if(tmp_int > tmp_motorwert[i]) tmp_int = (tmp_motorwert[i] + tmp_int) / 2; // MotorSmoothing |
1745 | if(tmp_int > tmp_motorwert[i]) tmp_int = (tmp_motorwert[i] + tmp_int) / 2; // MotorSmoothing |
- | 1746 | else tmp_int = 2 * tmp_int - tmp_motorwert[i]; // MotorSmoothing |
|
- | 1747 | */ |
|
- | 1748 | ||
- | 1749 | ||
- | 1750 | ||
- | 1751 | // MartinW; variable MS START |
|
- | 1752 | if(tmp_int > tmp_motorwert[i]) tmp_int = (tmp_motorwert[i] + tmp_int) / 2; // MotorSmoothing |
|
- | 1753 | // else tmp_int = 2 * tmp_int - tmp_motorwert[i]; // MotorSmoothing |
|
- | 1754 | // Arthur P: the original code allowed the motor value to drop to 0 or negative values |
|
- | 1755 | // straight off, i.e. could amplify an intended decrease excessively while upregulation |
|
- | 1756 | // is dampened. The modification would still allow immediate drop below intended value |
|
- | 1757 | // but would dampen this. This would still allow for airbraking of the prop to have effect |
|
- | 1758 | // but it might lead to less sudden excessive drops in rpm with only gradual recovery. |
|
- | 1759 | // 090807 Arthur P: Due to problems with uart.c which still refers to user parameter 1 and 2 and |
|
- | 1760 | // possible timing issues with the shutter interval load, removed the shutter interval functions |
|
- | 1761 | // and switched to use of userparam6 for the motor smoothing. |
|
- | 1762 | // 091114 Inserted modification into 0.76g source code. |
|
- | 1763 | // 20100804 Modified v.0.80d code where motorsmoothing is no longer a separate function. |
|
- | 1764 | // Downsmoothing either uses default v.0.7x+ 150% downstep (user para 7 == 0), |
|
- | 1765 | // 50% downstep (user para 7 == 1 or 2), or downsteps of x% (userpara7 ==): |
|
- | 1766 | // 66.6% (3), 75% (4), 80% (5), 90% (10), 95% (20), 97.5% (40), 98% (50), 99% (100). |
|
- | 1767 | else |
|
- | 1768 | { |
|
- | 1769 | if(Parameter_UserParam7 < 2) |
|
- | 1770 | { // Original function |
|
- | 1771 | tmp_int = 2 * tmp_int - tmp_motorwert[i]; |
|
- | 1772 | } |
|
- | 1773 | else |
|
- | 1774 | { |
|
- | 1775 | // If userpara7 >= 2 then allow >= 50% of the intended step down to rapidly reach the intended value. |
|
- | 1776 | tmp_int = tmp_int + ((tmp_motorwert[i] - tmp_int)/Parameter_UserParam7); |
|
- | 1777 | } |
|
- | 1778 | } |
|
- | 1779 | ||
- | 1780 | ||
- | 1781 | ||
- | 1782 | // MartinW; variable MS END |
|
1719 | else tmp_int = 2 * tmp_int - tmp_motorwert[i]; // MotorSmoothing |
1783 | |
1720 | 1784 | ||
1721 | LIMIT_MIN_MAX(tmp_int,(int) MIN_GAS * 4,(int) MAX_GAS * 4); |
1785 | LIMIT_MIN_MAX(tmp_int,(int) MIN_GAS * 4,(int) MAX_GAS * 4); |
1722 | Motor[i].SetPoint = tmp_int / 4; |
1786 | Motor[i].SetPoint = tmp_int / 4; |
1723 | Motor[i].SetPointLowerBits = (tmp_int % 4)<<1; // (3 bits total) |
1787 | Motor[i].SetPointLowerBits = (tmp_int % 4)<<1; // (3 bits total) |
1724 | tmp_motorwert[i] = tmp_int; |
1788 | tmp_motorwert[i] = tmp_int; |
1725 | } |
1789 | } |
1726 | else |
1790 | else |
1727 | { |
1791 | { |
1728 | Motor[i].SetPoint = 0; |
1792 | Motor[i].SetPoint = 0; |
1729 | Motor[i].SetPointLowerBits = 0; |
1793 | Motor[i].SetPointLowerBits = 0; |
1730 | } |
1794 | } |
1731 | } |
1795 | } |
1732 | } |
1796 | } |
1733 | 1797 |