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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 | 59 | ||
60 | unsigned char h,m,s; |
60 | unsigned char h,m,s; |
61 | unsigned int BaroExpandActive = 0; |
61 | unsigned int BaroExpandActive = 0; |
62 | volatile unsigned int I2CTimeout = 100; |
62 | volatile unsigned int I2CTimeout = 100; |
63 | int MesswertNick,MesswertRoll,MesswertGier,MesswertGierBias, RohMesswertNick,RohMesswertRoll; |
63 | int MesswertNick,MesswertRoll,MesswertGier,MesswertGierBias, RohMesswertNick,RohMesswertRoll; |
64 | int TrimNick, TrimRoll; |
64 | int TrimNick, TrimRoll; |
65 | int AdNeutralNick = 0,AdNeutralRoll = 0,AdNeutralGier = 0,StartNeutralRoll = 0,StartNeutralNick = 0; |
65 | int AdNeutralNick = 0,AdNeutralRoll = 0,AdNeutralGier = 0,StartNeutralRoll = 0,StartNeutralNick = 0; |
66 | int Mittelwert_AccNick, Mittelwert_AccRoll,Mittelwert_AccHoch; |
66 | int Mittelwert_AccNick, Mittelwert_AccRoll,Mittelwert_AccHoch; |
67 | unsigned int NeutralAccX=0, NeutralAccY=0; |
67 | unsigned int NeutralAccX=0, NeutralAccY=0; |
68 | int NaviAccNick, NaviAccRoll,NaviCntAcc = 0; |
68 | int NaviAccNick, NaviAccRoll,NaviCntAcc = 0; |
69 | int NeutralAccZ = 0; |
69 | int NeutralAccZ = 0; |
70 | unsigned char CosinusNickWinkel = 0, CosinusRollWinkel = 0 , ControlHeading = 0; |
70 | unsigned char CosinusNickWinkel = 0, CosinusRollWinkel = 0 , ControlHeading = 0; |
71 | long IntegralNick = 0,IntegralNick2 = 0; |
71 | long IntegralNick = 0,IntegralNick2 = 0; |
72 | long IntegralRoll = 0,IntegralRoll2 = 0; |
72 | long IntegralRoll = 0,IntegralRoll2 = 0; |
73 | long IntegralAccNick = 0,IntegralAccRoll = 0,IntegralAccZ = 0; |
73 | long IntegralAccNick = 0,IntegralAccRoll = 0,IntegralAccZ = 0; |
74 | long Integral_Gier = 0; |
74 | long Integral_Gier = 0; |
75 | long Mess_IntegralNick = 0,Mess_IntegralNick2 = 0; |
75 | long Mess_IntegralNick = 0,Mess_IntegralNick2 = 0; |
76 | long Mess_IntegralRoll = 0,Mess_IntegralRoll2 = 0; |
76 | long Mess_IntegralRoll = 0,Mess_IntegralRoll2 = 0; |
77 | long Mess_Integral_Gier = 0,Mess_Integral_Gier2 = 0; |
77 | long Mess_Integral_Gier = 0,Mess_Integral_Gier2 = 0; |
78 | long MittelIntegralNick,MittelIntegralRoll,MittelIntegralNick2,MittelIntegralRoll2; |
78 | long MittelIntegralNick,MittelIntegralRoll,MittelIntegralNick2,MittelIntegralRoll2; |
79 | volatile long Mess_Integral_Hoch = 0; |
79 | volatile long Mess_Integral_Hoch = 0; |
80 | int KompassValue = 0; |
80 | int KompassValue = 0; |
81 | int KompassStartwert = 0; |
81 | int KompassStartwert = 0; |
82 | int KompassRichtung = 0; |
82 | int KompassRichtung = 0; |
83 | unsigned int KompassSignalSchlecht = 500; |
83 | unsigned int KompassSignalSchlecht = 500; |
84 | unsigned char MAX_GAS,MIN_GAS; |
84 | unsigned char MAX_GAS,MIN_GAS; |
85 | unsigned char HoehenReglerAktiv = 0; |
85 | unsigned char HoehenReglerAktiv = 0; |
86 | unsigned char TrichterFlug = 0; |
86 | unsigned char TrichterFlug = 0; |
87 | long Umschlag180Nick = 250000L, Umschlag180Roll = 250000L; |
87 | long Umschlag180Nick = 250000L, Umschlag180Roll = 250000L; |
88 | long ErsatzKompass; |
88 | long ErsatzKompass; |
89 | int ErsatzKompassInGrad; // Kompasswert in Grad |
89 | int ErsatzKompassInGrad; // Kompasswert in Grad |
90 | int GierGyroFehler = 0; |
90 | int GierGyroFehler = 0; |
91 | char GyroFaktor,GyroFaktorGier; |
91 | char GyroFaktor,GyroFaktorGier; |
92 | char IntegralFaktor,IntegralFaktorGier; |
92 | char IntegralFaktor,IntegralFaktorGier; |
93 | int DiffNick,DiffRoll; |
93 | int DiffNick,DiffRoll; |
94 | //int Poti1 = 0, Poti2 = 0, Poti3 = 0, Poti4 = 0, Poti5 = 0, Poti6 = 0, Poti7 = 0, Poti8 = 0; |
94 | //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}; |
95 | unsigned char Poti[9] = {0,0,0,0,0,0,0,0}; |
96 | volatile unsigned char SenderOkay = 0; |
96 | volatile unsigned char SenderOkay = 0; |
97 | int StickNick = 0,StickRoll = 0,StickGier = 0,StickGas = 0; |
97 | int StickNick = 0,StickRoll = 0,StickGier = 0,StickGas = 0; |
98 | char MotorenEin = 0; |
98 | char MotorenEin = 0; |
99 | long HoehenWert = 0; |
99 | long HoehenWert = 0; |
100 | long SollHoehe = 0; |
100 | long SollHoehe = 0; |
101 | int LageKorrekturRoll = 0,LageKorrekturNick = 0; |
101 | int LageKorrekturRoll = 0,LageKorrekturNick = 0; |
102 | //float Ki = FAKTOR_I; |
102 | //float Ki = FAKTOR_I; |
103 | int Ki = (10300/2) / 33; |
103 | int Ki = (10300/2) / 33; |
104 | unsigned char Looping_Nick = 0,Looping_Roll = 0; |
104 | unsigned char Looping_Nick = 0,Looping_Roll = 0; |
105 | unsigned char Looping_Links = 0, Looping_Rechts = 0, Looping_Unten = 0, Looping_Oben = 0; |
105 | unsigned char Looping_Links = 0, Looping_Rechts = 0, Looping_Unten = 0, Looping_Oben = 0; |
106 | 106 | ||
107 | unsigned char Parameter_Luftdruck_D = 48; // Wert : 0-250 |
107 | unsigned char Parameter_Luftdruck_D = 48; // Wert : 0-250 |
108 | unsigned char Parameter_MaxHoehe = 251; // Wert : 0-250 |
108 | unsigned char Parameter_MaxHoehe = 251; // Wert : 0-250 |
109 | unsigned char Parameter_Hoehe_P = 16; // Wert : 0-32 |
109 | unsigned char Parameter_Hoehe_P = 16; // Wert : 0-32 |
110 | unsigned char Parameter_Hoehe_ACC_Wirkung = 58; // Wert : 0-250 |
110 | unsigned char Parameter_Hoehe_ACC_Wirkung = 58; // Wert : 0-250 |
111 | unsigned char Parameter_KompassWirkung = 64; // Wert : 0-250 |
111 | unsigned char Parameter_KompassWirkung = 64; // Wert : 0-250 |
112 | unsigned char Parameter_Hoehe_GPS_Z = 64; // Wert : 0-250 |
112 | unsigned char Parameter_Hoehe_GPS_Z = 64; // Wert : 0-250 |
113 | unsigned char Parameter_Gyro_D = 8; // Wert : 0-250 |
113 | unsigned char Parameter_Gyro_D = 8; // Wert : 0-250 |
114 | unsigned char Parameter_Gyro_P = 150; // Wert : 10-250 |
114 | unsigned char Parameter_Gyro_P = 150; // Wert : 10-250 |
115 | unsigned char Parameter_Gyro_I = 150; // Wert : 0-250 |
115 | unsigned char Parameter_Gyro_I = 150; // Wert : 0-250 |
116 | unsigned char Parameter_Gyro_Gier_P = 150; // Wert : 10-250 |
116 | unsigned char Parameter_Gyro_Gier_P = 150; // Wert : 10-250 |
117 | unsigned char Parameter_Gyro_Gier_I = 150; // Wert : 10-250 |
117 | unsigned char Parameter_Gyro_Gier_I = 150; // Wert : 10-250 |
118 | unsigned char Parameter_Gier_P = 2; // Wert : 1-20 |
118 | unsigned char Parameter_Gier_P = 2; // Wert : 1-20 |
119 | unsigned char Parameter_I_Faktor = 10; // Wert : 1-20 |
119 | unsigned char Parameter_I_Faktor = 10; // Wert : 1-20 |
120 | unsigned char Parameter_UserParam1 = 0; |
120 | unsigned char Parameter_UserParam1 = 0; |
121 | unsigned char Parameter_UserParam2 = 0; |
121 | unsigned char Parameter_UserParam2 = 0; |
122 | unsigned char Parameter_UserParam3 = 0; |
122 | unsigned char Parameter_UserParam3 = 0; |
123 | unsigned char Parameter_UserParam4 = 0; |
123 | unsigned char Parameter_UserParam4 = 0; |
124 | unsigned char Parameter_UserParam5 = 0; |
124 | unsigned char Parameter_UserParam5 = 0; |
125 | unsigned char Parameter_UserParam6 = 0; |
125 | unsigned char Parameter_UserParam6 = 0; |
126 | unsigned char Parameter_UserParam7 = 0; |
126 | unsigned char Parameter_UserParam7 = 0; |
127 | unsigned char Parameter_UserParam8 = 0; |
127 | unsigned char Parameter_UserParam8 = 0; |
128 | unsigned char Parameter_ServoNickControl = 100; |
128 | unsigned char Parameter_ServoNickControl = 100; |
129 | unsigned char Parameter_ServoRollControl = 100; |
129 | unsigned char Parameter_ServoRollControl = 100; |
130 | unsigned char Parameter_LoopGasLimit = 70; |
130 | unsigned char Parameter_LoopGasLimit = 70; |
131 | unsigned char Parameter_AchsKopplung1 = 90; |
131 | unsigned char Parameter_AchsKopplung1 = 90; |
132 | unsigned char Parameter_AchsKopplung2 = 65; |
132 | unsigned char Parameter_AchsKopplung2 = 65; |
133 | unsigned char Parameter_CouplingYawCorrection = 64; |
133 | unsigned char Parameter_CouplingYawCorrection = 64; |
134 | //unsigned char Parameter_AchsGegenKopplung1 = 0; |
134 | //unsigned char Parameter_AchsGegenKopplung1 = 0; |
135 | unsigned char Parameter_DynamicStability = 100; |
135 | unsigned char Parameter_DynamicStability = 100; |
136 | unsigned char Parameter_J16Bitmask; // for the J16 Output |
136 | unsigned char Parameter_J16Bitmask; // for the J16 Output |
137 | unsigned char Parameter_J16Timing; // for the J16 Output |
137 | unsigned char Parameter_J16Timing; // for the J16 Output |
138 | unsigned char Parameter_J17Bitmask; // for the J17 Output |
138 | unsigned char Parameter_J17Bitmask; // for the J17 Output |
139 | unsigned char Parameter_J17Timing; // for the J17 Output |
139 | unsigned char Parameter_J17Timing; // for the J17 Output |
140 | unsigned char Parameter_NaviGpsModeControl; // Parameters for the Naviboard |
140 | unsigned char Parameter_NaviGpsModeControl; // Parameters for the Naviboard |
141 | unsigned char Parameter_NaviGpsGain; |
141 | unsigned char Parameter_NaviGpsGain; |
142 | unsigned char Parameter_NaviGpsP; |
142 | unsigned char Parameter_NaviGpsP; |
143 | unsigned char Parameter_NaviGpsI; |
143 | unsigned char Parameter_NaviGpsI; |
144 | unsigned char Parameter_NaviGpsD; |
144 | unsigned char Parameter_NaviGpsD; |
145 | unsigned char Parameter_NaviGpsACC; |
145 | unsigned char Parameter_NaviGpsACC; |
146 | unsigned char Parameter_NaviOperatingRadius; |
146 | unsigned char Parameter_NaviOperatingRadius; |
147 | unsigned char Parameter_NaviWindCorrection; |
147 | unsigned char Parameter_NaviWindCorrection; |
148 | unsigned char Parameter_NaviSpeedCompensation; |
148 | unsigned char Parameter_NaviSpeedCompensation; |
149 | unsigned char Parameter_ExternalControl; |
149 | unsigned char Parameter_ExternalControl; |
150 | unsigned char Parameter_Servo3,Parameter_Servo4,Parameter_Servo5; |
150 | unsigned char Parameter_Servo3,Parameter_Servo4,Parameter_Servo5; |
151 | unsigned char HeadFree = 0; |
151 | unsigned char HeadFree = 0; |
152 | 152 | ||
153 | signed int ExternStickNick = 0,ExternStickRoll = 0,ExternStickGier = 0, ExternHoehenValue = -20; |
153 | signed int ExternStickNick = 0,ExternStickRoll = 0,ExternStickGier = 0, ExternHoehenValue = -20; |
154 | int MaxStickNick = 0,MaxStickRoll = 0; |
154 | int MaxStickNick = 0,MaxStickRoll = 0; |
155 | unsigned int modell_fliegt = 0; |
155 | unsigned int modell_fliegt = 0; |
156 | volatile unsigned char FCFlags = 0; |
156 | volatile unsigned char FCFlags = 0; |
157 | long GIER_GRAD_FAKTOR = 1291; |
157 | long GIER_GRAD_FAKTOR = 1291; |
158 | signed int KopplungsteilNickRoll,KopplungsteilRollNick; |
158 | signed int KopplungsteilNickRoll,KopplungsteilRollNick; |
159 | signed int tmp_motorwert[MAX_MOTORS]; |
159 | signed int tmp_motorwert[MAX_MOTORS]; |
160 | char VarioCharacter = ' '; |
160 | char VarioCharacter = ' '; |
161 | 161 | ||
162 | #define LIMIT_MIN(value, min) {if(value <= min) value = min;} |
162 | #define LIMIT_MIN(value, min) {if(value <= min) value = min;} |
163 | #define LIMIT_MAX(value, max) {if(value >= max) value = max;} |
163 | #define LIMIT_MAX(value, max) {if(value >= max) value = max;} |
164 | #define LIMIT_MIN_MAX(value, min, max) {if(value <= min) value = min; else if(value >= max) value = max;} |
164 | #define LIMIT_MIN_MAX(value, min, max) {if(value <= min) value = min; else if(value >= max) value = max;} |
165 | 165 | ||
166 | 166 | ||
167 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
167 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
168 | // Debugwerte zuordnen |
168 | // Debugwerte zuordnen |
169 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
169 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
170 | void CopyDebugValues(void) |
170 | void CopyDebugValues(void) |
171 | { |
171 | { |
172 | DebugOut.Analog[0] = IntegralNick / (EE_Parameter.GyroAccFaktor * 4); |
172 | DebugOut.Analog[0] = IntegralNick / (EE_Parameter.GyroAccFaktor * 4); |
173 | DebugOut.Analog[1] = IntegralRoll / (EE_Parameter.GyroAccFaktor * 4); |
173 | DebugOut.Analog[1] = IntegralRoll / (EE_Parameter.GyroAccFaktor * 4); |
174 | DebugOut.Analog[2] = Mittelwert_AccNick / 4; |
174 | DebugOut.Analog[2] = Mittelwert_AccNick / 4; |
175 | DebugOut.Analog[3] = Mittelwert_AccRoll / 4; |
175 | DebugOut.Analog[3] = Mittelwert_AccRoll / 4; |
176 | DebugOut.Analog[4] = MesswertGier; |
176 | DebugOut.Analog[4] = (signed int) AdNeutralGier - AdWertGier; |
177 | DebugOut.Analog[5] = HoehenWert/5; |
177 | DebugOut.Analog[5] = HoehenWert/5; |
178 | DebugOut.Analog[6] = (Mess_Integral_Hoch / 512);//AdWertAccHoch;// Aktuell_az;//(Mess_Integral_Hoch / 512);//Aktuell_az; |
178 | DebugOut.Analog[6] = (Mess_Integral_Hoch / 512);//AdWertAccHoch;// Aktuell_az;//(Mess_Integral_Hoch / 512);//Aktuell_az; |
179 | DebugOut.Analog[8] = KompassValue; |
179 | DebugOut.Analog[8] = KompassValue; |
180 | DebugOut.Analog[9] = UBat; |
180 | DebugOut.Analog[9] = UBat; |
181 | DebugOut.Analog[10] = SenderOkay; |
181 | DebugOut.Analog[10] = SenderOkay; |
182 | DebugOut.Analog[11] = ErsatzKompass / GIER_GRAD_FAKTOR; |
182 | DebugOut.Analog[11] = ErsatzKompass / GIER_GRAD_FAKTOR; |
183 | //DebugOut.Analog[16] = NeutralAccZ; |
183 | //DebugOut.Analog[16] = NeutralAccZ; |
184 | //DebugOut.Analog[16] = Motor[0].Temperature; |
184 | //DebugOut.Analog[16] = Motor[0].Temperature; |
185 | //DebugOut.Analog[17] = FromNaviCtrl_Value.Distance; |
185 | //DebugOut.Analog[17] = FromNaviCtrl_Value.Distance; |
186 | // DebugOut.Analog[18] = VarioMeter; |
186 | // DebugOut.Analog[18] = VarioMeter; |
187 | // DebugOut.Analog[19] = WinkelOut.CalcState; |
187 | // DebugOut.Analog[19] = WinkelOut.CalcState; |
188 | DebugOut.Analog[20] = ServoNickValue; |
188 | DebugOut.Analog[20] = ServoNickValue; |
189 | DebugOut.Analog[22] = Capacity.ActualCurrent; |
189 | DebugOut.Analog[22] = Capacity.ActualCurrent; |
190 | DebugOut.Analog[23] = Capacity.UsedCapacity; |
190 | DebugOut.Analog[23] = Capacity.UsedCapacity; |
191 | // DebugOut.Analog[22] = FromNaviCtrl_Value.GpsZ; |
191 | // DebugOut.Analog[22] = FromNaviCtrl_Value.GpsZ; |
192 | // DebugOut.Analog[24] = MesswertNick/2; |
192 | // DebugOut.Analog[24] = MesswertNick/2; |
193 | // DebugOut.Analog[25] = MesswertRoll/2; |
193 | // DebugOut.Analog[25] = MesswertRoll/2; |
194 | // DebugOut.Analog[27] = (int)FromNaviCtrl_Value.Kalman_MaxDrift; |
194 | // DebugOut.Analog[27] = (int)FromNaviCtrl_Value.Kalman_MaxDrift; |
195 | // DebugOut.Analog[28] = (int)FromNaviCtrl_Value.Kalman_MaxFusion; |
195 | // DebugOut.Analog[28] = (int)FromNaviCtrl_Value.Kalman_MaxFusion; |
196 | // DebugOut.Analog[29] = (int)FromNaviCtrl_Value.Kalman_K; |
196 | // DebugOut.Analog[29] = (int)FromNaviCtrl_Value.Kalman_K; |
197 | //DebugOut.Analog[28] = I2CError; |
197 | //DebugOut.Analog[28] = I2CError; |
198 | DebugOut.Analog[29] = FromNaviCtrl_Value.SerialDataOkay; |
198 | DebugOut.Analog[29] = FromNaviCtrl_Value.SerialDataOkay; |
199 | DebugOut.Analog[30] = GPS_Nick; |
199 | DebugOut.Analog[30] = GPS_Nick; |
200 | DebugOut.Analog[31] = GPS_Roll; |
200 | DebugOut.Analog[31] = GPS_Roll; |
201 | } |
201 | } |
202 | 202 | ||
203 | void Piep(unsigned char Anzahl, unsigned int dauer) |
203 | void Piep(unsigned char Anzahl, unsigned int dauer) |
204 | { |
204 | { |
205 | if(MotorenEin) return; //auf keinen Fall im Flug! |
205 | if(MotorenEin) return; //auf keinen Fall im Flug! |
206 | while(Anzahl--) |
206 | while(Anzahl--) |
207 | { |
207 | { |
208 | beeptime = dauer; |
208 | beeptime = dauer; |
209 | while(beeptime); |
209 | while(beeptime); |
210 | Delay_ms(dauer * 2); |
210 | Delay_ms(dauer * 2); |
211 | } |
211 | } |
212 | } |
212 | } |
213 | 213 | ||
214 | //############################################################################ |
214 | //############################################################################ |
215 | // Messwerte beim Ermitteln der Nullage |
215 | // Messwerte beim Ermitteln der Nullage |
216 | void CalibrierMittelwert(void) |
216 | void CalibrierMittelwert(void) |
217 | //############################################################################ |
217 | //############################################################################ |
218 | { |
218 | { |
219 | unsigned char i; |
219 | unsigned char i; |
220 | if(PlatinenVersion == 13) SucheGyroOffset(); |
220 | if(PlatinenVersion == 13) SucheGyroOffset(); |
221 | // ADC auschalten, damit die Werte sich nicht während der Berechnung ändern |
221 | // ADC auschalten, damit die Werte sich nicht während der Berechnung ändern |
222 | ANALOG_OFF; |
222 | ANALOG_OFF; |
223 | MesswertNick = AdWertNick; |
223 | MesswertNick = AdWertNick; |
224 | MesswertRoll = AdWertRoll; |
224 | MesswertRoll = AdWertRoll; |
225 | MesswertGier = AdWertGier; |
225 | MesswertGier = AdWertGier; |
226 | Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
226 | Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
227 | Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
227 | Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
228 | Mittelwert_AccHoch = (long)AdWertAccHoch; |
228 | Mittelwert_AccHoch = (long)AdWertAccHoch; |
229 | // ADC einschalten |
229 | // ADC einschalten |
230 | ANALOG_ON; |
230 | ANALOG_ON; |
231 | for(i=0;i<8;i++) |
231 | for(i=0;i<8;i++) |
232 | { |
232 | { |
233 | int tmp; |
233 | int tmp; |
234 | tmp = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
234 | tmp = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
235 | LIMIT_MIN_MAX(tmp, 0, 255); |
235 | LIMIT_MIN_MAX(tmp, 0, 255); |
236 | if(Poti[i] > tmp) Poti[i]--; else if(Poti[i] < tmp) Poti[i]++; |
236 | if(Poti[i] > tmp) Poti[i]--; else if(Poti[i] < tmp) Poti[i]++; |
237 | } |
237 | } |
238 | Umschlag180Nick = (long) EE_Parameter.WinkelUmschlagNick * 2500L; |
238 | Umschlag180Nick = (long) EE_Parameter.WinkelUmschlagNick * 2500L; |
239 | Umschlag180Roll = (long) EE_Parameter.WinkelUmschlagRoll * 2500L; |
239 | Umschlag180Roll = (long) EE_Parameter.WinkelUmschlagRoll * 2500L; |
240 | } |
240 | } |
241 | 241 | ||
242 | //############################################################################ |
242 | //############################################################################ |
243 | // Nullwerte ermitteln |
243 | // Nullwerte ermitteln |
244 | void SetNeutral(unsigned char AccAdjustment) |
244 | void SetNeutral(unsigned char AccAdjustment) |
245 | //############################################################################ |
245 | //############################################################################ |
246 | { |
246 | { |
247 | unsigned char i; |
247 | unsigned char i; |
248 | unsigned int gier_neutral=0, nick_neutral=0, roll_neutral=0; |
248 | unsigned int gier_neutral=0, nick_neutral=0, roll_neutral=0; |
249 | 249 | ||
250 | HEF4017R_ON; |
250 | HEF4017R_ON; |
251 | NeutralAccX = 0; |
251 | NeutralAccX = 0; |
252 | NeutralAccY = 0; |
252 | NeutralAccY = 0; |
253 | NeutralAccZ = 0; |
253 | NeutralAccZ = 0; |
254 | 254 | ||
255 | AdNeutralNick = 0; |
255 | AdNeutralNick = 0; |
256 | AdNeutralRoll = 0; |
256 | AdNeutralRoll = 0; |
257 | AdNeutralGier = 0; |
257 | AdNeutralGier = 0; |
258 | 258 | ||
259 | Parameter_AchsKopplung1 = 0; |
259 | Parameter_AchsKopplung1 = 0; |
260 | Parameter_AchsKopplung2 = 0; |
260 | Parameter_AchsKopplung2 = 0; |
261 | 261 | ||
262 | ExpandBaro = 0; |
262 | ExpandBaro = 0; |
263 | 263 | ||
264 | I2C_SendBLConfig(); |
264 | I2C_SendBLConfig(); |
265 | 265 | ||
266 | CalibrierMittelwert(); |
266 | CalibrierMittelwert(); |
267 | Delay_ms_Mess(100); |
267 | Delay_ms_Mess(100); |
268 | 268 | ||
269 | CalibrierMittelwert(); |
269 | CalibrierMittelwert(); |
270 | 270 | ||
271 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
271 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
272 | { |
272 | { |
273 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
273 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
274 | } |
274 | } |
275 | #define NEUTRAL_FILTER 32 |
275 | #define NEUTRAL_FILTER 32 |
276 | for(i=0; i<NEUTRAL_FILTER; i++) |
276 | for(i=0; i<NEUTRAL_FILTER; i++) |
277 | { |
277 | { |
278 | Delay_ms_Mess(10); |
278 | Delay_ms_Mess(10); |
279 | gier_neutral += AdWertGier; |
279 | gier_neutral += AdWertGier; |
280 | nick_neutral += AdWertNick; |
280 | nick_neutral += AdWertNick; |
281 | roll_neutral += AdWertRoll; |
281 | roll_neutral += AdWertRoll; |
282 | } |
282 | } |
283 | AdNeutralNick= (nick_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
283 | AdNeutralNick= (nick_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
284 | AdNeutralRoll= (roll_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
284 | AdNeutralRoll= (roll_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
285 | AdNeutralGier= (gier_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER); |
285 | AdNeutralGier= (gier_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER); |
286 | 286 | ||
287 | StartNeutralRoll = AdNeutralRoll; |
287 | StartNeutralRoll = AdNeutralRoll; |
288 | StartNeutralNick = AdNeutralNick; |
288 | StartNeutralNick = AdNeutralNick; |
289 | 289 | ||
290 | if(AccAdjustment) |
290 | if(AccAdjustment) |
291 | { |
291 | { |
292 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
292 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
293 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
293 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
294 | NeutralAccZ = Aktuell_az; |
294 | NeutralAccZ = Aktuell_az; |
295 | 295 | ||
296 | // Save ACC neutral settings to eeprom |
296 | // Save ACC neutral settings to eeprom |
297 | SetParamWord(PID_ACC_NICK, (uint16_t)NeutralAccX); |
297 | SetParamWord(PID_ACC_NICK, (uint16_t)NeutralAccX); |
298 | SetParamWord(PID_ACC_ROLL, (uint16_t)NeutralAccY); |
298 | SetParamWord(PID_ACC_ROLL, (uint16_t)NeutralAccY); |
299 | SetParamWord(PID_ACC_TOP, (uint16_t)NeutralAccZ); |
299 | SetParamWord(PID_ACC_TOP, (uint16_t)NeutralAccZ); |
300 | } |
300 | } |
301 | else |
301 | else |
302 | { |
302 | { |
303 | // restore from eeprom |
303 | // restore from eeprom |
304 | NeutralAccX = (int16_t)GetParamWord(PID_ACC_NICK); |
304 | NeutralAccX = (int16_t)GetParamWord(PID_ACC_NICK); |
305 | NeutralAccY = (int16_t)GetParamWord(PID_ACC_ROLL); |
305 | NeutralAccY = (int16_t)GetParamWord(PID_ACC_ROLL); |
306 | NeutralAccZ = (int16_t)GetParamWord(PID_ACC_TOP); |
306 | NeutralAccZ = (int16_t)GetParamWord(PID_ACC_TOP); |
307 | // strange settings? |
307 | // strange settings? |
308 | if(((unsigned int) NeutralAccX > 2048) || ((unsigned int) NeutralAccY > 2048) || ((unsigned int) NeutralAccZ > 1024)) |
308 | if(((unsigned int) NeutralAccX > 2048) || ((unsigned int) NeutralAccY > 2048) || ((unsigned int) NeutralAccZ > 1024)) |
309 | { |
309 | { |
310 | printf("\n\rACC not calibrated!\r\n"); |
310 | printf("\n\rACC not calibrated!\r\n"); |
311 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
311 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
312 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
312 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
313 | NeutralAccZ = Aktuell_az; |
313 | NeutralAccZ = Aktuell_az; |
314 | } |
314 | } |
315 | } |
315 | } |
316 | 316 | ||
317 | MesswertNick = 0; |
317 | MesswertNick = 0; |
318 | MesswertRoll = 0; |
318 | MesswertRoll = 0; |
319 | MesswertGier = 0; |
319 | MesswertGier = 0; |
320 | Delay_ms_Mess(100); |
320 | Delay_ms_Mess(100); |
321 | Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
321 | Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
322 | Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
322 | Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
323 | IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
323 | IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
324 | IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
324 | IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
325 | Mess_IntegralNick2 = IntegralNick; |
325 | Mess_IntegralNick2 = IntegralNick; |
326 | Mess_IntegralRoll2 = IntegralRoll; |
326 | Mess_IntegralRoll2 = IntegralRoll; |
327 | Mess_Integral_Gier = 0; |
327 | Mess_Integral_Gier = 0; |
328 | StartLuftdruck = Luftdruck; |
328 | StartLuftdruck = Luftdruck; |
329 | VarioMeter = 0; |
329 | VarioMeter = 0; |
330 | Mess_Integral_Hoch = 0; |
330 | Mess_Integral_Hoch = 0; |
331 | KompassStartwert = KompassValue; |
331 | KompassStartwert = KompassValue; |
332 | ControlHeading = KompassValue / 15; |
- | |
333 | GPS_Neutral(); |
332 | GPS_Neutral(); |
334 | beeptime = 50; |
333 | beeptime = 50; |
335 | Umschlag180Nick = ((long) EE_Parameter.WinkelUmschlagNick * 2500L) + 15000L; |
334 | Umschlag180Nick = ((long) EE_Parameter.WinkelUmschlagNick * 2500L) + 15000L; |
336 | Umschlag180Roll = ((long) EE_Parameter.WinkelUmschlagRoll * 2500L) + 15000L; |
335 | Umschlag180Roll = ((long) EE_Parameter.WinkelUmschlagRoll * 2500L) + 15000L; |
337 | ExternHoehenValue = 0; |
336 | ExternHoehenValue = 0; |
338 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
337 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
339 | GierGyroFehler = 0; |
338 | GierGyroFehler = 0; |
340 | SendVersionToNavi = 1; |
339 | SendVersionToNavi = 1; |
341 | LED_Init(); |
340 | LED_Init(); |
342 | FCFlags |= FCFLAG_CALIBRATE; |
341 | FCFlags |= FCFLAG_CALIBRATE; |
343 | FromNaviCtrl_Value.Kalman_K = -1; |
342 | FromNaviCtrl_Value.Kalman_K = -1; |
344 | FromNaviCtrl_Value.Kalman_MaxDrift = 0; |
343 | FromNaviCtrl_Value.Kalman_MaxDrift = 0; |
345 | FromNaviCtrl_Value.Kalman_MaxFusion = 32; |
344 | FromNaviCtrl_Value.Kalman_MaxFusion = 32; |
346 | 345 | ||
347 | for(i=0;i<8;i++) |
346 | for(i=0;i<8;i++) |
348 | { |
347 | { |
349 | Poti[i] = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
348 | Poti[i] = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
350 | } |
349 | } |
351 | SenderOkay = 100; |
350 | SenderOkay = 100; |
352 | if(ServoActive) |
351 | if(ServoActive) |
353 | { |
352 | { |
354 | HEF4017R_ON; |
353 | HEF4017R_ON; |
355 | DDRD |=0x80; // enable J7 -> Servo signal |
354 | DDRD |=0x80; // enable J7 -> Servo signal |
356 | } |
355 | } |
357 | } |
356 | } |
358 | 357 | ||
359 | //############################################################################ |
358 | //############################################################################ |
360 | // Bearbeitet die Messwerte |
359 | // Bearbeitet die Messwerte |
361 | void Mittelwert(void) |
360 | void Mittelwert(void) |
362 | //############################################################################ |
361 | //############################################################################ |
363 | { |
362 | { |
364 | static signed long tmpl,tmpl2,tmpl3,tmpl4; |
363 | static signed long tmpl,tmpl2,tmpl3,tmpl4; |
365 | static signed int oldNick, oldRoll, d2Roll, d2Nick; |
364 | static signed int oldNick, oldRoll, d2Roll, d2Nick; |
366 | signed long winkel_nick, winkel_roll; |
365 | signed long winkel_nick, winkel_roll; |
367 | unsigned char i; |
366 | unsigned char i; |
368 | MesswertGier = (signed int) AdNeutralGier - AdWertGier; |
367 | MesswertGier = (signed int) AdNeutralGier - AdWertGier; |
369 | MesswertNick = (signed int) AdWertNickFilter / 8; |
368 | MesswertNick = (signed int) AdWertNickFilter / 8; |
370 | MesswertRoll = (signed int) AdWertRollFilter / 8; |
369 | MesswertRoll = (signed int) AdWertRollFilter / 8; |
371 | RohMesswertNick = MesswertNick; |
370 | RohMesswertNick = MesswertNick; |
372 | RohMesswertRoll = MesswertRoll; |
371 | RohMesswertRoll = MesswertRoll; |
373 | 372 | ||
374 | // Beschleunigungssensor ++++++++++++++++++++++++++++++++++++++++++++++++ |
373 | // Beschleunigungssensor ++++++++++++++++++++++++++++++++++++++++++++++++ |
375 | Mittelwert_AccNick = ((long)Mittelwert_AccNick * 3 + ((ACC_AMPLIFY * (long)AdWertAccNick))) / 4L; |
374 | Mittelwert_AccNick = ((long)Mittelwert_AccNick * 3 + ((ACC_AMPLIFY * (long)AdWertAccNick))) / 4L; |
376 | Mittelwert_AccRoll = ((long)Mittelwert_AccRoll * 3 + ((ACC_AMPLIFY * (long)AdWertAccRoll))) / 4L; |
375 | Mittelwert_AccRoll = ((long)Mittelwert_AccRoll * 3 + ((ACC_AMPLIFY * (long)AdWertAccRoll))) / 4L; |
377 | Mittelwert_AccHoch = ((long)Mittelwert_AccHoch * 3 + ((long)AdWertAccHoch)) / 4L; |
376 | Mittelwert_AccHoch = ((long)Mittelwert_AccHoch * 3 + ((long)AdWertAccHoch)) / 4L; |
378 | IntegralAccNick += ACC_AMPLIFY * AdWertAccNick; |
377 | IntegralAccNick += ACC_AMPLIFY * AdWertAccNick; |
379 | IntegralAccRoll += ACC_AMPLIFY * AdWertAccRoll; |
378 | IntegralAccRoll += ACC_AMPLIFY * AdWertAccRoll; |
380 | NaviAccNick += AdWertAccNick; |
379 | NaviAccNick += AdWertAccNick; |
381 | NaviAccRoll += AdWertAccRoll; |
380 | NaviAccRoll += AdWertAccRoll; |
382 | NaviCntAcc++; |
381 | NaviCntAcc++; |
383 | IntegralAccZ += Aktuell_az - NeutralAccZ; |
382 | IntegralAccZ += Aktuell_az - NeutralAccZ; |
384 | 383 | ||
385 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
384 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
386 | // ADC einschalten |
385 | // ADC einschalten |
387 | ANALOG_ON; |
386 | ANALOG_ON; |
388 | AdReady = 0; |
387 | AdReady = 0; |
389 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
388 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
390 | 389 | ||
391 | if(Mess_IntegralRoll > 93000L) winkel_roll = 93000L; |
390 | if(Mess_IntegralRoll > 93000L) winkel_roll = 93000L; |
392 | else if(Mess_IntegralRoll <-93000L) winkel_roll = -93000L; |
391 | else if(Mess_IntegralRoll <-93000L) winkel_roll = -93000L; |
393 | else winkel_roll = Mess_IntegralRoll; |
392 | else winkel_roll = Mess_IntegralRoll; |
394 | 393 | ||
395 | if(Mess_IntegralNick > 93000L) winkel_nick = 93000L; |
394 | if(Mess_IntegralNick > 93000L) winkel_nick = 93000L; |
396 | else if(Mess_IntegralNick <-93000L) winkel_nick = -93000L; |
395 | else if(Mess_IntegralNick <-93000L) winkel_nick = -93000L; |
397 | else winkel_nick = Mess_IntegralNick; |
396 | else winkel_nick = Mess_IntegralNick; |
398 | 397 | ||
399 | // Gier ++++++++++++++++++++++++++++++++++++++++++++++++ |
398 | // Gier ++++++++++++++++++++++++++++++++++++++++++++++++ |
400 | Mess_Integral_Gier += MesswertGier; |
399 | Mess_Integral_Gier += MesswertGier; |
401 | ErsatzKompass += MesswertGier; |
400 | ErsatzKompass += MesswertGier; |
402 | // Kopplungsanteil +++++++++++++++++++++++++++++++++++++ |
401 | // Kopplungsanteil +++++++++++++++++++++++++++++++++++++ |
403 | if(!Looping_Nick && !Looping_Roll && (EE_Parameter.GlobalConfig & CFG_ACHSENKOPPLUNG_AKTIV)) |
402 | if(!Looping_Nick && !Looping_Roll && (EE_Parameter.GlobalConfig & CFG_ACHSENKOPPLUNG_AKTIV)) |
404 | { |
403 | { |
405 | tmpl3 = (MesswertRoll * winkel_nick) / 2048L; |
404 | tmpl3 = (MesswertRoll * winkel_nick) / 2048L; |
406 | tmpl3 *= Parameter_AchsKopplung2; //65 |
405 | tmpl3 *= Parameter_AchsKopplung2; //65 |
407 | tmpl3 /= 4096L; |
406 | tmpl3 /= 4096L; |
408 | tmpl4 = (MesswertNick * winkel_roll) / 2048L; |
407 | tmpl4 = (MesswertNick * winkel_roll) / 2048L; |
409 | tmpl4 *= Parameter_AchsKopplung2; //65 |
408 | tmpl4 *= Parameter_AchsKopplung2; //65 |
410 | tmpl4 /= 4096L; |
409 | tmpl4 /= 4096L; |
411 | KopplungsteilNickRoll = tmpl3; |
410 | KopplungsteilNickRoll = tmpl3; |
412 | KopplungsteilRollNick = tmpl4; |
411 | KopplungsteilRollNick = tmpl4; |
413 | tmpl4 -= tmpl3; |
412 | tmpl4 -= tmpl3; |
414 | ErsatzKompass += tmpl4; |
413 | ErsatzKompass += tmpl4; |
415 | if(!Parameter_CouplingYawCorrection) Mess_Integral_Gier -= tmpl4/2; // Gier nachhelfen |
414 | if(!Parameter_CouplingYawCorrection) Mess_Integral_Gier -= tmpl4/2; // Gier nachhelfen |
416 | 415 | ||
417 | tmpl = ((MesswertGier + tmpl4) * winkel_nick) / 2048L; |
416 | tmpl = ((MesswertGier + tmpl4) * winkel_nick) / 2048L; |
418 | tmpl *= Parameter_AchsKopplung1; // 90 |
417 | tmpl *= Parameter_AchsKopplung1; // 90 |
419 | tmpl /= 4096L; |
418 | tmpl /= 4096L; |
420 | tmpl2 = ((MesswertGier + tmpl4) * winkel_roll) / 2048L; |
419 | tmpl2 = ((MesswertGier + tmpl4) * winkel_roll) / 2048L; |
421 | tmpl2 *= Parameter_AchsKopplung1; |
420 | tmpl2 *= Parameter_AchsKopplung1; |
422 | tmpl2 /= 4096L; |
421 | tmpl2 /= 4096L; |
423 | if(abs(MesswertGier) > 64) if(labs(tmpl) > 128 || labs(tmpl2) > 128) TrichterFlug = 1; |
422 | if(abs(MesswertGier) > 64) if(labs(tmpl) > 128 || labs(tmpl2) > 128) TrichterFlug = 1; |
424 | //MesswertGier += (Parameter_CouplingYawCorrection * tmpl4) / 256; |
423 | //MesswertGier += (Parameter_CouplingYawCorrection * tmpl4) / 256; |
425 | } |
424 | } |
426 | else tmpl = tmpl2 = KopplungsteilNickRoll = KopplungsteilRollNick = 0; |
425 | else tmpl = tmpl2 = KopplungsteilNickRoll = KopplungsteilRollNick = 0; |
427 | TrimRoll = tmpl - tmpl2 / 100L; |
426 | TrimRoll = tmpl - tmpl2 / 100L; |
428 | TrimNick = -tmpl2 + tmpl / 100L; |
427 | TrimNick = -tmpl2 + tmpl / 100L; |
429 | // Kompasswert begrenzen ++++++++++++++++++++++++++++++++++++++++++++++++ |
428 | // Kompasswert begrenzen ++++++++++++++++++++++++++++++++++++++++++++++++ |
430 | if(ErsatzKompass >= (360L * GIER_GRAD_FAKTOR)) ErsatzKompass -= 360L * GIER_GRAD_FAKTOR; // 360° Umschlag |
429 | if(ErsatzKompass >= (360L * GIER_GRAD_FAKTOR)) ErsatzKompass -= 360L * GIER_GRAD_FAKTOR; // 360° Umschlag |
431 | if(ErsatzKompass < 0) ErsatzKompass += 360L * GIER_GRAD_FAKTOR; |
430 | if(ErsatzKompass < 0) ErsatzKompass += 360L * GIER_GRAD_FAKTOR; |
432 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
431 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
433 | Mess_IntegralRoll2 += MesswertRoll + TrimRoll; |
432 | Mess_IntegralRoll2 += MesswertRoll + TrimRoll; |
434 | Mess_IntegralRoll += MesswertRoll + TrimRoll - LageKorrekturRoll; |
433 | Mess_IntegralRoll += MesswertRoll + TrimRoll - LageKorrekturRoll; |
435 | if(Mess_IntegralRoll > Umschlag180Roll) |
434 | if(Mess_IntegralRoll > Umschlag180Roll) |
436 | { |
435 | { |
437 | Mess_IntegralRoll = -(Umschlag180Roll - 25000L); |
436 | Mess_IntegralRoll = -(Umschlag180Roll - 25000L); |
438 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
437 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
439 | } |
438 | } |
440 | if(Mess_IntegralRoll <-Umschlag180Roll) |
439 | if(Mess_IntegralRoll <-Umschlag180Roll) |
441 | { |
440 | { |
442 | Mess_IntegralRoll = (Umschlag180Roll - 25000L); |
441 | Mess_IntegralRoll = (Umschlag180Roll - 25000L); |
443 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
442 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
444 | } |
443 | } |
445 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
444 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
446 | Mess_IntegralNick2 += MesswertNick + TrimNick; |
445 | Mess_IntegralNick2 += MesswertNick + TrimNick; |
447 | Mess_IntegralNick += MesswertNick + TrimNick - LageKorrekturNick; |
446 | Mess_IntegralNick += MesswertNick + TrimNick - LageKorrekturNick; |
448 | if(Mess_IntegralNick > Umschlag180Nick) |
447 | if(Mess_IntegralNick > Umschlag180Nick) |
449 | { |
448 | { |
450 | Mess_IntegralNick = -(Umschlag180Nick - 25000L); |
449 | Mess_IntegralNick = -(Umschlag180Nick - 25000L); |
451 | Mess_IntegralNick2 = Mess_IntegralNick; |
450 | Mess_IntegralNick2 = Mess_IntegralNick; |
452 | } |
451 | } |
453 | if(Mess_IntegralNick <-Umschlag180Nick) |
452 | if(Mess_IntegralNick <-Umschlag180Nick) |
454 | { |
453 | { |
455 | Mess_IntegralNick = (Umschlag180Nick - 25000L); |
454 | Mess_IntegralNick = (Umschlag180Nick - 25000L); |
456 | Mess_IntegralNick2 = Mess_IntegralNick; |
455 | Mess_IntegralNick2 = Mess_IntegralNick; |
457 | } |
456 | } |
458 | 457 | ||
459 | Integral_Gier = Mess_Integral_Gier; |
458 | Integral_Gier = Mess_Integral_Gier; |
460 | IntegralNick = Mess_IntegralNick; |
459 | IntegralNick = Mess_IntegralNick; |
461 | IntegralRoll = Mess_IntegralRoll; |
460 | IntegralRoll = Mess_IntegralRoll; |
462 | IntegralNick2 = Mess_IntegralNick2; |
461 | IntegralNick2 = Mess_IntegralNick2; |
463 | IntegralRoll2 = Mess_IntegralRoll2; |
462 | IntegralRoll2 = Mess_IntegralRoll2; |
464 | 463 | ||
465 | #define D_LIMIT 128 |
464 | #define D_LIMIT 128 |
466 | 465 | ||
467 | MesswertNick = HiResNick / 8; |
466 | MesswertNick = HiResNick / 8; |
468 | MesswertRoll = HiResRoll / 8; |
467 | MesswertRoll = HiResRoll / 8; |
469 | 468 | ||
470 | if(AdWertNick < 15) MesswertNick = -1000; if(AdWertNick < 7) MesswertNick = -2000; |
469 | if(AdWertNick < 15) MesswertNick = -1000; if(AdWertNick < 7) MesswertNick = -2000; |
471 | if(PlatinenVersion == 10) { if(AdWertNick > 1010) MesswertNick = +1000; if(AdWertNick > 1017) MesswertNick = +2000; } |
470 | if(PlatinenVersion == 10) { if(AdWertNick > 1010) MesswertNick = +1000; if(AdWertNick > 1017) MesswertNick = +2000; } |
472 | else { if(AdWertNick > 2000) MesswertNick = +1000; if(AdWertNick > 2015) MesswertNick = +2000; } |
471 | else { if(AdWertNick > 2000) MesswertNick = +1000; if(AdWertNick > 2015) MesswertNick = +2000; } |
473 | if(AdWertRoll < 15) MesswertRoll = -1000; if(AdWertRoll < 7) MesswertRoll = -2000; |
472 | if(AdWertRoll < 15) MesswertRoll = -1000; if(AdWertRoll < 7) MesswertRoll = -2000; |
474 | if(PlatinenVersion == 10) { if(AdWertRoll > 1010) MesswertRoll = +1000; if(AdWertRoll > 1017) MesswertRoll = +2000; } |
473 | if(PlatinenVersion == 10) { if(AdWertRoll > 1010) MesswertRoll = +1000; if(AdWertRoll > 1017) MesswertRoll = +2000; } |
475 | else { if(AdWertRoll > 2000) MesswertRoll = +1000; if(AdWertRoll > 2015) MesswertRoll = +2000; } |
474 | else { if(AdWertRoll > 2000) MesswertRoll = +1000; if(AdWertRoll > 2015) MesswertRoll = +2000; } |
476 | 475 | ||
477 | if(Parameter_Gyro_D) |
476 | if(Parameter_Gyro_D) |
478 | { |
477 | { |
479 | d2Nick = HiResNick - oldNick; |
478 | d2Nick = HiResNick - oldNick; |
480 | oldNick = (oldNick + HiResNick)/2; |
479 | oldNick = (oldNick + HiResNick)/2; |
481 | if(d2Nick > D_LIMIT) d2Nick = D_LIMIT; |
480 | if(d2Nick > D_LIMIT) d2Nick = D_LIMIT; |
482 | else if(d2Nick < -D_LIMIT) d2Nick = -D_LIMIT; |
481 | else if(d2Nick < -D_LIMIT) d2Nick = -D_LIMIT; |
483 | MesswertNick += (d2Nick * (signed int) Parameter_Gyro_D) / 16; |
482 | MesswertNick += (d2Nick * (signed int) Parameter_Gyro_D) / 16; |
484 | d2Roll = HiResRoll - oldRoll; |
483 | d2Roll = HiResRoll - oldRoll; |
485 | oldRoll = (oldRoll + HiResRoll)/2; |
484 | oldRoll = (oldRoll + HiResRoll)/2; |
486 | if(d2Roll > D_LIMIT) d2Roll = D_LIMIT; |
485 | if(d2Roll > D_LIMIT) d2Roll = D_LIMIT; |
487 | else if(d2Roll < -D_LIMIT) d2Roll = -D_LIMIT; |
486 | else if(d2Roll < -D_LIMIT) d2Roll = -D_LIMIT; |
488 | MesswertRoll += (d2Roll * (signed int) Parameter_Gyro_D) / 16; |
487 | MesswertRoll += (d2Roll * (signed int) Parameter_Gyro_D) / 16; |
489 | HiResNick += (d2Nick * (signed int) Parameter_Gyro_D); |
488 | HiResNick += (d2Nick * (signed int) Parameter_Gyro_D); |
490 | HiResRoll += (d2Roll * (signed int) Parameter_Gyro_D); |
489 | HiResRoll += (d2Roll * (signed int) Parameter_Gyro_D); |
491 | } |
490 | } |
492 | 491 | ||
493 | if(RohMesswertRoll > 0) TrimRoll += ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
492 | if(RohMesswertRoll > 0) TrimRoll += ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
494 | else TrimRoll -= ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
493 | else TrimRoll -= ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
495 | if(RohMesswertNick > 0) TrimNick += ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
494 | if(RohMesswertNick > 0) TrimNick += ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
496 | else TrimNick -= ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
495 | else TrimNick -= ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
497 | 496 | ||
498 | if(EE_Parameter.GlobalConfig & CFG_DREHRATEN_BEGRENZER && !Looping_Nick && !Looping_Roll) |
497 | if(EE_Parameter.GlobalConfig & CFG_DREHRATEN_BEGRENZER && !Looping_Nick && !Looping_Roll) |
499 | { |
498 | { |
500 | if(RohMesswertNick > 256) MesswertNick += 1 * (RohMesswertNick - 256); |
499 | if(RohMesswertNick > 256) MesswertNick += 1 * (RohMesswertNick - 256); |
501 | else if(RohMesswertNick < -256) MesswertNick += 1 * (RohMesswertNick + 256); |
500 | else if(RohMesswertNick < -256) MesswertNick += 1 * (RohMesswertNick + 256); |
502 | if(RohMesswertRoll > 256) MesswertRoll += 1 * (RohMesswertRoll - 256); |
501 | if(RohMesswertRoll > 256) MesswertRoll += 1 * (RohMesswertRoll - 256); |
503 | else if(RohMesswertRoll < -256) MesswertRoll += 1 * (RohMesswertRoll + 256); |
502 | else if(RohMesswertRoll < -256) MesswertRoll += 1 * (RohMesswertRoll + 256); |
504 | } |
503 | } |
505 | for(i=0;i<8;i++) |
504 | for(i=0;i<8;i++) |
506 | { |
505 | { |
507 | int tmp; |
506 | int tmp; |
508 | tmp = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
507 | tmp = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
509 | if(tmp > 255) tmp = 255; else if(tmp < 0) tmp = 0; |
508 | if(tmp > 255) tmp = 255; else if(tmp < 0) tmp = 0; |
510 | if(tmp != Poti[i]) |
509 | if(tmp != Poti[i]) |
511 | { |
510 | { |
512 | Poti[i] += (tmp - Poti[i]) / 8; |
511 | Poti[i] += (tmp - Poti[i]) / 8; |
513 | if(Poti[i] > tmp) Poti[i]--; |
512 | if(Poti[i] > tmp) Poti[i]--; |
514 | else Poti[i]++; |
513 | else Poti[i]++; |
515 | } |
514 | } |
516 | } |
515 | } |
517 | } |
516 | } |
518 | 517 | ||
519 | //############################################################################ |
518 | //############################################################################ |
520 | // Senden der Motorwerte per I2C-Bus |
519 | // Senden der Motorwerte per I2C-Bus |
521 | void SendMotorData(void) |
520 | void SendMotorData(void) |
522 | //############################################################################ |
521 | //############################################################################ |
523 | { |
522 | { |
524 | unsigned char i; |
523 | unsigned char i; |
525 | if(!MotorenEin) |
524 | if(!MotorenEin) |
526 | { |
525 | { |
527 | FCFlags &= ~(FCFLAG_MOTOR_RUN | FCFLAG_FLY); |
526 | FCFlags &= ~(FCFLAG_MOTOR_RUN | FCFLAG_FLY); |
528 | for(i=0;i<MAX_MOTORS;i++) |
527 | for(i=0;i<MAX_MOTORS;i++) |
529 | { |
528 | { |
530 | if(!PC_MotortestActive) MotorTest[i] = 0; |
529 | if(!PC_MotortestActive) MotorTest[i] = 0; |
531 | Motor[i].SetPoint = MotorTest[i]; |
530 | Motor[i].SetPoint = MotorTest[i]; |
532 | Motor[i].SetPointLowerBits = 0; |
531 | Motor[i].SetPointLowerBits = 0; |
533 | /* |
532 | /* |
534 | Motor[i].SetPoint = MotorTest[i] / 4; |
533 | Motor[i].SetPoint = MotorTest[i] / 4; |
535 | Motor[i].SetPointLowerBits = MotorTest[i] % 4; |
534 | Motor[i].SetPointLowerBits = MotorTest[i] % 4; |
536 | */ |
535 | */ |
537 | } |
536 | } |
538 | if(PC_MotortestActive) PC_MotortestActive--; |
537 | if(PC_MotortestActive) PC_MotortestActive--; |
539 | } |
538 | } |
540 | else FCFlags |= FCFLAG_MOTOR_RUN; |
539 | else FCFlags |= FCFLAG_MOTOR_RUN; |
541 | 540 | ||
542 | DebugOut.Analog[12] = Motor[0].SetPoint; |
541 | DebugOut.Analog[12] = Motor[0].SetPoint; |
543 | DebugOut.Analog[13] = Motor[1].SetPoint; |
542 | DebugOut.Analog[13] = Motor[1].SetPoint; |
544 | DebugOut.Analog[14] = Motor[2].SetPoint; |
543 | DebugOut.Analog[14] = Motor[2].SetPoint; |
545 | DebugOut.Analog[15] = Motor[3].SetPoint; |
544 | DebugOut.Analog[15] = Motor[3].SetPoint; |
546 | 545 | ||
547 | //Start I2C Interrupt Mode |
546 | //Start I2C Interrupt Mode |
548 | twi_state = 0; |
547 | twi_state = 0; |
549 | motor = 0; |
548 | motor = 0; |
550 | I2C_Start(); |
549 | I2C_Start(); |
551 | } |
550 | } |
552 | 551 | ||
553 | 552 | ||
554 | 553 | ||
555 | //############################################################################ |
554 | //############################################################################ |
556 | // Trägt ggf. das Poti als Parameter ein |
555 | // Trägt ggf. das Poti als Parameter ein |
557 | void ParameterZuordnung(void) |
556 | void ParameterZuordnung(void) |
558 | //############################################################################ |
557 | //############################################################################ |
559 | { |
558 | { |
560 | 559 | ||
561 | #define CHK_POTI(b,a) {if(a < 248) b = a; else b = Poti[255 - a];} |
560 | #define CHK_POTI(b,a) {if(a < 248) b = a; else b = Poti[255 - a];} |
562 | #define CHK_POTI_MM(b,a,min,max) {CHK_POTI(b,a); LIMIT_MIN_MAX(b, min, max);} |
561 | #define CHK_POTI_MM(b,a,min,max) {CHK_POTI(b,a); LIMIT_MIN_MAX(b, min, max);} |
563 | 562 | ||
564 | CHK_POTI_MM(Parameter_Luftdruck_D,EE_Parameter.Luftdruck_D,0,100); |
563 | CHK_POTI_MM(Parameter_Luftdruck_D,EE_Parameter.Luftdruck_D,0,100); |
565 | CHK_POTI_MM(Parameter_Hoehe_P,EE_Parameter.Hoehe_P,0,100); |
564 | CHK_POTI_MM(Parameter_Hoehe_P,EE_Parameter.Hoehe_P,0,100); |
566 | CHK_POTI_MM(Parameter_Gyro_P,EE_Parameter.Gyro_P,10,255); |
565 | CHK_POTI_MM(Parameter_Gyro_P,EE_Parameter.Gyro_P,10,255); |
567 | CHK_POTI_MM(Parameter_J16Timing,EE_Parameter.J16Timing,1,255); |
566 | CHK_POTI_MM(Parameter_J16Timing,EE_Parameter.J16Timing,1,255); |
568 | CHK_POTI_MM(Parameter_J17Timing,EE_Parameter.J17Timing,1,255); |
567 | CHK_POTI_MM(Parameter_J17Timing,EE_Parameter.J17Timing,1,255); |
569 | CHK_POTI(Parameter_Servo3,EE_Parameter.Servo3); |
568 | CHK_POTI(Parameter_Servo3,EE_Parameter.Servo3); |
570 | CHK_POTI(Parameter_Servo4,EE_Parameter.Servo4); |
569 | CHK_POTI(Parameter_Servo4,EE_Parameter.Servo4); |
571 | CHK_POTI(Parameter_Servo5,EE_Parameter.Servo5); |
570 | CHK_POTI(Parameter_Servo5,EE_Parameter.Servo5); |
572 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
571 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
573 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
572 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
574 | CHK_POTI(Parameter_Hoehe_ACC_Wirkung,EE_Parameter.Hoehe_ACC_Wirkung); |
573 | CHK_POTI(Parameter_Hoehe_ACC_Wirkung,EE_Parameter.Hoehe_ACC_Wirkung); |
575 | CHK_POTI(Parameter_Hoehe_GPS_Z,EE_Parameter.Hoehe_GPS_Z); |
574 | CHK_POTI(Parameter_Hoehe_GPS_Z,EE_Parameter.Hoehe_GPS_Z); |
576 | CHK_POTI(Parameter_KompassWirkung,EE_Parameter.KompassWirkung); |
575 | CHK_POTI(Parameter_KompassWirkung,EE_Parameter.KompassWirkung); |
577 | CHK_POTI(Parameter_Gyro_I,EE_Parameter.Gyro_I); |
576 | CHK_POTI(Parameter_Gyro_I,EE_Parameter.Gyro_I); |
578 | CHK_POTI(Parameter_Gyro_D,EE_Parameter.Gyro_D); |
577 | CHK_POTI(Parameter_Gyro_D,EE_Parameter.Gyro_D); |
579 | CHK_POTI(Parameter_Gyro_Gier_P,EE_Parameter.Gyro_Gier_P); |
578 | CHK_POTI(Parameter_Gyro_Gier_P,EE_Parameter.Gyro_Gier_P); |
580 | CHK_POTI(Parameter_Gyro_Gier_I,EE_Parameter.Gyro_Gier_I); |
579 | CHK_POTI(Parameter_Gyro_Gier_I,EE_Parameter.Gyro_Gier_I); |
581 | CHK_POTI(Parameter_I_Faktor,EE_Parameter.I_Faktor); |
580 | CHK_POTI(Parameter_I_Faktor,EE_Parameter.I_Faktor); |
582 | CHK_POTI(Parameter_UserParam1,EE_Parameter.UserParam1); |
581 | CHK_POTI(Parameter_UserParam1,EE_Parameter.UserParam1); |
583 | CHK_POTI(Parameter_UserParam2,EE_Parameter.UserParam2); |
582 | CHK_POTI(Parameter_UserParam2,EE_Parameter.UserParam2); |
584 | CHK_POTI(Parameter_UserParam3,EE_Parameter.UserParam3); |
583 | CHK_POTI(Parameter_UserParam3,EE_Parameter.UserParam3); |
585 | CHK_POTI(Parameter_UserParam4,EE_Parameter.UserParam4); |
584 | CHK_POTI(Parameter_UserParam4,EE_Parameter.UserParam4); |
586 | CHK_POTI(Parameter_UserParam5,EE_Parameter.UserParam5); |
585 | CHK_POTI(Parameter_UserParam5,EE_Parameter.UserParam5); |
587 | CHK_POTI(Parameter_UserParam6,EE_Parameter.UserParam6); |
586 | CHK_POTI(Parameter_UserParam6,EE_Parameter.UserParam6); |
588 | CHK_POTI(Parameter_UserParam7,EE_Parameter.UserParam7); |
587 | CHK_POTI(Parameter_UserParam7,EE_Parameter.UserParam7); |
589 | CHK_POTI(Parameter_UserParam8,EE_Parameter.UserParam8); |
588 | CHK_POTI(Parameter_UserParam8,EE_Parameter.UserParam8); |
590 | CHK_POTI(Parameter_ServoNickControl,EE_Parameter.ServoNickControl); |
589 | CHK_POTI(Parameter_ServoNickControl,EE_Parameter.ServoNickControl); |
591 | CHK_POTI(Parameter_ServoRollControl,EE_Parameter.ServoRollControl); |
590 | CHK_POTI(Parameter_ServoRollControl,EE_Parameter.ServoRollControl); |
592 | CHK_POTI(Parameter_LoopGasLimit,EE_Parameter.LoopGasLimit); |
591 | CHK_POTI(Parameter_LoopGasLimit,EE_Parameter.LoopGasLimit); |
593 | CHK_POTI(Parameter_AchsKopplung1, EE_Parameter.AchsKopplung1); |
592 | CHK_POTI(Parameter_AchsKopplung1, EE_Parameter.AchsKopplung1); |
594 | CHK_POTI(Parameter_AchsKopplung2, EE_Parameter.AchsKopplung2); |
593 | CHK_POTI(Parameter_AchsKopplung2, EE_Parameter.AchsKopplung2); |
595 | CHK_POTI(Parameter_CouplingYawCorrection,EE_Parameter.CouplingYawCorrection); |
594 | CHK_POTI(Parameter_CouplingYawCorrection,EE_Parameter.CouplingYawCorrection); |
596 | // CHK_POTI(Parameter_AchsGegenKopplung1,EE_Parameter.AchsGegenKopplung1,0,255); |
595 | // CHK_POTI(Parameter_AchsGegenKopplung1,EE_Parameter.AchsGegenKopplung1,0,255); |
597 | CHK_POTI(Parameter_DynamicStability,EE_Parameter.DynamicStability); |
596 | CHK_POTI(Parameter_DynamicStability,EE_Parameter.DynamicStability); |
598 | CHK_POTI(Parameter_ExternalControl,EE_Parameter.ExternalControl); |
597 | CHK_POTI(Parameter_ExternalControl,EE_Parameter.ExternalControl); |
599 | Ki = (10300 / 2) / (Parameter_I_Faktor + 1); |
598 | Ki = (10300 / 2) / (Parameter_I_Faktor + 1); |
600 | MAX_GAS = EE_Parameter.Gas_Max; |
599 | MAX_GAS = EE_Parameter.Gas_Max; |
601 | MIN_GAS = EE_Parameter.Gas_Min; |
600 | MIN_GAS = EE_Parameter.Gas_Min; |
602 | if(Poti4 > 50) HeadFree = 1; else HeadFree = 0; |
601 | if(Poti4 > 50) HeadFree = 1; else HeadFree = 0; |
603 | if(HeadFree) {if(Parameter_AchsKopplung1 < 210) Parameter_AchsKopplung1 += 30;} |
602 | if(HeadFree) {if(Parameter_AchsKopplung1 < 210) Parameter_AchsKopplung1 += 30;} |
604 | } |
603 | } |
605 | 604 | ||
606 | //############################################################################ |
605 | //############################################################################ |
607 | // |
606 | // |
608 | void MotorRegler(void) |
607 | void MotorRegler(void) |
609 | //############################################################################ |
608 | //############################################################################ |
610 | { |
609 | { |
611 | int pd_ergebnis_nick,pd_ergebnis_roll,tmp_int, tmp_int2; |
610 | int pd_ergebnis_nick,pd_ergebnis_roll,tmp_int, tmp_int2; |
612 | int GierMischanteil,GasMischanteil; |
611 | int GierMischanteil,GasMischanteil; |
613 | static long SummeNick=0,SummeRoll=0; |
612 | static long SummeNick=0,SummeRoll=0; |
614 | static long sollGier = 0,tmp_long,tmp_long2; |
613 | static long sollGier = 0,tmp_long,tmp_long2; |
615 | static long IntegralFehlerNick = 0; |
614 | static long IntegralFehlerNick = 0; |
616 | static long IntegralFehlerRoll = 0; |
615 | static long IntegralFehlerRoll = 0; |
617 | static unsigned int RcLostTimer; |
616 | static unsigned int RcLostTimer; |
618 | static unsigned char delay_neutral = 0; |
617 | static unsigned char delay_neutral = 0; |
619 | static unsigned char delay_einschalten = 0,delay_ausschalten = 0; |
618 | static unsigned char delay_einschalten = 0,delay_ausschalten = 0; |
620 | static unsigned char calibration_done = 0; |
619 | static unsigned char calibration_done = 0; |
621 | static char NeueKompassRichtungMerken = 0; |
620 | static char NeueKompassRichtungMerken = 0; |
622 | static long ausgleichNick, ausgleichRoll; |
621 | static long ausgleichNick, ausgleichRoll; |
623 | int IntegralNickMalFaktor,IntegralRollMalFaktor; |
622 | int IntegralNickMalFaktor,IntegralRollMalFaktor; |
624 | unsigned char i; |
623 | unsigned char i; |
625 | Mittelwert(); |
624 | Mittelwert(); |
626 | GRN_ON; |
625 | GRN_ON; |
627 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
626 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
628 | // Gaswert ermitteln |
627 | // Gaswert ermitteln |
629 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
628 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
630 | GasMischanteil = StickGas; |
629 | GasMischanteil = StickGas; |
631 | if(GasMischanteil < MIN_GAS + 10) GasMischanteil = MIN_GAS + 10; |
630 | if(GasMischanteil < MIN_GAS + 10) GasMischanteil = MIN_GAS + 10; |
632 | 631 | ||
633 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
632 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
634 | // Empfang schlecht |
633 | // Empfang schlecht |
635 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
634 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
636 | if(SenderOkay < 100) |
635 | if(SenderOkay < 100) |
637 | { |
636 | { |
638 | if(RcLostTimer) RcLostTimer--; |
637 | if(RcLostTimer) RcLostTimer--; |
639 | else |
638 | else |
640 | { |
639 | { |
641 | MotorenEin = 0; |
640 | MotorenEin = 0; |
642 | FCFlags &= ~FCFLAG_NOTLANDUNG; |
641 | FCFlags &= ~FCFLAG_NOTLANDUNG; |
643 | } |
642 | } |
644 | ROT_ON; |
643 | ROT_ON; |
645 | if(modell_fliegt > 1000) // wahrscheinlich in der Luft --> langsam absenken |
644 | if(modell_fliegt > 1000) // wahrscheinlich in der Luft --> langsam absenken |
646 | { |
645 | { |
647 | GasMischanteil = EE_Parameter.NotGas; |
646 | GasMischanteil = EE_Parameter.NotGas; |
648 | FCFlags |= FCFLAG_NOTLANDUNG; |
647 | FCFlags |= FCFLAG_NOTLANDUNG; |
649 | PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
648 | PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
650 | PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
649 | PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
651 | PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
650 | PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
652 | PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
651 | PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
653 | PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] = 0; |
652 | PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] = 0; |
654 | } |
653 | } |
655 | else MotorenEin = 0; |
654 | else MotorenEin = 0; |
656 | } |
655 | } |
657 | else |
656 | else |
658 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
657 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
659 | // Emfang gut |
658 | // Emfang gut |
660 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
659 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
661 | if(SenderOkay > 140) |
660 | if(SenderOkay > 140) |
662 | { |
661 | { |
663 | FCFlags &= ~FCFLAG_NOTLANDUNG; |
662 | FCFlags &= ~FCFLAG_NOTLANDUNG; |
664 | RcLostTimer = EE_Parameter.NotGasZeit * 50; |
663 | RcLostTimer = EE_Parameter.NotGasZeit * 50; |
665 | if(GasMischanteil > 40 && MotorenEin) |
664 | if(GasMischanteil > 40 && MotorenEin) |
666 | { |
665 | { |
667 | if(modell_fliegt < 0xffff) modell_fliegt++; |
666 | if(modell_fliegt < 0xffff) modell_fliegt++; |
668 | } |
667 | } |
669 | if((modell_fliegt < 256)) |
668 | if((modell_fliegt < 256)) |
670 | { |
669 | { |
671 | SummeNick = 0; |
670 | SummeNick = 0; |
672 | SummeRoll = 0; |
671 | SummeRoll = 0; |
673 | if(modell_fliegt == 250) |
672 | if(modell_fliegt == 250) |
674 | { |
673 | { |
675 | NeueKompassRichtungMerken = 1; |
674 | NeueKompassRichtungMerken = 1; |
676 | sollGier = 0; |
675 | sollGier = 0; |
677 | Mess_Integral_Gier = 0; |
676 | Mess_Integral_Gier = 0; |
678 | // Mess_Integral_Gier2 = 0; |
677 | // Mess_Integral_Gier2 = 0; |
679 | } |
678 | } |
680 | } else FCFlags |= FCFLAG_FLY; |
679 | } else FCFlags |= FCFLAG_FLY; |
681 | 680 | ||
682 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] > 80) && MotorenEin == 0) |
681 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] > 80) && MotorenEin == 0) |
683 | { |
682 | { |
684 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
683 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
685 | // auf Nullwerte kalibrieren |
684 | // auf Nullwerte kalibrieren |
686 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
685 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
687 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) // Neutralwerte |
686 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) // Neutralwerte |
688 | { |
687 | { |
689 | if(++delay_neutral > 200) // nicht sofort |
688 | if(++delay_neutral > 200) // nicht sofort |
690 | { |
689 | { |
691 | GRN_OFF; |
690 | GRN_OFF; |
692 | MotorenEin = 0; |
691 | MotorenEin = 0; |
693 | delay_neutral = 0; |
692 | delay_neutral = 0; |
694 | modell_fliegt = 0; |
693 | modell_fliegt = 0; |
695 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) > 70) |
694 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) > 70) |
696 | { |
695 | { |
697 | unsigned char setting=1; |
696 | unsigned char setting=1; |
698 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 1; |
697 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 1; |
699 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 2; |
698 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 2; |
700 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 3; |
699 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 3; |
701 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 4; |
700 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 4; |
702 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 5; |
701 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 5; |
703 | SetActiveParamSet(setting); // aktiven Datensatz merken |
702 | SetActiveParamSet(setting); // aktiven Datensatz merken |
704 | } |
703 | } |
705 | // else |
704 | // else |
706 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 30 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -70) |
705 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 30 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -70) |
707 | { |
706 | { |
708 | WinkelOut.CalcState = 1; |
707 | WinkelOut.CalcState = 1; |
709 | beeptime = 1000; |
708 | beeptime = 1000; |
710 | } |
709 | } |
711 | else |
710 | else |
712 | { |
711 | { |
713 | ParamSet_ReadFromEEProm(GetActiveParamSet()); |
712 | ParamSet_ReadFromEEProm(GetActiveParamSet()); |
714 | LipoDetection(0); |
713 | LipoDetection(0); |
715 | LIBFC_ReceiverInit(EE_Parameter.Receiver); |
714 | LIBFC_ReceiverInit(EE_Parameter.Receiver); |
716 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
715 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
717 | { |
716 | { |
718 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
717 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
719 | } |
718 | } |
720 | ServoActive = 0; |
719 | ServoActive = 0; |
721 | SetNeutral(0); |
720 | SetNeutral(0); |
722 | calibration_done = 1; |
721 | calibration_done = 1; |
723 | ServoActive = 1; |
722 | ServoActive = 1; |
724 | DDRD |=0x80; // enable J7 -> Servo signal |
723 | DDRD |=0x80; // enable J7 -> Servo signal |
725 | Piep(GetActiveParamSet(),120); |
724 | Piep(GetActiveParamSet(),120); |
726 | } |
725 | } |
727 | } |
726 | } |
728 | } |
727 | } |
729 | else |
728 | else |
730 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) // ACC Neutralwerte speichern |
729 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) // ACC Neutralwerte speichern |
731 | { |
730 | { |
732 | if(++delay_neutral > 200) // nicht sofort |
731 | if(++delay_neutral > 200) // nicht sofort |
733 | { |
732 | { |
734 | GRN_OFF; |
733 | GRN_OFF; |
735 | MotorenEin = 0; |
734 | MotorenEin = 0; |
736 | delay_neutral = 0; |
735 | delay_neutral = 0; |
737 | modell_fliegt = 0; |
736 | modell_fliegt = 0; |
738 | SetNeutral(1); |
737 | SetNeutral(1); |
739 | calibration_done = 1; |
738 | calibration_done = 1; |
740 | Piep(GetActiveParamSet(),120); |
739 | Piep(GetActiveParamSet(),120); |
741 | } |
740 | } |
742 | } |
741 | } |
743 | else delay_neutral = 0; |
742 | else delay_neutral = 0; |
744 | } |
743 | } |
745 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
744 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
746 | // Gas ist unten |
745 | // Gas ist unten |
747 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
746 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
748 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] < 35-120) |
747 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] < 35-120) |
749 | { |
748 | { |
750 | // Motoren Starten |
749 | // Motoren Starten |
751 | if(!MotorenEin) |
750 | if(!MotorenEin) |
752 | { |
751 | { |
753 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) |
752 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) |
754 | { |
753 | { |
755 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
754 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
756 | // Einschalten |
755 | // Einschalten |
757 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
756 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
758 | if(++delay_einschalten > 200) |
757 | if(++delay_einschalten > 200) |
759 | { |
758 | { |
760 | delay_einschalten = 0; |
759 | delay_einschalten = 0; |
761 | if(calibration_done) |
760 | if(calibration_done) |
762 | { |
761 | { |
763 | modell_fliegt = 1; |
762 | modell_fliegt = 1; |
764 | MotorenEin = 1; |
763 | MotorenEin = 1; |
765 | sollGier = 0; |
764 | sollGier = 0; |
766 | Mess_Integral_Gier = 0; |
765 | Mess_Integral_Gier = 0; |
767 | Mess_Integral_Gier2 = 0; |
766 | Mess_Integral_Gier2 = 0; |
768 | Mess_IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
767 | Mess_IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
769 | Mess_IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
768 | Mess_IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
770 | Mess_IntegralNick2 = IntegralNick; |
769 | Mess_IntegralNick2 = IntegralNick; |
771 | Mess_IntegralRoll2 = IntegralRoll; |
770 | Mess_IntegralRoll2 = IntegralRoll; |
772 | SummeNick = 0; |
771 | SummeNick = 0; |
773 | SummeRoll = 0; |
772 | SummeRoll = 0; |
774 | FCFlags |= FCFLAG_START; |
773 | FCFlags |= FCFLAG_START; |
- | 774 | ControlHeading = KompassValue / 15; |
|
775 | } |
775 | } |
776 | else |
776 | else |
777 | { |
777 | { |
778 | beeptime = 1500; // indicate missing calibration |
778 | beeptime = 1500; // indicate missing calibration |
779 | } |
779 | } |
780 | } |
780 | } |
781 | } |
781 | } |
782 | else delay_einschalten = 0; |
782 | else delay_einschalten = 0; |
783 | } |
783 | } |
784 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
784 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
785 | // Auschalten |
785 | // Auschalten |
786 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
786 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
787 | else // only if motors are running |
787 | else // only if motors are running |
788 | { |
788 | { |
789 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) |
789 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) |
790 | { |
790 | { |
791 | if(++delay_ausschalten > 200) // nicht sofort |
791 | if(++delay_ausschalten > 200) // nicht sofort |
792 | { |
792 | { |
793 | MotorenEin = 0; |
793 | MotorenEin = 0; |
794 | delay_ausschalten = 0; |
794 | delay_ausschalten = 0; |
795 | modell_fliegt = 0; |
795 | modell_fliegt = 0; |
796 | } |
796 | } |
797 | } |
797 | } |
798 | else delay_ausschalten = 0; |
798 | else delay_ausschalten = 0; |
799 | } |
799 | } |
800 | } |
800 | } |
801 | } |
801 | } |
802 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
802 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
803 | // neue Werte von der Funke |
803 | // neue Werte von der Funke |
804 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
804 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
805 | 805 | ||
806 | if(!NewPpmData-- || (FCFlags & FCFLAG_NOTLANDUNG)) |
806 | if(!NewPpmData-- || (FCFlags & FCFLAG_NOTLANDUNG)) |
807 | { |
807 | { |
808 | static int stick_nick,stick_roll; |
808 | static int stick_nick,stick_roll; |
809 | 809 | ||
810 | unsigned char angle = 180/15; |
810 | unsigned char angle = 180/15; |
811 | signed char sintab[31] = { 0, 4, 8, 11, 14, 16, 16, 16, 14, 11, 8, 4, 0, -4, -8, -11, -14, -16, -16, -16, -14, -11, -8, -4, 0, 4, 8, 11, 14, 16, 16}; |
811 | signed char sintab[31] = { 0, 4, 8, 11, 14, 16, 16, 16, 14, 11, 8, 4, 0, -4, -8, -11, -14, -16, -16, -16, -14, -11, -8, -4, 0, 4, 8, 11, 14, 16, 16}; |
812 | //signed char costab[24] = {16, 16, 14, 11, 8, 4, 0, -4, -8, -11, -14, -16, -16, -16, -14, -11, -8, -4, 0, 4, 8, 11, 14, 16}; |
812 | //signed char costab[24] = {16, 16, 14, 11, 8, 4, 0, -4, -8, -11, -14, -16, -16, -16, -14, -11, -8, -4, 0, 4, 8, 11, 14, 16}; |
813 | angle = (ControlHeading + (360/15) - ErsatzKompass / (GIER_GRAD_FAKTOR * 15)) % 24; |
813 | angle = (ControlHeading + (360/15) - ErsatzKompass / (GIER_GRAD_FAKTOR * 15)) % 24; |
814 | 814 | ||
815 | signed int cos_h, sin_h; |
815 | signed int cos_h, sin_h; |
816 | cos_h = sintab[angle + 6]/2; |
816 | cos_h = sintab[angle + 6]/2; |
817 | sin_h = sintab[angle]/2; |
817 | sin_h = sintab[angle]/2; |
818 | 818 | ||
819 | ParameterZuordnung(); |
819 | ParameterZuordnung(); |
820 | stick_nick = (stick_nick * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_P) / 4; |
820 | stick_nick = (stick_nick * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_P) / 4; |
821 | stick_nick += PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_D; |
821 | stick_nick += PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_D; |
822 | stick_roll = (stick_roll * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_P) / 4; |
822 | stick_roll = (stick_roll * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_P) / 4; |
823 | stick_roll += PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_D; |
823 | stick_roll += PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_D; |
824 | 824 | ||
825 | if(HeadFree) |
825 | if(HeadFree) |
826 | { |
826 | { |
827 | StickNick = ((cos_h * stick_nick) + (sin_h * stick_roll))/8; |
827 | StickNick = ((cos_h * stick_nick) + (sin_h * stick_roll))/8; |
828 | StickRoll = ((cos_h * stick_roll) - (sin_h * stick_nick))/8; |
828 | StickRoll = ((cos_h * stick_roll) - (sin_h * stick_nick))/8; |
829 | } |
829 | } |
830 | else |
830 | else |
831 | { |
831 | { |
832 | StickNick = stick_nick; |
832 | StickNick = stick_nick; |
833 | StickRoll = stick_roll; |
833 | StickRoll = stick_roll; |
834 | } |
834 | } |
835 | 835 | ||
836 | StickGier = -PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]; |
836 | StickGier = -PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]; |
837 | if(StickGier > 2) StickGier -= 2; else |
837 | if(StickGier > 2) StickGier -= 2; else |
838 | if(StickGier < -2) StickGier += 2; else StickGier = 0; |
838 | if(StickGier < -2) StickGier += 2; else StickGier = 0; |
839 | 839 | ||
840 | StickNick -= (GPS_Nick + GPS_Nick2); |
840 | StickNick -= (GPS_Nick + GPS_Nick2); |
841 | StickRoll -= (GPS_Roll + GPS_Roll2); |
841 | StickRoll -= (GPS_Roll + GPS_Roll2); |
842 | StickGas = PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] + 120; |
842 | StickGas = PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] + 120; |
843 | 843 | ||
844 | GyroFaktor = (Parameter_Gyro_P + 10.0); |
844 | GyroFaktor = (Parameter_Gyro_P + 10.0); |
845 | IntegralFaktor = Parameter_Gyro_I; |
845 | IntegralFaktor = Parameter_Gyro_I; |
846 | GyroFaktorGier = (Parameter_Gyro_Gier_P + 10.0); |
846 | GyroFaktorGier = (Parameter_Gyro_Gier_P + 10.0); |
847 | IntegralFaktorGier = Parameter_Gyro_Gier_I; |
847 | IntegralFaktorGier = Parameter_Gyro_Gier_I; |
848 | 848 | ||
849 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
849 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
850 | //+ Analoge Steuerung per Seriell |
850 | //+ Analoge Steuerung per Seriell |
851 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
851 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
852 | if(ExternControl.Config & 0x01 && Parameter_ExternalControl > 128) |
852 | if(ExternControl.Config & 0x01 && Parameter_ExternalControl > 128) |
853 | { |
853 | { |
854 | StickNick += (int) ExternControl.Nick * (int) EE_Parameter.Stick_P; |
854 | StickNick += (int) ExternControl.Nick * (int) EE_Parameter.Stick_P; |
855 | StickRoll += (int) ExternControl.Roll * (int) EE_Parameter.Stick_P; |
855 | StickRoll += (int) ExternControl.Roll * (int) EE_Parameter.Stick_P; |
856 | StickGier += ExternControl.Gier; |
856 | StickGier += ExternControl.Gier; |
857 | ExternHoehenValue = (int) ExternControl.Hight * (int)EE_Parameter.Hoehe_Verstaerkung; |
857 | ExternHoehenValue = (int) ExternControl.Hight * (int)EE_Parameter.Hoehe_Verstaerkung; |
858 | if(ExternControl.Gas < StickGas) StickGas = ExternControl.Gas; |
858 | if(ExternControl.Gas < StickGas) StickGas = ExternControl.Gas; |
859 | } |
859 | } |
860 | if(StickGas < 0) StickGas = 0; |
860 | if(StickGas < 0) StickGas = 0; |
861 | 861 | ||
862 | if(EE_Parameter.GlobalConfig & CFG_HEADING_HOLD) IntegralFaktor = 0; |
862 | if(EE_Parameter.GlobalConfig & CFG_HEADING_HOLD) IntegralFaktor = 0; |
863 | //if(GyroFaktor < 0) GyroFaktor = 0; |
863 | //if(GyroFaktor < 0) GyroFaktor = 0; |
864 | //if(IntegralFaktor < 0) IntegralFaktor = 0; |
864 | //if(IntegralFaktor < 0) IntegralFaktor = 0; |
865 | 865 | ||
866 | if(abs(StickNick/STICK_GAIN) > MaxStickNick) |
866 | if(abs(StickNick/STICK_GAIN) > MaxStickNick) |
867 | { |
867 | { |
868 | MaxStickNick = abs(StickNick)/STICK_GAIN; |
868 | MaxStickNick = abs(StickNick)/STICK_GAIN; |
869 | if(MaxStickNick > 100) MaxStickNick = 100; |
869 | if(MaxStickNick > 100) MaxStickNick = 100; |
870 | } |
870 | } |
871 | else MaxStickNick--; |
871 | else MaxStickNick--; |
872 | if(abs(StickRoll/STICK_GAIN) > MaxStickRoll) |
872 | if(abs(StickRoll/STICK_GAIN) > MaxStickRoll) |
873 | { |
873 | { |
874 | MaxStickRoll = abs(StickRoll)/STICK_GAIN; |
874 | MaxStickRoll = abs(StickRoll)/STICK_GAIN; |
875 | if(MaxStickRoll > 100) MaxStickRoll = 100; |
875 | if(MaxStickRoll > 100) MaxStickRoll = 100; |
876 | } |
876 | } |
877 | else MaxStickRoll--; |
877 | else MaxStickRoll--; |
878 | if(FCFlags & FCFLAG_NOTLANDUNG) {MaxStickNick = 0; MaxStickRoll = 0;} |
878 | if(FCFlags & FCFLAG_NOTLANDUNG) {MaxStickNick = 0; MaxStickRoll = 0;} |
879 | 879 | ||
880 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
880 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
881 | // Looping? |
881 | // Looping? |
882 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
882 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
883 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_LINKS) Looping_Links = 1; |
883 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_LINKS) Looping_Links = 1; |
884 | else |
884 | else |
885 | { |
885 | { |
886 | { |
886 | { |
887 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Links = 0; |
887 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Links = 0; |
888 | } |
888 | } |
889 | } |
889 | } |
890 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_RECHTS) Looping_Rechts = 1; |
890 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_RECHTS) Looping_Rechts = 1; |
891 | else |
891 | else |
892 | { |
892 | { |
893 | if(Looping_Rechts) // Hysterese |
893 | if(Looping_Rechts) // Hysterese |
894 | { |
894 | { |
895 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Rechts = 0; |
895 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Rechts = 0; |
896 | } |
896 | } |
897 | } |
897 | } |
898 | 898 | ||
899 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_OBEN) Looping_Oben = 1; |
899 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_OBEN) Looping_Oben = 1; |
900 | else |
900 | else |
901 | { |
901 | { |
902 | if(Looping_Oben) // Hysterese |
902 | if(Looping_Oben) // Hysterese |
903 | { |
903 | { |
904 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Oben = 0; |
904 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Oben = 0; |
905 | } |
905 | } |
906 | } |
906 | } |
907 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_UNTEN) Looping_Unten = 1; |
907 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_UNTEN) Looping_Unten = 1; |
908 | else |
908 | else |
909 | { |
909 | { |
910 | if(Looping_Unten) // Hysterese |
910 | if(Looping_Unten) // Hysterese |
911 | { |
911 | { |
912 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Unten = 0; |
912 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Unten = 0; |
913 | } |
913 | } |
914 | } |
914 | } |
915 | 915 | ||
916 | if(Looping_Links || Looping_Rechts) Looping_Roll = 1; else Looping_Roll = 0; |
916 | if(Looping_Links || Looping_Rechts) Looping_Roll = 1; else Looping_Roll = 0; |
917 | if(Looping_Oben || Looping_Unten) { Looping_Nick = 1; Looping_Roll = 0; Looping_Links = 0; Looping_Rechts = 0;} else Looping_Nick = 0; |
917 | if(Looping_Oben || Looping_Unten) { Looping_Nick = 1; Looping_Roll = 0; Looping_Links = 0; Looping_Rechts = 0;} else Looping_Nick = 0; |
918 | } // Ende neue Funken-Werte |
918 | } // Ende neue Funken-Werte |
919 | 919 | ||
920 | if(Looping_Roll || Looping_Nick) |
920 | if(Looping_Roll || Looping_Nick) |
921 | { |
921 | { |
922 | if(GasMischanteil > EE_Parameter.LoopGasLimit) GasMischanteil = EE_Parameter.LoopGasLimit; |
922 | if(GasMischanteil > EE_Parameter.LoopGasLimit) GasMischanteil = EE_Parameter.LoopGasLimit; |
923 | TrichterFlug = 1; |
923 | TrichterFlug = 1; |
924 | } |
924 | } |
925 | 925 | ||
926 | 926 | ||
927 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
927 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
928 | // Bei Empfangsausfall im Flug |
928 | // Bei Empfangsausfall im Flug |
929 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
929 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
930 | if(FCFlags & FCFLAG_NOTLANDUNG) |
930 | if(FCFlags & FCFLAG_NOTLANDUNG) |
931 | { |
931 | { |
932 | StickGier = 0; |
932 | StickGier = 0; |
933 | StickNick = 0; |
933 | StickNick = 0; |
934 | StickRoll = 0; |
934 | StickRoll = 0; |
935 | GyroFaktor = 90; |
935 | GyroFaktor = 90; |
936 | IntegralFaktor = 120; |
936 | IntegralFaktor = 120; |
937 | GyroFaktorGier = 90; |
937 | GyroFaktorGier = 90; |
938 | IntegralFaktorGier = 120; |
938 | IntegralFaktorGier = 120; |
939 | Looping_Roll = 0; |
939 | Looping_Roll = 0; |
940 | Looping_Nick = 0; |
940 | Looping_Nick = 0; |
941 | } |
941 | } |
942 | 942 | ||
943 | 943 | ||
944 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
944 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
945 | // Integrale auf ACC-Signal abgleichen |
945 | // Integrale auf ACC-Signal abgleichen |
946 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
946 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
947 | #define ABGLEICH_ANZAHL 256L |
947 | #define ABGLEICH_ANZAHL 256L |
948 | 948 | ||
949 | MittelIntegralNick += IntegralNick; // Für die Mittelwertbildung aufsummieren |
949 | MittelIntegralNick += IntegralNick; // Für die Mittelwertbildung aufsummieren |
950 | MittelIntegralRoll += IntegralRoll; |
950 | MittelIntegralRoll += IntegralRoll; |
951 | MittelIntegralNick2 += IntegralNick2; |
951 | MittelIntegralNick2 += IntegralNick2; |
952 | MittelIntegralRoll2 += IntegralRoll2; |
952 | MittelIntegralRoll2 += IntegralRoll2; |
953 | 953 | ||
954 | if(Looping_Nick || Looping_Roll) |
954 | if(Looping_Nick || Looping_Roll) |
955 | { |
955 | { |
956 | IntegralAccNick = 0; |
956 | IntegralAccNick = 0; |
957 | IntegralAccRoll = 0; |
957 | IntegralAccRoll = 0; |
958 | MittelIntegralNick = 0; |
958 | MittelIntegralNick = 0; |
959 | MittelIntegralRoll = 0; |
959 | MittelIntegralRoll = 0; |
960 | MittelIntegralNick2 = 0; |
960 | MittelIntegralNick2 = 0; |
961 | MittelIntegralRoll2 = 0; |
961 | MittelIntegralRoll2 = 0; |
962 | Mess_IntegralNick2 = Mess_IntegralNick; |
962 | Mess_IntegralNick2 = Mess_IntegralNick; |
963 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
963 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
964 | ZaehlMessungen = 0; |
964 | ZaehlMessungen = 0; |
965 | LageKorrekturNick = 0; |
965 | LageKorrekturNick = 0; |
966 | LageKorrekturRoll = 0; |
966 | LageKorrekturRoll = 0; |
967 | } |
967 | } |
968 | 968 | ||
969 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
969 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
970 | if(!Looping_Nick && !Looping_Roll && (Aktuell_az > 512 || MotorenEin)) |
970 | if(!Looping_Nick && !Looping_Roll && (Aktuell_az > 512 || MotorenEin)) |
971 | { |
971 | { |
972 | long tmp_long, tmp_long2; |
972 | long tmp_long, tmp_long2; |
973 | if(FromNaviCtrl_Value.Kalman_K != -1 /*&& !TrichterFlug*/) |
973 | if(FromNaviCtrl_Value.Kalman_K != -1 /*&& !TrichterFlug*/) |
974 | { |
974 | { |
975 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
975 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
976 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
976 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
977 | tmp_long = (tmp_long * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
977 | tmp_long = (tmp_long * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
978 | tmp_long2 = (tmp_long2 * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
978 | tmp_long2 = (tmp_long2 * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
979 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
979 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
980 | { |
980 | { |
981 | tmp_long /= 2; |
981 | tmp_long /= 2; |
982 | tmp_long2 /= 2; |
982 | tmp_long2 /= 2; |
983 | } |
983 | } |
984 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
984 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
985 | { |
985 | { |
986 | tmp_long /= 3; |
986 | tmp_long /= 3; |
987 | tmp_long2 /= 3; |
987 | tmp_long2 /= 3; |
988 | } |
988 | } |
989 | if(tmp_long > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
989 | if(tmp_long > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
990 | if(tmp_long < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
990 | if(tmp_long < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
991 | if(tmp_long2 > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
991 | if(tmp_long2 > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
992 | if(tmp_long2 < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
992 | if(tmp_long2 < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
993 | } |
993 | } |
994 | else |
994 | else |
995 | { |
995 | { |
996 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
996 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
997 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
997 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
998 | tmp_long /= 16; |
998 | tmp_long /= 16; |
999 | tmp_long2 /= 16; |
999 | tmp_long2 /= 16; |
1000 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
1000 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
1001 | { |
1001 | { |
1002 | tmp_long /= 3; |
1002 | tmp_long /= 3; |
1003 | tmp_long2 /= 3; |
1003 | tmp_long2 /= 3; |
1004 | } |
1004 | } |
1005 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
1005 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
1006 | { |
1006 | { |
1007 | tmp_long /= 3; |
1007 | tmp_long /= 3; |
1008 | tmp_long2 /= 3; |
1008 | tmp_long2 /= 3; |
1009 | } |
1009 | } |
1010 | 1010 | ||
1011 | #define AUSGLEICH 32 |
1011 | #define AUSGLEICH 32 |
1012 | if(tmp_long > AUSGLEICH) tmp_long = AUSGLEICH; |
1012 | if(tmp_long > AUSGLEICH) tmp_long = AUSGLEICH; |
1013 | if(tmp_long < -AUSGLEICH) tmp_long =-AUSGLEICH; |
1013 | if(tmp_long < -AUSGLEICH) tmp_long =-AUSGLEICH; |
1014 | if(tmp_long2 > AUSGLEICH) tmp_long2 = AUSGLEICH; |
1014 | if(tmp_long2 > AUSGLEICH) tmp_long2 = AUSGLEICH; |
1015 | if(tmp_long2 <-AUSGLEICH) tmp_long2 =-AUSGLEICH; |
1015 | if(tmp_long2 <-AUSGLEICH) tmp_long2 =-AUSGLEICH; |
1016 | } |
1016 | } |
1017 | 1017 | ||
1018 | //if(Poti2 > 20) { tmp_long = 0; tmp_long2 = 0;} |
1018 | //if(Poti2 > 20) { tmp_long = 0; tmp_long2 = 0;} |
1019 | Mess_IntegralNick -= tmp_long; |
1019 | Mess_IntegralNick -= tmp_long; |
1020 | Mess_IntegralRoll -= tmp_long2; |
1020 | Mess_IntegralRoll -= tmp_long2; |
1021 | } |
1021 | } |
1022 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1022 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1023 | if(ZaehlMessungen >= ABGLEICH_ANZAHL) |
1023 | if(ZaehlMessungen >= ABGLEICH_ANZAHL) |
1024 | { |
1024 | { |
1025 | static int cnt = 0; |
1025 | static int cnt = 0; |
1026 | static char last_n_p,last_n_n,last_r_p,last_r_n; |
1026 | static char last_n_p,last_n_n,last_r_p,last_r_n; |
1027 | static long MittelIntegralNick_Alt,MittelIntegralRoll_Alt; |
1027 | static long MittelIntegralNick_Alt,MittelIntegralRoll_Alt; |
1028 | if(!Looping_Nick && !Looping_Roll && !TrichterFlug && EE_Parameter.Driftkomp) |
1028 | if(!Looping_Nick && !Looping_Roll && !TrichterFlug && EE_Parameter.Driftkomp) |
1029 | { |
1029 | { |
1030 | MittelIntegralNick /= ABGLEICH_ANZAHL; |
1030 | MittelIntegralNick /= ABGLEICH_ANZAHL; |
1031 | MittelIntegralRoll /= ABGLEICH_ANZAHL; |
1031 | MittelIntegralRoll /= ABGLEICH_ANZAHL; |
1032 | IntegralAccNick = (EE_Parameter.GyroAccFaktor * IntegralAccNick) / ABGLEICH_ANZAHL; |
1032 | IntegralAccNick = (EE_Parameter.GyroAccFaktor * IntegralAccNick) / ABGLEICH_ANZAHL; |
1033 | IntegralAccRoll = (EE_Parameter.GyroAccFaktor * IntegralAccRoll) / ABGLEICH_ANZAHL; |
1033 | IntegralAccRoll = (EE_Parameter.GyroAccFaktor * IntegralAccRoll) / ABGLEICH_ANZAHL; |
1034 | IntegralAccZ = IntegralAccZ / ABGLEICH_ANZAHL; |
1034 | IntegralAccZ = IntegralAccZ / ABGLEICH_ANZAHL; |
1035 | #define MAX_I 0//(Poti2/10) |
1035 | #define MAX_I 0//(Poti2/10) |
1036 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
1036 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
1037 | IntegralFehlerNick = (long)(MittelIntegralNick - (long)IntegralAccNick); |
1037 | IntegralFehlerNick = (long)(MittelIntegralNick - (long)IntegralAccNick); |
1038 | ausgleichNick = IntegralFehlerNick / EE_Parameter.GyroAccAbgleich; |
1038 | ausgleichNick = IntegralFehlerNick / EE_Parameter.GyroAccAbgleich; |
1039 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
1039 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
1040 | IntegralFehlerRoll = (long)(MittelIntegralRoll - (long)IntegralAccRoll); |
1040 | IntegralFehlerRoll = (long)(MittelIntegralRoll - (long)IntegralAccRoll); |
1041 | ausgleichRoll = IntegralFehlerRoll / EE_Parameter.GyroAccAbgleich; |
1041 | ausgleichRoll = IntegralFehlerRoll / EE_Parameter.GyroAccAbgleich; |
1042 | 1042 | ||
1043 | LageKorrekturNick = ausgleichNick / ABGLEICH_ANZAHL; |
1043 | LageKorrekturNick = ausgleichNick / ABGLEICH_ANZAHL; |
1044 | LageKorrekturRoll = ausgleichRoll / ABGLEICH_ANZAHL; |
1044 | LageKorrekturRoll = ausgleichRoll / ABGLEICH_ANZAHL; |
1045 | 1045 | ||
1046 | if(((MaxStickNick > 64) || (MaxStickRoll > 64) || (abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25)) && (FromNaviCtrl_Value.Kalman_K == -1)) |
1046 | if(((MaxStickNick > 64) || (MaxStickRoll > 64) || (abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25)) && (FromNaviCtrl_Value.Kalman_K == -1)) |
1047 | { |
1047 | { |
1048 | LageKorrekturNick /= 2; |
1048 | LageKorrekturNick /= 2; |
1049 | LageKorrekturRoll /= 2; |
1049 | LageKorrekturRoll /= 2; |
1050 | } |
1050 | } |
1051 | 1051 | ||
1052 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1052 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1053 | // Gyro-Drift ermitteln |
1053 | // Gyro-Drift ermitteln |
1054 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1054 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1055 | MittelIntegralNick2 /= ABGLEICH_ANZAHL; |
1055 | MittelIntegralNick2 /= ABGLEICH_ANZAHL; |
1056 | MittelIntegralRoll2 /= ABGLEICH_ANZAHL; |
1056 | MittelIntegralRoll2 /= ABGLEICH_ANZAHL; |
1057 | tmp_long = IntegralNick2 - IntegralNick; |
1057 | tmp_long = IntegralNick2 - IntegralNick; |
1058 | tmp_long2 = IntegralRoll2 - IntegralRoll; |
1058 | tmp_long2 = IntegralRoll2 - IntegralRoll; |
1059 | //DebugOut.Analog[25] = MittelIntegralRoll2 / 26; |
1059 | //DebugOut.Analog[25] = MittelIntegralRoll2 / 26; |
1060 | 1060 | ||
1061 | IntegralFehlerNick = tmp_long; |
1061 | IntegralFehlerNick = tmp_long; |
1062 | IntegralFehlerRoll = tmp_long2; |
1062 | IntegralFehlerRoll = tmp_long2; |
1063 | Mess_IntegralNick2 -= IntegralFehlerNick; |
1063 | Mess_IntegralNick2 -= IntegralFehlerNick; |
1064 | Mess_IntegralRoll2 -= IntegralFehlerRoll; |
1064 | Mess_IntegralRoll2 -= IntegralFehlerRoll; |
1065 | 1065 | ||
1066 | if(EE_Parameter.Driftkomp) |
1066 | if(EE_Parameter.Driftkomp) |
1067 | { |
1067 | { |
1068 | if(GierGyroFehler > ABGLEICH_ANZAHL/2) { AdNeutralGier++; } |
1068 | if(GierGyroFehler > ABGLEICH_ANZAHL/2) { AdNeutralGier++; } |
1069 | if(GierGyroFehler <-ABGLEICH_ANZAHL/2) { AdNeutralGier--; } |
1069 | if(GierGyroFehler <-ABGLEICH_ANZAHL/2) { AdNeutralGier--; } |
1070 | } |
1070 | } |
1071 | GierGyroFehler = 0; |
1071 | GierGyroFehler = 0; |
1072 | 1072 | ||
1073 | 1073 | ||
1074 | #define FEHLER_LIMIT (ABGLEICH_ANZAHL / 2) |
1074 | #define FEHLER_LIMIT (ABGLEICH_ANZAHL / 2) |
1075 | #define FEHLER_LIMIT1 (ABGLEICH_ANZAHL * 2) //4 |
1075 | #define FEHLER_LIMIT1 (ABGLEICH_ANZAHL * 2) //4 |
1076 | #define FEHLER_LIMIT2 (ABGLEICH_ANZAHL * 16) //16 |
1076 | #define FEHLER_LIMIT2 (ABGLEICH_ANZAHL * 16) //16 |
1077 | #define BEWEGUNGS_LIMIT 20000 |
1077 | #define BEWEGUNGS_LIMIT 20000 |
1078 | // Nick +++++++++++++++++++++++++++++++++++++++++++++++++ |
1078 | // Nick +++++++++++++++++++++++++++++++++++++++++++++++++ |
1079 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
1079 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
1080 | if(labs(IntegralFehlerNick) > FEHLER_LIMIT1) cnt = 4; |
1080 | if(labs(IntegralFehlerNick) > FEHLER_LIMIT1) cnt = 4; |
1081 | if(labs(MittelIntegralNick_Alt - MittelIntegralNick) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
1081 | if(labs(MittelIntegralNick_Alt - MittelIntegralNick) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
1082 | { |
1082 | { |
1083 | if(IntegralFehlerNick > FEHLER_LIMIT2) |
1083 | if(IntegralFehlerNick > FEHLER_LIMIT2) |
1084 | { |
1084 | { |
1085 | if(last_n_p) |
1085 | if(last_n_p) |
1086 | { |
1086 | { |
1087 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
1087 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
1088 | ausgleichNick = IntegralFehlerNick / 8; |
1088 | ausgleichNick = IntegralFehlerNick / 8; |
1089 | if(ausgleichNick > 5000) ausgleichNick = 5000; |
1089 | if(ausgleichNick > 5000) ausgleichNick = 5000; |
1090 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1090 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1091 | } |
1091 | } |
1092 | else last_n_p = 1; |
1092 | else last_n_p = 1; |
1093 | } else last_n_p = 0; |
1093 | } else last_n_p = 0; |
1094 | if(IntegralFehlerNick < -FEHLER_LIMIT2) |
1094 | if(IntegralFehlerNick < -FEHLER_LIMIT2) |
1095 | { |
1095 | { |
1096 | if(last_n_n) |
1096 | if(last_n_n) |
1097 | { |
1097 | { |
1098 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
1098 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
1099 | ausgleichNick = IntegralFehlerNick / 8; |
1099 | ausgleichNick = IntegralFehlerNick / 8; |
1100 | if(ausgleichNick < -5000) ausgleichNick = -5000; |
1100 | if(ausgleichNick < -5000) ausgleichNick = -5000; |
1101 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1101 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1102 | } |
1102 | } |
1103 | else last_n_n = 1; |
1103 | else last_n_n = 1; |
1104 | } else last_n_n = 0; |
1104 | } else last_n_n = 0; |
1105 | } |
1105 | } |
1106 | else |
1106 | else |
1107 | { |
1107 | { |
1108 | cnt = 0; |
1108 | cnt = 0; |
1109 | KompassSignalSchlecht = 1000; |
1109 | KompassSignalSchlecht = 1000; |
1110 | } |
1110 | } |
1111 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1111 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1112 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
1112 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
1113 | if(IntegralFehlerNick > FEHLER_LIMIT) AdNeutralNick += cnt; |
1113 | if(IntegralFehlerNick > FEHLER_LIMIT) AdNeutralNick += cnt; |
1114 | if(IntegralFehlerNick < -FEHLER_LIMIT) AdNeutralNick -= cnt; |
1114 | if(IntegralFehlerNick < -FEHLER_LIMIT) AdNeutralNick -= cnt; |
1115 | 1115 | ||
1116 | // Roll +++++++++++++++++++++++++++++++++++++++++++++++++ |
1116 | // Roll +++++++++++++++++++++++++++++++++++++++++++++++++ |
1117 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
1117 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
1118 | if(labs(IntegralFehlerRoll) > FEHLER_LIMIT1) cnt = 4; |
1118 | if(labs(IntegralFehlerRoll) > FEHLER_LIMIT1) cnt = 4; |
1119 | ausgleichRoll = 0; |
1119 | ausgleichRoll = 0; |
1120 | if(labs(MittelIntegralRoll_Alt - MittelIntegralRoll) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
1120 | if(labs(MittelIntegralRoll_Alt - MittelIntegralRoll) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
1121 | { |
1121 | { |
1122 | if(IntegralFehlerRoll > FEHLER_LIMIT2) |
1122 | if(IntegralFehlerRoll > FEHLER_LIMIT2) |
1123 | { |
1123 | { |
1124 | if(last_r_p) |
1124 | if(last_r_p) |
1125 | { |
1125 | { |
1126 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
1126 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
1127 | ausgleichRoll = IntegralFehlerRoll / 8; |
1127 | ausgleichRoll = IntegralFehlerRoll / 8; |
1128 | if(ausgleichRoll > 5000) ausgleichRoll = 5000; |
1128 | if(ausgleichRoll > 5000) ausgleichRoll = 5000; |
1129 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
1129 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
1130 | } |
1130 | } |
1131 | else last_r_p = 1; |
1131 | else last_r_p = 1; |
1132 | } else last_r_p = 0; |
1132 | } else last_r_p = 0; |
1133 | if(IntegralFehlerRoll < -FEHLER_LIMIT2) |
1133 | if(IntegralFehlerRoll < -FEHLER_LIMIT2) |
1134 | { |
1134 | { |
1135 | if(last_r_n) |
1135 | if(last_r_n) |
1136 | { |
1136 | { |
1137 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
1137 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
1138 | ausgleichRoll = IntegralFehlerRoll / 8; |
1138 | ausgleichRoll = IntegralFehlerRoll / 8; |
1139 | if(ausgleichRoll < -5000) ausgleichRoll = -5000; |
1139 | if(ausgleichRoll < -5000) ausgleichRoll = -5000; |
1140 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
1140 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
1141 | } |
1141 | } |
1142 | else last_r_n = 1; |
1142 | else last_r_n = 1; |
1143 | } else last_r_n = 0; |
1143 | } else last_r_n = 0; |
1144 | } else |
1144 | } else |
1145 | { |
1145 | { |
1146 | cnt = 0; |
1146 | cnt = 0; |
1147 | KompassSignalSchlecht = 1000; |
1147 | KompassSignalSchlecht = 1000; |
1148 | } |
1148 | } |
1149 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1149 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1150 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
1150 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
1151 | if(IntegralFehlerRoll > FEHLER_LIMIT) AdNeutralRoll += cnt; |
1151 | if(IntegralFehlerRoll > FEHLER_LIMIT) AdNeutralRoll += cnt; |
1152 | if(IntegralFehlerRoll < -FEHLER_LIMIT) AdNeutralRoll -= cnt; |
1152 | if(IntegralFehlerRoll < -FEHLER_LIMIT) AdNeutralRoll -= cnt; |
1153 | } |
1153 | } |
1154 | else |
1154 | else |
1155 | { |
1155 | { |
1156 | LageKorrekturRoll = 0; |
1156 | LageKorrekturRoll = 0; |
1157 | LageKorrekturNick = 0; |
1157 | LageKorrekturNick = 0; |
1158 | TrichterFlug = 0; |
1158 | TrichterFlug = 0; |
1159 | } |
1159 | } |
1160 | 1160 | ||
1161 | if(!IntegralFaktor) { LageKorrekturRoll = 0; LageKorrekturNick = 0;} // z.B. bei HH |
1161 | if(!IntegralFaktor) { LageKorrekturRoll = 0; LageKorrekturNick = 0;} // z.B. bei HH |
1162 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1162 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1163 | MittelIntegralNick_Alt = MittelIntegralNick; |
1163 | MittelIntegralNick_Alt = MittelIntegralNick; |
1164 | MittelIntegralRoll_Alt = MittelIntegralRoll; |
1164 | MittelIntegralRoll_Alt = MittelIntegralRoll; |
1165 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1165 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1166 | IntegralAccNick = 0; |
1166 | IntegralAccNick = 0; |
1167 | IntegralAccRoll = 0; |
1167 | IntegralAccRoll = 0; |
1168 | IntegralAccZ = 0; |
1168 | IntegralAccZ = 0; |
1169 | MittelIntegralNick = 0; |
1169 | MittelIntegralNick = 0; |
1170 | MittelIntegralRoll = 0; |
1170 | MittelIntegralRoll = 0; |
1171 | MittelIntegralNick2 = 0; |
1171 | MittelIntegralNick2 = 0; |
1172 | MittelIntegralRoll2 = 0; |
1172 | MittelIntegralRoll2 = 0; |
1173 | ZaehlMessungen = 0; |
1173 | ZaehlMessungen = 0; |
1174 | } // ZaehlMessungen >= ABGLEICH_ANZAHL |
1174 | } // ZaehlMessungen >= ABGLEICH_ANZAHL |
1175 | 1175 | ||
1176 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1176 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1177 | // Gieren |
1177 | // Gieren |
1178 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1178 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1179 | // if(GasMischanteil < 35) { if(StickGier > 10) StickGier = 10; else if(StickGier < -10) StickGier = -10;}; |
1179 | // if(GasMischanteil < 35) { if(StickGier > 10) StickGier = 10; else if(StickGier < -10) StickGier = -10;}; |
1180 | if(abs(StickGier) > 15) // war 35 |
1180 | if(abs(StickGier) > 15) // war 35 |
1181 | { |
1181 | { |
1182 | KompassSignalSchlecht = 1000; |
1182 | KompassSignalSchlecht = 1000; |
1183 | if(!(EE_Parameter.GlobalConfig & CFG_KOMPASS_FIX)) |
1183 | if(!(EE_Parameter.GlobalConfig & CFG_KOMPASS_FIX)) |
1184 | { |
1184 | { |
1185 | NeueKompassRichtungMerken = 1; |
1185 | NeueKompassRichtungMerken = 1; |
1186 | }; |
1186 | }; |
1187 | } |
1187 | } |
1188 | tmp_int = (long) EE_Parameter.Gier_P * ((long)StickGier * abs(StickGier)) / 512L; // expo y = ax + bx² |
1188 | tmp_int = (long) EE_Parameter.Gier_P * ((long)StickGier * abs(StickGier)) / 512L; // expo y = ax + bx² |
1189 | tmp_int += (EE_Parameter.Gier_P * StickGier) / 4; |
1189 | tmp_int += (EE_Parameter.Gier_P * StickGier) / 4; |
1190 | sollGier = tmp_int; |
1190 | sollGier = tmp_int; |
1191 | Mess_Integral_Gier -= tmp_int; |
1191 | Mess_Integral_Gier -= tmp_int; |
1192 | if(Mess_Integral_Gier > 50000) Mess_Integral_Gier = 50000; // begrenzen |
1192 | if(Mess_Integral_Gier > 50000) Mess_Integral_Gier = 50000; // begrenzen |
1193 | if(Mess_Integral_Gier <-50000) Mess_Integral_Gier =-50000; |
1193 | if(Mess_Integral_Gier <-50000) Mess_Integral_Gier =-50000; |
1194 | 1194 | ||
1195 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1195 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1196 | // Kompass |
1196 | // Kompass |
1197 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1197 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1198 | DebugOut.Analog[18] = KompassSignalSchlecht; |
1198 | DebugOut.Analog[18] = KompassSignalSchlecht; |
1199 | 1199 | ||
1200 | if(KompassValue && (EE_Parameter.GlobalConfig & CFG_KOMPASS_AKTIV)) |
1200 | if(KompassValue && (EE_Parameter.GlobalConfig & CFG_KOMPASS_AKTIV)) |
1201 | { |
1201 | { |
1202 | int w,v,r,fehler,korrektur; |
1202 | int w,v,r,fehler,korrektur; |
1203 | w = abs(IntegralNick /512); // mit zunehmender Neigung den Einfluss drosseln |
1203 | w = abs(IntegralNick /512); // mit zunehmender Neigung den Einfluss drosseln |
1204 | v = abs(IntegralRoll /512); |
1204 | v = abs(IntegralRoll /512); |
1205 | if(v > w) w = v; // grösste Neigung ermitteln |
1205 | if(v > w) w = v; // grösste Neigung ermitteln |
1206 | korrektur = w / 8 + 2; |
1206 | korrektur = w / 8 + 2; |
1207 | fehler = ((540 + KompassValue - (ErsatzKompass/GIER_GRAD_FAKTOR)) % 360) - 180; |
1207 | fehler = ((540 + KompassValue - (ErsatzKompass/GIER_GRAD_FAKTOR)) % 360) - 180; |
1208 | if(abs(MesswertGier) > 128) |
1208 | fehler += MesswertGier / 12; |
1209 | { |
- | |
1210 | // korrektur = korrektur = w / 16 + 2; // schnell konvergieren |
- | |
1211 | } |
1209 | |
1212 | if(!KompassSignalSchlecht && w < 25) |
1210 | if(!KompassSignalSchlecht && w < 25) |
1213 | { |
1211 | { |
1214 | GierGyroFehler += fehler; |
1212 | GierGyroFehler += fehler; |
1215 | if(NeueKompassRichtungMerken) |
1213 | if(NeueKompassRichtungMerken) |
1216 | { |
1214 | { |
1217 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
1215 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
1218 | KompassStartwert = (ErsatzKompass/GIER_GRAD_FAKTOR); |
1216 | KompassStartwert = (ErsatzKompass/GIER_GRAD_FAKTOR); |
1219 | NeueKompassRichtungMerken = 0; |
1217 | NeueKompassRichtungMerken = 0; |
1220 | } |
1218 | } |
1221 | } |
1219 | } |
1222 | DebugOut.Analog[16] = fehler; |
1220 | DebugOut.Analog[16] = fehler; |
1223 | DebugOut.Analog[17] = korrektur; |
1221 | DebugOut.Analog[17] = korrektur; |
1224 | ErsatzKompass += (fehler * 16) / korrektur; |
1222 | ErsatzKompass += (fehler * 16) / korrektur; |
1225 | w = (w * Parameter_KompassWirkung) / 32; // auf die Wirkung normieren |
1223 | w = (w * Parameter_KompassWirkung) / 32; // auf die Wirkung normieren |
1226 | w = Parameter_KompassWirkung - w; // Wirkung ggf drosseln |
1224 | w = Parameter_KompassWirkung - w; // Wirkung ggf drosseln |
1227 | if(w >= 0) |
1225 | if(w >= 0) |
1228 | { |
1226 | { |
1229 | if(!KompassSignalSchlecht) |
1227 | if(!KompassSignalSchlecht) |
1230 | { |
1228 | { |
1231 | v = 64 + ((MaxStickNick + MaxStickRoll)) / 8; |
1229 | v = 64 + ((MaxStickNick + MaxStickRoll)) / 8; |
1232 | r = ((540 + (ErsatzKompass/GIER_GRAD_FAKTOR) - KompassStartwert) % 360) - 180; |
1230 | r = ((540 + (ErsatzKompass/GIER_GRAD_FAKTOR) - KompassStartwert) % 360) - 180; |
1233 | // r = KompassRichtung; |
1231 | // r = KompassRichtung; |
1234 | v = (r * w) / v; // nach Kompass ausrichten |
1232 | v = (r * w) / v; // nach Kompass ausrichten |
1235 | w = 3 * Parameter_KompassWirkung; |
1233 | w = 3 * Parameter_KompassWirkung; |
1236 | if(v > w) v = w; // Begrenzen |
1234 | if(v > w) v = w; // Begrenzen |
1237 | else |
1235 | else |
1238 | if(v < -w) v = -w; |
1236 | if(v < -w) v = -w; |
1239 | Mess_Integral_Gier += v; |
1237 | Mess_Integral_Gier += v; |
1240 | } |
1238 | } |
1241 | if(KompassSignalSchlecht) KompassSignalSchlecht--; |
1239 | if(KompassSignalSchlecht) KompassSignalSchlecht--; |
1242 | } |
1240 | } |
1243 | else KompassSignalSchlecht = 500; // so lange das Signal taub stellen --> ca. 1 sek |
1241 | else KompassSignalSchlecht = 500; // so lange das Signal taub stellen --> ca. 1 sek |
1244 | } |
1242 | } |
1245 | 1243 | ||
1246 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1244 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1247 | // Drehgeschwindigkeit und -winkel zu einem Istwert zusammenfassen |
1245 | // Drehgeschwindigkeit und -winkel zu einem Istwert zusammenfassen |
1248 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1246 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1249 | if(TrichterFlug) { SummeRoll = 0; SummeNick = 0;}; |
1247 | if(TrichterFlug) { SummeRoll = 0; SummeNick = 0;}; |
1250 | 1248 | ||
1251 | if(!Looping_Nick) IntegralNickMalFaktor = (IntegralNick * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralNickMalFaktor = 0; |
1249 | if(!Looping_Nick) IntegralNickMalFaktor = (IntegralNick * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralNickMalFaktor = 0; |
1252 | if(!Looping_Roll) IntegralRollMalFaktor = (IntegralRoll * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralRollMalFaktor = 0; |
1250 | if(!Looping_Roll) IntegralRollMalFaktor = (IntegralRoll * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralRollMalFaktor = 0; |
1253 | 1251 | ||
1254 | #define TRIM_MAX 200 |
1252 | #define TRIM_MAX 200 |
1255 | if(TrimNick > TRIM_MAX) TrimNick = TRIM_MAX; else if(TrimNick <-TRIM_MAX) TrimNick =-TRIM_MAX; |
1253 | if(TrimNick > TRIM_MAX) TrimNick = TRIM_MAX; else if(TrimNick <-TRIM_MAX) TrimNick =-TRIM_MAX; |
1256 | if(TrimRoll > TRIM_MAX) TrimRoll = TRIM_MAX; else if(TrimRoll <-TRIM_MAX) TrimRoll =-TRIM_MAX; |
1254 | if(TrimRoll > TRIM_MAX) TrimRoll = TRIM_MAX; else if(TrimRoll <-TRIM_MAX) TrimRoll =-TRIM_MAX; |
1257 | 1255 | ||
1258 | MesswertNick = IntegralNickMalFaktor + (long)((long)MesswertNick * GyroFaktor + (long)TrimNick * 128L) / (256L / STICK_GAIN); |
1256 | MesswertNick = IntegralNickMalFaktor + (long)((long)MesswertNick * GyroFaktor + (long)TrimNick * 128L) / (256L / STICK_GAIN); |
1259 | MesswertRoll = IntegralRollMalFaktor + (long)((long)MesswertRoll * GyroFaktor + (long)TrimRoll * 128L) / (256L / STICK_GAIN); |
1257 | MesswertRoll = IntegralRollMalFaktor + (long)((long)MesswertRoll * GyroFaktor + (long)TrimRoll * 128L) / (256L / STICK_GAIN); |
1260 | MesswertGier = (long)(MesswertGier * 2 * (long)GyroFaktorGier) / (256L / STICK_GAIN) + (long)(Integral_Gier * IntegralFaktorGier) / (2 * (44000 / STICK_GAIN)); |
1258 | MesswertGier = (long)(MesswertGier * 2 * (long)GyroFaktorGier) / (256L / STICK_GAIN) + (long)(Integral_Gier * IntegralFaktorGier) / (2 * (44000 / STICK_GAIN)); |
1261 | 1259 | ||
1262 | // Maximalwerte abfangen |
1260 | // Maximalwerte abfangen |
1263 | // #define MAX_SENSOR (4096*STICK_GAIN) |
1261 | // #define MAX_SENSOR (4096*STICK_GAIN) |
1264 | #define MAX_SENSOR (4096*4) |
1262 | #define MAX_SENSOR (4096*4) |
1265 | if(MesswertNick > MAX_SENSOR) MesswertNick = MAX_SENSOR; |
1263 | if(MesswertNick > MAX_SENSOR) MesswertNick = MAX_SENSOR; |
1266 | if(MesswertNick < -MAX_SENSOR) MesswertNick = -MAX_SENSOR; |
1264 | if(MesswertNick < -MAX_SENSOR) MesswertNick = -MAX_SENSOR; |
1267 | if(MesswertRoll > MAX_SENSOR) MesswertRoll = MAX_SENSOR; |
1265 | if(MesswertRoll > MAX_SENSOR) MesswertRoll = MAX_SENSOR; |
1268 | if(MesswertRoll < -MAX_SENSOR) MesswertRoll = -MAX_SENSOR; |
1266 | if(MesswertRoll < -MAX_SENSOR) MesswertRoll = -MAX_SENSOR; |
1269 | if(MesswertGier > MAX_SENSOR) MesswertGier = MAX_SENSOR; |
1267 | if(MesswertGier > MAX_SENSOR) MesswertGier = MAX_SENSOR; |
1270 | if(MesswertGier < -MAX_SENSOR) MesswertGier = -MAX_SENSOR; |
1268 | if(MesswertGier < -MAX_SENSOR) MesswertGier = -MAX_SENSOR; |
1271 | 1269 | ||
1272 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1270 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1273 | // Höhenregelung |
1271 | // Höhenregelung |
1274 | // Die Höhenregelung schwächt lediglich das Gas ab, erhöht es allerdings nicht |
1272 | // Die Höhenregelung schwächt lediglich das Gas ab, erhöht es allerdings nicht |
1275 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1273 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1276 | if(UBat > BattLowVoltageWarning) GasMischanteil = ((unsigned int)GasMischanteil * BattLowVoltageWarning) / UBat; // Gas auf das aktuelle Spannungvieveau beziehen |
1274 | if(UBat > BattLowVoltageWarning) GasMischanteil = ((unsigned int)GasMischanteil * BattLowVoltageWarning) / UBat; // Gas auf das aktuelle Spannungvieveau beziehen |
1277 | GasMischanteil *= STICK_GAIN; |
1275 | GasMischanteil *= STICK_GAIN; |
1278 | // if height control is activated |
1276 | // if height control is activated |
1279 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG) && !(Looping_Roll || Looping_Nick)) // Höhenregelung |
1277 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG) && !(Looping_Roll || Looping_Nick)) // Höhenregelung |
1280 | { |
1278 | { |
1281 | #define HOVER_GAS_AVERAGE 4096L // 4096 * 2ms = 8.2s averaging |
1279 | #define HOVER_GAS_AVERAGE 4096L // 4096 * 2ms = 8.2s averaging |
1282 | #define HC_GAS_AVERAGE 4 // 4 * 2ms= 8ms averaging |
1280 | #define HC_GAS_AVERAGE 4 // 4 * 2ms= 8ms averaging |
1283 | 1281 | ||
1284 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
1282 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
1285 | #define OPA_OFFSET_STEP 15 |
1283 | #define OPA_OFFSET_STEP 15 |
1286 | #else |
1284 | #else |
1287 | #define OPA_OFFSET_STEP 10 |
1285 | #define OPA_OFFSET_STEP 10 |
1288 | #endif |
1286 | #endif |
1289 | int HCGas, HeightDeviation = 0; |
1287 | int HCGas, HeightDeviation = 0; |
1290 | static int HeightTrimming = 0; // rate for change of height setpoint |
1288 | static int HeightTrimming = 0; // rate for change of height setpoint |
1291 | static int FilterHCGas = 0; |
1289 | static int FilterHCGas = 0; |
1292 | static int StickGasHover = 120, HoverGas = 0, HoverGasMin = 0, HoverGasMax = 1023; |
1290 | static int StickGasHover = 120, HoverGas = 0, HoverGasMin = 0, HoverGasMax = 1023; |
1293 | static unsigned long HoverGasFilter = 0; |
1291 | static unsigned long HoverGasFilter = 0; |
1294 | static unsigned char delay = 100, BaroAtUpperLimit = 0, BaroAtLowerLimit = 0; |
1292 | static unsigned char delay = 100, BaroAtUpperLimit = 0, BaroAtLowerLimit = 0; |
1295 | int CosAttitude; // for projection of hoover gas |
1293 | int CosAttitude; // for projection of hoover gas |
1296 | 1294 | ||
1297 | // get the current hooverpoint |
1295 | // get the current hooverpoint |
1298 | DebugOut.Analog[21] = HoverGas; |
1296 | DebugOut.Analog[21] = HoverGas; |
1299 | 1297 | ||
1300 | // Expand the measurement |
1298 | // Expand the measurement |
1301 | // measurement of air pressure close to upper limit and no overflow in correction of the new OCR0A value occurs |
1299 | // measurement of air pressure close to upper limit and no overflow in correction of the new OCR0A value occurs |
1302 | if(!BaroExpandActive) |
1300 | if(!BaroExpandActive) |
1303 | { |
1301 | { |
1304 | if(MessLuftdruck > 920) |
1302 | if(MessLuftdruck > 920) |
1305 | { // increase offset |
1303 | { // increase offset |
1306 | if(OCR0A < (255 - OPA_OFFSET_STEP)) |
1304 | if(OCR0A < (255 - OPA_OFFSET_STEP)) |
1307 | { |
1305 | { |
1308 | ExpandBaro -= 1; |
1306 | ExpandBaro -= 1; |
1309 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // increase offset to shift ADC down |
1307 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // increase offset to shift ADC down |
1310 | beeptime = 300; |
1308 | beeptime = 300; |
1311 | BaroExpandActive = 350; |
1309 | BaroExpandActive = 350; |
1312 | } |
1310 | } |
1313 | else |
1311 | else |
1314 | { |
1312 | { |
1315 | BaroAtLowerLimit = 1; |
1313 | BaroAtLowerLimit = 1; |
1316 | } |
1314 | } |
1317 | } |
1315 | } |
1318 | // measurement of air pressure close to lower limit and |
1316 | // measurement of air pressure close to lower limit and |
1319 | else |
1317 | else |
1320 | if(MessLuftdruck < 100) |
1318 | if(MessLuftdruck < 100) |
1321 | { // decrease offset |
1319 | { // decrease offset |
1322 | if(OCR0A > OPA_OFFSET_STEP) |
1320 | if(OCR0A > OPA_OFFSET_STEP) |
1323 | { |
1321 | { |
1324 | ExpandBaro += 1; |
1322 | ExpandBaro += 1; |
1325 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // decrease offset to shift ADC up |
1323 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // decrease offset to shift ADC up |
1326 | beeptime = 300; |
1324 | beeptime = 300; |
1327 | BaroExpandActive = 350; |
1325 | BaroExpandActive = 350; |
1328 | } |
1326 | } |
1329 | else |
1327 | else |
1330 | { |
1328 | { |
1331 | BaroAtUpperLimit = 1; |
1329 | BaroAtUpperLimit = 1; |
1332 | } |
1330 | } |
1333 | } |
1331 | } |
1334 | else |
1332 | else |
1335 | { |
1333 | { |
1336 | BaroAtUpperLimit = 0; |
1334 | BaroAtUpperLimit = 0; |
1337 | BaroAtLowerLimit = 0; |
1335 | BaroAtLowerLimit = 0; |
1338 | } |
1336 | } |
1339 | } |
1337 | } |
1340 | else // delay, because of expanding the Baro-Range |
1338 | else // delay, because of expanding the Baro-Range |
1341 | { |
1339 | { |
1342 | // now clear the D-values |
1340 | // now clear the D-values |
1343 | SummenHoehe = HoehenWert * SM_FILTER; |
1341 | SummenHoehe = HoehenWert * SM_FILTER; |
1344 | VarioMeter = 0; |
1342 | VarioMeter = 0; |
1345 | BaroExpandActive--; |
1343 | BaroExpandActive--; |
1346 | } |
1344 | } |
1347 | 1345 | ||
1348 | // if height control is activated by an rc channel |
1346 | // if height control is activated by an rc channel |
1349 | if(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER) // Regler wird über Schalter gesteuert |
1347 | if(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER) // Regler wird über Schalter gesteuert |
1350 | { // check if parameter is less than activation threshold |
1348 | { // check if parameter is less than activation threshold |
1351 | if(Parameter_MaxHoehe < 50) // for 3 or 2-state switch height control is disabled in lowest position |
1349 | if(Parameter_MaxHoehe < 50) // for 3 or 2-state switch height control is disabled in lowest position |
1352 | { //height control not active |
1350 | { //height control not active |
1353 | if(!delay--) |
1351 | if(!delay--) |
1354 | { |
1352 | { |
1355 | HoehenReglerAktiv = 0; // disable height control |
1353 | HoehenReglerAktiv = 0; // disable height control |
1356 | SollHoehe = HoehenWert; // update SetPoint with current reading |
1354 | SollHoehe = HoehenWert; // update SetPoint with current reading |
1357 | delay = 1; |
1355 | delay = 1; |
1358 | } |
1356 | } |
1359 | } |
1357 | } |
1360 | else |
1358 | else |
1361 | { //height control is activated |
1359 | { //height control is activated |
1362 | HoehenReglerAktiv = 1; // enable height control |
1360 | HoehenReglerAktiv = 1; // enable height control |
1363 | delay = 200; |
1361 | delay = 200; |
1364 | } |
1362 | } |
1365 | } |
1363 | } |
1366 | else // no switchable height control |
1364 | else // no switchable height control |
1367 | { |
1365 | { |
1368 | SollHoehe = ((int16_t) ExternHoehenValue + (int16_t) Parameter_MaxHoehe) * (int)EE_Parameter.Hoehe_Verstaerkung; |
1366 | SollHoehe = ((int16_t) ExternHoehenValue + (int16_t) Parameter_MaxHoehe) * (int)EE_Parameter.Hoehe_Verstaerkung; |
1369 | HoehenReglerAktiv = 1; |
1367 | HoehenReglerAktiv = 1; |
1370 | } |
1368 | } |
1371 | 1369 | ||
1372 | // calculate cos of nick and roll angle used for projection of the vertical hoover gas |
1370 | // calculate cos of nick and roll angle used for projection of the vertical hoover gas |
1373 | tmp_int = (int)(IntegralNick/GIER_GRAD_FAKTOR); // nick angle in deg |
1371 | tmp_int = (int)(IntegralNick/GIER_GRAD_FAKTOR); // nick angle in deg |
1374 | tmp_int2 = (int)(IntegralRoll/GIER_GRAD_FAKTOR); // roll angle in deg |
1372 | tmp_int2 = (int)(IntegralRoll/GIER_GRAD_FAKTOR); // roll angle in deg |
1375 | CosAttitude = (int16_t)ihypot(tmp_int, tmp_int2); // phytagoras gives effective attitude angle in deg |
1373 | CosAttitude = (int16_t)ihypot(tmp_int, tmp_int2); // phytagoras gives effective attitude angle in deg |
1376 | LIMIT_MAX(CosAttitude, 60); // limit effective attitude angle |
1374 | LIMIT_MAX(CosAttitude, 60); // limit effective attitude angle |
1377 | CosAttitude = c_cos_8192(CosAttitude); // cos of actual attitude |
1375 | CosAttitude = c_cos_8192(CosAttitude); // cos of actual attitude |
1378 | VarioCharacter = ' '; |
1376 | VarioCharacter = ' '; |
1379 | if(HoehenReglerAktiv && !(FCFlags & FCFLAG_NOTLANDUNG)) |
1377 | if(HoehenReglerAktiv && !(FCFlags & FCFLAG_NOTLANDUNG)) |
1380 | { |
1378 | { |
1381 | #define HEIGHT_TRIM_UP 0x01 |
1379 | #define HEIGHT_TRIM_UP 0x01 |
1382 | #define HEIGHT_TRIM_DOWN 0x02 |
1380 | #define HEIGHT_TRIM_DOWN 0x02 |
1383 | static unsigned char HeightTrimmingFlag = 0x00; |
1381 | static unsigned char HeightTrimmingFlag = 0x00; |
1384 | 1382 | ||
1385 | #define HEIGHT_CONTROL_STICKTHRESHOLD 15 |
1383 | #define HEIGHT_CONTROL_STICKTHRESHOLD 15 |
1386 | // Holger original version |
1384 | // Holger original version |
1387 | // start of height control algorithm |
1385 | // start of height control algorithm |
1388 | // the height control is only an attenuation of the actual gas stick. |
1386 | // the height control is only an attenuation of the actual gas stick. |
1389 | // I.e. it will work only if the gas stick is higher than the hover gas |
1387 | // I.e. it will work only if the gas stick is higher than the hover gas |
1390 | // and the hover height will be allways larger than height setpoint. |
1388 | // and the hover height will be allways larger than height setpoint. |
1391 | if((EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) || !(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER)) // Regler wird über Schalter gesteuert) |
1389 | if((EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) || !(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER)) // Regler wird über Schalter gesteuert) |
1392 | { // old version |
1390 | { // old version |
1393 | HCGas = GasMischanteil; // take current stick gas as neutral point for the height control |
1391 | HCGas = GasMischanteil; // take current stick gas as neutral point for the height control |
1394 | HeightTrimming = 0; |
1392 | HeightTrimming = 0; |
1395 | } |
1393 | } |
1396 | else |
1394 | else |
1397 | { |
1395 | { |
1398 | // alternative height control |
1396 | // alternative height control |
1399 | // PD-Control with respect to hoover point |
1397 | // PD-Control with respect to hoover point |
1400 | // the thrust loss out of horizontal attitude is compensated |
1398 | // the thrust loss out of horizontal attitude is compensated |
1401 | // the setpoint will be fine adjusted with the gas stick position |
1399 | // the setpoint will be fine adjusted with the gas stick position |
1402 | if(FCFlags & FCFLAG_FLY) // trim setpoint only when flying |
1400 | if(FCFlags & FCFLAG_FLY) // trim setpoint only when flying |
1403 | { // gas stick is above hoover point |
1401 | { // gas stick is above hoover point |
1404 | if(StickGas > (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtUpperLimit) |
1402 | if(StickGas > (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtUpperLimit) |
1405 | { |
1403 | { |
1406 | if(HeightTrimmingFlag & HEIGHT_TRIM_DOWN) |
1404 | if(HeightTrimmingFlag & HEIGHT_TRIM_DOWN) |
1407 | { |
1405 | { |
1408 | HeightTrimmingFlag &= ~HEIGHT_TRIM_DOWN; |
1406 | HeightTrimmingFlag &= ~HEIGHT_TRIM_DOWN; |
1409 | SollHoehe = HoehenWert; // update setpoint to current heigth |
1407 | SollHoehe = HoehenWert; // update setpoint to current heigth |
1410 | } |
1408 | } |
1411 | HeightTrimmingFlag |= HEIGHT_TRIM_UP; |
1409 | HeightTrimmingFlag |= HEIGHT_TRIM_UP; |
1412 | HeightTrimming += abs(StickGas - (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD)); |
1410 | HeightTrimming += abs(StickGas - (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD)); |
1413 | VarioCharacter = '+'; |
1411 | VarioCharacter = '+'; |
1414 | } // gas stick is below hoover point |
1412 | } // gas stick is below hoover point |
1415 | else if(StickGas < (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtLowerLimit ) |
1413 | else if(StickGas < (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtLowerLimit ) |
1416 | { |
1414 | { |
1417 | if(HeightTrimmingFlag & HEIGHT_TRIM_UP) |
1415 | if(HeightTrimmingFlag & HEIGHT_TRIM_UP) |
1418 | { |
1416 | { |
1419 | HeightTrimmingFlag &= ~HEIGHT_TRIM_UP; |
1417 | HeightTrimmingFlag &= ~HEIGHT_TRIM_UP; |
1420 | SollHoehe = HoehenWert; // update setpoint to current heigth |
1418 | SollHoehe = HoehenWert; // update setpoint to current heigth |
1421 | } |
1419 | } |
1422 | HeightTrimmingFlag |= HEIGHT_TRIM_DOWN; |
1420 | HeightTrimmingFlag |= HEIGHT_TRIM_DOWN; |
1423 | HeightTrimming -= abs(StickGas - (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD)); |
1421 | HeightTrimming -= abs(StickGas - (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD)); |
1424 | VarioCharacter = '-'; |
1422 | VarioCharacter = '-'; |
1425 | } |
1423 | } |
1426 | else // Gas Stick in Hover Range |
1424 | else // Gas Stick in Hover Range |
1427 | { |
1425 | { |
1428 | if(HeightTrimmingFlag & (HEIGHT_TRIM_UP | HEIGHT_TRIM_DOWN)) |
1426 | if(HeightTrimmingFlag & (HEIGHT_TRIM_UP | HEIGHT_TRIM_DOWN)) |
1429 | { |
1427 | { |
1430 | HeightTrimmingFlag &= ~(HEIGHT_TRIM_UP | HEIGHT_TRIM_DOWN); |
1428 | HeightTrimmingFlag &= ~(HEIGHT_TRIM_UP | HEIGHT_TRIM_DOWN); |
1431 | HeightTrimming = 0; |
1429 | HeightTrimming = 0; |
1432 | SollHoehe = HoehenWert; // update setpoint to current height |
1430 | SollHoehe = HoehenWert; // update setpoint to current height |
1433 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 500; |
1431 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 500; |
1434 | } |
1432 | } |
1435 | VarioCharacter = '='; |
1433 | VarioCharacter = '='; |
1436 | } |
1434 | } |
1437 | // Trim height set point |
1435 | // Trim height set point |
1438 | if(abs(HeightTrimming) > 512) |
1436 | if(abs(HeightTrimming) > 512) |
1439 | { |
1437 | { |
1440 | SollHoehe += (HeightTrimming * EE_Parameter.Hoehe_Verstaerkung)/(5 * 512 / 2); // move setpoint |
1438 | SollHoehe += (HeightTrimming * EE_Parameter.Hoehe_Verstaerkung)/(5 * 512 / 2); // move setpoint |
1441 | HeightTrimming = 0; |
1439 | HeightTrimming = 0; |
1442 | LIMIT_MIN_MAX(SollHoehe, (HoehenWert-1024), (HoehenWert+1024)); // max. 10m Unterschied |
1440 | LIMIT_MIN_MAX(SollHoehe, (HoehenWert-1024), (HoehenWert+1024)); // max. 10m Unterschied |
1443 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 75; |
1441 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 75; |
1444 | //update hoover gas stick value when setpoint is shifted |
1442 | //update hoover gas stick value when setpoint is shifted |
1445 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
1443 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
1446 | { |
1444 | { |
1447 | StickGasHover = HoverGas/STICK_GAIN; //rescale back to stick value |
1445 | StickGasHover = HoverGas/STICK_GAIN; //rescale back to stick value |
1448 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
1446 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
1449 | if(StickGasHover < 70) StickGasHover = 70; |
1447 | if(StickGasHover < 70) StickGasHover = 70; |
1450 | else if(StickGasHover > 150) StickGasHover = 150; |
1448 | else if(StickGasHover > 150) StickGasHover = 150; |
1451 | } |
1449 | } |
1452 | } |
1450 | } |
1453 | if(BaroExpandActive) SollHoehe = HoehenWert; // update setpoint to current altitude if Expanding is active |
1451 | if(BaroExpandActive) SollHoehe = HoehenWert; // update setpoint to current altitude if Expanding is active |
1454 | } //if FCFlags & MKFCFLAG_FLY |
1452 | } //if FCFlags & MKFCFLAG_FLY |
1455 | else |
1453 | else |
1456 | { |
1454 | { |
1457 | SollHoehe = HoehenWert - 400; |
1455 | SollHoehe = HoehenWert - 400; |
1458 | if(EE_Parameter.Hoehe_StickNeutralPoint) StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
1456 | if(EE_Parameter.Hoehe_StickNeutralPoint) StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
1459 | else StickGasHover = 120; |
1457 | else StickGasHover = 120; |
1460 | } |
1458 | } |
1461 | HCGas = HoverGas; // take hover gas (neutral point) |
1459 | HCGas = HoverGas; // take hover gas (neutral point) |
1462 | } |
1460 | } |
1463 | if(HoehenWert > SollHoehe || !(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT)) |
1461 | if(HoehenWert > SollHoehe || !(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT)) |
1464 | { |
1462 | { |
1465 | // from this point the Heigth Control Algorithm is identical for both versions |
1463 | // from this point the Heigth Control Algorithm is identical for both versions |
1466 | if(BaroExpandActive) // baro range expanding active |
1464 | if(BaroExpandActive) // baro range expanding active |
1467 | { |
1465 | { |
1468 | HCGas = HoverGas; // hover while expanding baro adc range |
1466 | HCGas = HoverGas; // hover while expanding baro adc range |
1469 | HeightDeviation = 0; |
1467 | HeightDeviation = 0; |
1470 | } // EOF // baro range expanding active |
1468 | } // EOF // baro range expanding active |
1471 | else // valid data from air pressure sensor |
1469 | else // valid data from air pressure sensor |
1472 | { |
1470 | { |
1473 | // ------------------------- P-Part ---------------------------- |
1471 | // ------------------------- P-Part ---------------------------- |
1474 | tmp_long = (HoehenWert - SollHoehe); // positive when too high |
1472 | tmp_long = (HoehenWert - SollHoehe); // positive when too high |
1475 | LIMIT_MIN_MAX(tmp_long, -32767L, 32767L); // avoid overflov when casting to int16_t |
1473 | LIMIT_MIN_MAX(tmp_long, -32767L, 32767L); // avoid overflov when casting to int16_t |
1476 | HeightDeviation = (int)(tmp_long); // positive when too high |
1474 | HeightDeviation = (int)(tmp_long); // positive when too high |
1477 | tmp_long = (tmp_long * (long)Parameter_Hoehe_P) / 16L; // p-part |
1475 | tmp_long = (tmp_long * (long)Parameter_Hoehe_P) / 16L; // p-part |
1478 | LIMIT_MIN_MAX(tmp_long, -255 * STICK_GAIN, 255 * STICK_GAIN); // more than 2 times the full range makes no sense |
1476 | LIMIT_MIN_MAX(tmp_long, -255 * STICK_GAIN, 255 * STICK_GAIN); // more than 2 times the full range makes no sense |
1479 | HCGas -= tmp_long; |
1477 | HCGas -= tmp_long; |
1480 | // ------------------------- D-Part 1: Vario Meter ---------------------------- |
1478 | // ------------------------- D-Part 1: Vario Meter ---------------------------- |
1481 | tmp_int = VarioMeter / 8; |
1479 | tmp_int = VarioMeter / 8; |
1482 | LIMIT_MIN_MAX(tmp_int, -181, 181); // avoid overflow when squared (181^2 = 32761) |
1480 | LIMIT_MIN_MAX(tmp_int, -181, 181); // avoid overflow when squared (181^2 = 32761) |
1483 | tmp_int2 = tmp_int; |
1481 | tmp_int2 = tmp_int; |
1484 | LIMIT_MAX(tmp_int2, 8); // limit quadratic part on upward movement to avoid to much gas reduction |
1482 | LIMIT_MAX(tmp_int2, 8); // limit quadratic part on upward movement to avoid to much gas reduction |
1485 | if(tmp_int2 > 0) tmp_int = tmp_int + (tmp_int2 * tmp_int2) / 4; |
1483 | if(tmp_int2 > 0) tmp_int = tmp_int + (tmp_int2 * tmp_int2) / 4; |
1486 | else tmp_int = tmp_int - (tmp_int2 * tmp_int2) / 4; |
1484 | else tmp_int = tmp_int - (tmp_int2 * tmp_int2) / 4; |
1487 | tmp_int = (tmp_int * (long)Parameter_Luftdruck_D) / 128L; // scale to d-gain parameter |
1485 | tmp_int = (tmp_int * (long)Parameter_Luftdruck_D) / 128L; // scale to d-gain parameter |
1488 | LIMIT_MIN_MAX(tmp_int,-32 * STICK_GAIN, 64 * STICK_GAIN); |
1486 | LIMIT_MIN_MAX(tmp_int,-32 * STICK_GAIN, 64 * STICK_GAIN); |
1489 | HCGas -= tmp_int; |
1487 | HCGas -= tmp_int; |
1490 | } // EOF no baro range expanding |
1488 | } // EOF no baro range expanding |
1491 | // ------------------------ D-Part 2: ACC-Z Integral ------------------------ |
1489 | // ------------------------ D-Part 2: ACC-Z Integral ------------------------ |
1492 | tmp_long = ((Mess_Integral_Hoch / 128L) * (int32_t) Parameter_Hoehe_ACC_Wirkung) / (128L / STICK_GAIN); |
1490 | tmp_long = ((Mess_Integral_Hoch / 128L) * (int32_t) Parameter_Hoehe_ACC_Wirkung) / (128L / STICK_GAIN); |
1493 | LIMIT_MIN_MAX(tmp_long, -32 * STICK_GAIN, 64 * STICK_GAIN); |
1491 | LIMIT_MIN_MAX(tmp_long, -32 * STICK_GAIN, 64 * STICK_GAIN); |
1494 | HCGas -= tmp_long; |
1492 | HCGas -= tmp_long; |
1495 | // ------------------------ D-Part 3: GpsZ ---------------------------------- |
1493 | // ------------------------ D-Part 3: GpsZ ---------------------------------- |
1496 | tmp_int = (Parameter_Hoehe_GPS_Z * (int)FromNaviCtrl_Value.GpsZ)/128L; |
1494 | tmp_int = (Parameter_Hoehe_GPS_Z * (int)FromNaviCtrl_Value.GpsZ)/128L; |
1497 | LIMIT_MIN_MAX(tmp_int, -32 * STICK_GAIN, 64 * STICK_GAIN); |
1495 | LIMIT_MIN_MAX(tmp_int, -32 * STICK_GAIN, 64 * STICK_GAIN); |
1498 | HCGas -= tmp_int; |
1496 | HCGas -= tmp_int; |
1499 | 1497 | ||
1500 | // limit deviation from hoover point within the target region |
1498 | // limit deviation from hoover point within the target region |
1501 | if( (abs(HeightDeviation) < 150) && (!HeightTrimming) && (HoverGas > 0)) // height setpoint is not changed and hoover gas not zero |
1499 | if( (abs(HeightDeviation) < 150) && (!HeightTrimming) && (HoverGas > 0)) // height setpoint is not changed and hoover gas not zero |
1502 | { |
1500 | { |
1503 | LIMIT_MIN_MAX(HCGas, HoverGasMin, HoverGasMax); // limit gas around the hoover point |
1501 | LIMIT_MIN_MAX(HCGas, HoverGasMin, HoverGasMax); // limit gas around the hoover point |
1504 | } |
1502 | } |
1505 | 1503 | ||
1506 | // strech control output by inverse attitude projection 1/cos |
1504 | // strech control output by inverse attitude projection 1/cos |
1507 | // + 1/cos(angle) ++++++++++++++++++++++++++ |
1505 | // + 1/cos(angle) ++++++++++++++++++++++++++ |
1508 | tmp_long2 = (int32_t)HCGas; |
1506 | tmp_long2 = (int32_t)HCGas; |
1509 | tmp_long2 *= 8192L; |
1507 | tmp_long2 *= 8192L; |
1510 | tmp_long2 /= CosAttitude; |
1508 | tmp_long2 /= CosAttitude; |
1511 | HCGas = (int16_t)tmp_long2; |
1509 | HCGas = (int16_t)tmp_long2; |
1512 | // update height control gas averaging |
1510 | // update height control gas averaging |
1513 | FilterHCGas = (FilterHCGas * (HC_GAS_AVERAGE - 1) + HCGas) / HC_GAS_AVERAGE; |
1511 | FilterHCGas = (FilterHCGas * (HC_GAS_AVERAGE - 1) + HCGas) / HC_GAS_AVERAGE; |
1514 | // limit height control gas pd-control output |
1512 | // limit height control gas pd-control output |
1515 | LIMIT_MIN_MAX(FilterHCGas, EE_Parameter.Hoehe_MinGas * STICK_GAIN, (MAX_GAS - 20) * STICK_GAIN); |
1513 | LIMIT_MIN_MAX(FilterHCGas, EE_Parameter.Hoehe_MinGas * STICK_GAIN, (MAX_GAS - 20) * STICK_GAIN); |
1516 | // set GasMischanteil to HeightControlGasFilter |
1514 | // set GasMischanteil to HeightControlGasFilter |
1517 | if(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) |
1515 | if(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) |
1518 | { // old version |
1516 | { // old version |
1519 | LIMIT_MAX(FilterHCGas, GasMischanteil); // nicht mehr als Gas |
1517 | LIMIT_MAX(FilterHCGas, GasMischanteil); // nicht mehr als Gas |
1520 | } |
1518 | } |
1521 | GasMischanteil = FilterHCGas; |
1519 | GasMischanteil = FilterHCGas; |
1522 | } |
1520 | } |
1523 | }// EOF height control active |
1521 | }// EOF height control active |
1524 | else // HC not active |
1522 | else // HC not active |
1525 | { |
1523 | { |
1526 | //update hoover gas stick value when HC is not active |
1524 | //update hoover gas stick value when HC is not active |
1527 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
1525 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
1528 | { |
1526 | { |
1529 | StickGasHover = HoverGas/STICK_GAIN; // rescale back to stick value |
1527 | StickGasHover = HoverGas/STICK_GAIN; // rescale back to stick value |
1530 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
1528 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
1531 | } |
1529 | } |
1532 | else StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
1530 | else StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
1533 | LIMIT_MIN_MAX(StickGasHover, 70, 150); // reserve some range for trim up and down |
1531 | LIMIT_MIN_MAX(StickGasHover, 70, 150); // reserve some range for trim up and down |
1534 | FilterHCGas = GasMischanteil; |
1532 | FilterHCGas = GasMischanteil; |
1535 | } |
1533 | } |
1536 | 1534 | ||
1537 | // Hover gas estimation by averaging gas control output on small z-velocities |
1535 | // Hover gas estimation by averaging gas control output on small z-velocities |
1538 | // this is done only if height contol option is selected in global config and aircraft is flying |
1536 | // this is done only if height contol option is selected in global config and aircraft is flying |
1539 | if((FCFlags & FCFLAG_FLY) && !(FCFlags & FCFLAG_NOTLANDUNG)) |
1537 | if((FCFlags & FCFLAG_FLY) && !(FCFlags & FCFLAG_NOTLANDUNG)) |
1540 | { |
1538 | { |
1541 | if(HoverGasFilter == 0) HoverGasFilter = HOVER_GAS_AVERAGE * (unsigned long)(GasMischanteil); // init estimation |
1539 | if(HoverGasFilter == 0) HoverGasFilter = HOVER_GAS_AVERAGE * (unsigned long)(GasMischanteil); // init estimation |
1542 | if(abs(VarioMeter) < 100) // only on small vertical speed |
1540 | if(abs(VarioMeter) < 100) // only on small vertical speed |
1543 | { |
1541 | { |
1544 | tmp_long2 = (int32_t)GasMischanteil; // take current thrust |
1542 | tmp_long2 = (int32_t)GasMischanteil; // take current thrust |
1545 | tmp_long2 *= CosAttitude; // apply attitude projection |
1543 | tmp_long2 *= CosAttitude; // apply attitude projection |
1546 | tmp_long2 /= 8192; |
1544 | tmp_long2 /= 8192; |
1547 | 1545 | ||
1548 | // average vertical projected thrust |
1546 | // average vertical projected thrust |
1549 | if(modell_fliegt < 2000) // the first 4 seconds |
1547 | if(modell_fliegt < 2000) // the first 4 seconds |
1550 | { // reduce the time constant of averaging by factor of 8 to get much faster a stable value |
1548 | { // reduce the time constant of averaging by factor of 8 to get much faster a stable value |
1551 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/8L); |
1549 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/8L); |
1552 | HoverGasFilter += 8L * tmp_long2; |
1550 | HoverGasFilter += 8L * tmp_long2; |
1553 | } |
1551 | } |
1554 | else if(modell_fliegt < 4000) // the first 8 seconds |
1552 | else if(modell_fliegt < 4000) // the first 8 seconds |
1555 | { // reduce the time constant of averaging by factor of 4 to get much faster a stable value |
1553 | { // reduce the time constant of averaging by factor of 4 to get much faster a stable value |
1556 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/4L); |
1554 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/4L); |
1557 | HoverGasFilter += 4L * tmp_long2; |
1555 | HoverGasFilter += 4L * tmp_long2; |
1558 | } |
1556 | } |
1559 | else if(modell_fliegt < 8000) // the first 16 seconds |
1557 | else if(modell_fliegt < 8000) // the first 16 seconds |
1560 | { // reduce the time constant of averaging by factor of 2 to get much faster a stable value |
1558 | { // reduce the time constant of averaging by factor of 2 to get much faster a stable value |
1561 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/2L); |
1559 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/2L); |
1562 | HoverGasFilter += 2L * tmp_long2; |
1560 | HoverGasFilter += 2L * tmp_long2; |
1563 | } |
1561 | } |
1564 | else //later |
1562 | else //later |
1565 | { |
1563 | { |
1566 | HoverGasFilter -= HoverGasFilter/HOVER_GAS_AVERAGE; |
1564 | HoverGasFilter -= HoverGasFilter/HOVER_GAS_AVERAGE; |
1567 | HoverGasFilter += tmp_long2; |
1565 | HoverGasFilter += tmp_long2; |
1568 | } |
1566 | } |
1569 | HoverGas = (int16_t)(HoverGasFilter/HOVER_GAS_AVERAGE); |
1567 | HoverGas = (int16_t)(HoverGasFilter/HOVER_GAS_AVERAGE); |
1570 | if(EE_Parameter.Hoehe_HoverBand) |
1568 | if(EE_Parameter.Hoehe_HoverBand) |
1571 | { |
1569 | { |
1572 | int16_t band; |
1570 | int16_t band; |
1573 | band = HoverGas / EE_Parameter.Hoehe_HoverBand; // the higher the parameter the smaller the range |
1571 | band = HoverGas / EE_Parameter.Hoehe_HoverBand; // the higher the parameter the smaller the range |
1574 | HoverGasMin = HoverGas - band; |
1572 | HoverGasMin = HoverGas - band; |
1575 | HoverGasMax = HoverGas + band; |
1573 | HoverGasMax = HoverGas + band; |
1576 | } |
1574 | } |
1577 | else |
1575 | else |
1578 | { // no limit |
1576 | { // no limit |
1579 | HoverGasMin = 0; |
1577 | HoverGasMin = 0; |
1580 | HoverGasMax = 1023; |
1578 | HoverGasMax = 1023; |
1581 | } |
1579 | } |
1582 | } |
1580 | } |
1583 | } |
1581 | } |
1584 | }// EOF ParamSet.GlobalConfig & CFG_HEIGHT_CONTROL |
1582 | }// EOF ParamSet.GlobalConfig & CFG_HEIGHT_CONTROL |
1585 | 1583 | ||
1586 | // limit gas to parameter setting |
1584 | // limit gas to parameter setting |
1587 | LIMIT_MIN(GasMischanteil, (MIN_GAS + 10) * STICK_GAIN); |
1585 | LIMIT_MIN(GasMischanteil, (MIN_GAS + 10) * STICK_GAIN); |
1588 | if(GasMischanteil > (MAX_GAS - 20) * STICK_GAIN) GasMischanteil = (MAX_GAS - 20) * STICK_GAIN; |
1586 | if(GasMischanteil > (MAX_GAS - 20) * STICK_GAIN) GasMischanteil = (MAX_GAS - 20) * STICK_GAIN; |
1589 | 1587 | ||
1590 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1588 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1591 | // all BL-Ctrl connected? |
1589 | // all BL-Ctrl connected? |
1592 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1590 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1593 | if(MissingMotor) |
1591 | if(MissingMotor) |
1594 | if(modell_fliegt > 1 && modell_fliegt < 50 && GasMischanteil > 0) |
1592 | if(modell_fliegt > 1 && modell_fliegt < 50 && GasMischanteil > 0) |
1595 | { |
1593 | { |
1596 | modell_fliegt = 1; |
1594 | modell_fliegt = 1; |
1597 | GasMischanteil = MIN_GAS; |
1595 | GasMischanteil = MIN_GAS; |
1598 | } |
1596 | } |
1599 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1597 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1600 | // + Mischer und PI-Regler |
1598 | // + Mischer und PI-Regler |
1601 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1599 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1602 | DebugOut.Analog[7] = GasMischanteil; |
1600 | DebugOut.Analog[7] = GasMischanteil; |
1603 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1601 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1604 | // Gier-Anteil |
1602 | // Gier-Anteil |
1605 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1603 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1606 | GierMischanteil = MesswertGier - sollGier * STICK_GAIN; // Regler für Gier |
1604 | GierMischanteil = MesswertGier - sollGier * STICK_GAIN; // Regler für Gier |
1607 | #define MIN_GIERGAS (40*STICK_GAIN) // unter diesem Gaswert trotzdem Gieren |
1605 | #define MIN_GIERGAS (40*STICK_GAIN) // unter diesem Gaswert trotzdem Gieren |
1608 | if(GasMischanteil > MIN_GIERGAS) |
1606 | if(GasMischanteil > MIN_GIERGAS) |
1609 | { |
1607 | { |
1610 | if(GierMischanteil > (GasMischanteil / 2)) GierMischanteil = GasMischanteil / 2; |
1608 | if(GierMischanteil > (GasMischanteil / 2)) GierMischanteil = GasMischanteil / 2; |
1611 | if(GierMischanteil < -(GasMischanteil / 2)) GierMischanteil = -(GasMischanteil / 2); |
1609 | if(GierMischanteil < -(GasMischanteil / 2)) GierMischanteil = -(GasMischanteil / 2); |
1612 | } |
1610 | } |
1613 | else |
1611 | else |
1614 | { |
1612 | { |
1615 | if(GierMischanteil > (MIN_GIERGAS / 2)) GierMischanteil = MIN_GIERGAS / 2; |
1613 | if(GierMischanteil > (MIN_GIERGAS / 2)) GierMischanteil = MIN_GIERGAS / 2; |
1616 | if(GierMischanteil < -(MIN_GIERGAS / 2)) GierMischanteil = -(MIN_GIERGAS / 2); |
1614 | if(GierMischanteil < -(MIN_GIERGAS / 2)) GierMischanteil = -(MIN_GIERGAS / 2); |
1617 | } |
1615 | } |
1618 | tmp_int = MAX_GAS*STICK_GAIN; |
1616 | tmp_int = MAX_GAS*STICK_GAIN; |
1619 | if(GierMischanteil > ((tmp_int - GasMischanteil))) GierMischanteil = ((tmp_int - GasMischanteil)); |
1617 | if(GierMischanteil > ((tmp_int - GasMischanteil))) GierMischanteil = ((tmp_int - GasMischanteil)); |
1620 | if(GierMischanteil < -((tmp_int - GasMischanteil))) GierMischanteil = -((tmp_int - GasMischanteil)); |
1618 | if(GierMischanteil < -((tmp_int - GasMischanteil))) GierMischanteil = -((tmp_int - GasMischanteil)); |
1621 | 1619 | ||
1622 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1620 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1623 | // Nick-Achse |
1621 | // Nick-Achse |
1624 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1622 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1625 | DiffNick = MesswertNick - StickNick; // Differenz bestimmen |
1623 | DiffNick = MesswertNick - StickNick; // Differenz bestimmen |
1626 | if(IntegralFaktor) SummeNick += IntegralNickMalFaktor - StickNick; // I-Anteil bei Winkelregelung |
1624 | if(IntegralFaktor) SummeNick += IntegralNickMalFaktor - StickNick; // I-Anteil bei Winkelregelung |
1627 | else SummeNick += DiffNick; // I-Anteil bei HH |
1625 | else SummeNick += DiffNick; // I-Anteil bei HH |
1628 | if(SummeNick > (STICK_GAIN * 16000L)) SummeNick = (STICK_GAIN * 16000L); |
1626 | if(SummeNick > (STICK_GAIN * 16000L)) SummeNick = (STICK_GAIN * 16000L); |
1629 | if(SummeNick < -(16000L * STICK_GAIN)) SummeNick = -(16000L * STICK_GAIN); |
1627 | if(SummeNick < -(16000L * STICK_GAIN)) SummeNick = -(16000L * STICK_GAIN); |
1630 | pd_ergebnis_nick = DiffNick + SummeNick / Ki; // PI-Regler für Nick |
1628 | pd_ergebnis_nick = DiffNick + SummeNick / Ki; // PI-Regler für Nick |
1631 | // Motor Vorn |
1629 | // Motor Vorn |
1632 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / (64/2); |
1630 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / (64/2); |
1633 | if(pd_ergebnis_nick > tmp_int) pd_ergebnis_nick = tmp_int; |
1631 | if(pd_ergebnis_nick > tmp_int) pd_ergebnis_nick = tmp_int; |
1634 | if(pd_ergebnis_nick < -tmp_int) pd_ergebnis_nick = -tmp_int; |
1632 | if(pd_ergebnis_nick < -tmp_int) pd_ergebnis_nick = -tmp_int; |
1635 | 1633 | ||
1636 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1634 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1637 | // Roll-Achse |
1635 | // Roll-Achse |
1638 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1636 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1639 | DiffRoll = MesswertRoll - StickRoll; // Differenz bestimmen |
1637 | DiffRoll = MesswertRoll - StickRoll; // Differenz bestimmen |
1640 | if(IntegralFaktor) SummeRoll += IntegralRollMalFaktor - StickRoll;// I-Anteil bei Winkelregelung |
1638 | if(IntegralFaktor) SummeRoll += IntegralRollMalFaktor - StickRoll;// I-Anteil bei Winkelregelung |
1641 | else SummeRoll += DiffRoll; // I-Anteil bei HH |
1639 | else SummeRoll += DiffRoll; // I-Anteil bei HH |
1642 | if(SummeRoll > (STICK_GAIN * 16000L)) SummeRoll = (STICK_GAIN * 16000L); |
1640 | if(SummeRoll > (STICK_GAIN * 16000L)) SummeRoll = (STICK_GAIN * 16000L); |
1643 | if(SummeRoll < -(16000L * STICK_GAIN)) SummeRoll = -(16000L * STICK_GAIN); |
1641 | if(SummeRoll < -(16000L * STICK_GAIN)) SummeRoll = -(16000L * STICK_GAIN); |
1644 | pd_ergebnis_roll = DiffRoll + SummeRoll / Ki; // PI-Regler für Roll |
1642 | pd_ergebnis_roll = DiffRoll + SummeRoll / Ki; // PI-Regler für Roll |
1645 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / (64/2); |
1643 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / (64/2); |
1646 | if(pd_ergebnis_roll > tmp_int) pd_ergebnis_roll = tmp_int; |
1644 | if(pd_ergebnis_roll > tmp_int) pd_ergebnis_roll = tmp_int; |
1647 | if(pd_ergebnis_roll < -tmp_int) pd_ergebnis_roll = -tmp_int; |
1645 | if(pd_ergebnis_roll < -tmp_int) pd_ergebnis_roll = -tmp_int; |
1648 | 1646 | ||
1649 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1647 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1650 | // Universal Mixer |
1648 | // Universal Mixer |
1651 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1649 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1652 | for(i=0; i<MAX_MOTORS; i++) |
1650 | for(i=0; i<MAX_MOTORS; i++) |
1653 | { |
1651 | { |
1654 | signed int tmp_int; |
1652 | signed int tmp_int; |
1655 | if(Mixer.Motor[i][0] > 0) |
1653 | if(Mixer.Motor[i][0] > 0) |
1656 | { |
1654 | { |
1657 | // Gas |
1655 | // Gas |
1658 | if(Mixer.Motor[i][0] == 64) tmp_int = GasMischanteil * 2; else tmp_int = ((long)GasMischanteil * Mixer.Motor[i][0]) / 32L; |
1656 | if(Mixer.Motor[i][0] == 64) tmp_int = GasMischanteil * 2; else tmp_int = ((long)GasMischanteil * Mixer.Motor[i][0]) / 32L; |
1659 | // Nick |
1657 | // Nick |
1660 | if(Mixer.Motor[i][1] == 64) tmp_int += pd_ergebnis_nick; |
1658 | if(Mixer.Motor[i][1] == 64) tmp_int += pd_ergebnis_nick; |
1661 | else if(Mixer.Motor[i][1] == -64) tmp_int -= pd_ergebnis_nick; |
1659 | else if(Mixer.Motor[i][1] == -64) tmp_int -= pd_ergebnis_nick; |
1662 | else tmp_int += ((long)pd_ergebnis_nick * Mixer.Motor[i][1]) / 64L; |
1660 | else tmp_int += ((long)pd_ergebnis_nick * Mixer.Motor[i][1]) / 64L; |
1663 | // Roll |
1661 | // Roll |
1664 | if(Mixer.Motor[i][2] == 64) tmp_int += pd_ergebnis_roll; |
1662 | if(Mixer.Motor[i][2] == 64) tmp_int += pd_ergebnis_roll; |
1665 | else if(Mixer.Motor[i][2] == -64) tmp_int -= pd_ergebnis_roll; |
1663 | else if(Mixer.Motor[i][2] == -64) tmp_int -= pd_ergebnis_roll; |
1666 | else tmp_int += ((long)pd_ergebnis_roll * Mixer.Motor[i][2]) / 64L; |
1664 | else tmp_int += ((long)pd_ergebnis_roll * Mixer.Motor[i][2]) / 64L; |
1667 | // Gier |
1665 | // Gier |
1668 | if(Mixer.Motor[i][3] == 64) tmp_int += GierMischanteil * 2; |
1666 | if(Mixer.Motor[i][3] == 64) tmp_int += GierMischanteil * 2; |
1669 | else if(Mixer.Motor[i][3] == -64) tmp_int -= GierMischanteil * 2; |
1667 | else if(Mixer.Motor[i][3] == -64) tmp_int -= GierMischanteil * 2; |
1670 | else tmp_int += ((long)GierMischanteil * Mixer.Motor[i][3]) / 32L; |
1668 | else tmp_int += ((long)GierMischanteil * Mixer.Motor[i][3]) / 32L; |
1671 | /* |
1669 | /* |
1672 | if(tmp_int > tmp_motorwert[i]) tmp_int = (tmp_motorwert[i] + tmp_int) / 2; // MotorSmoothing |
1670 | if(tmp_int > tmp_motorwert[i]) tmp_int = (tmp_motorwert[i] + tmp_int) / 2; // MotorSmoothing |
1673 | else tmp_int = 2 * tmp_int - tmp_motorwert[i]; // MotorSmoothing |
1671 | else tmp_int = 2 * tmp_int - tmp_motorwert[i]; // MotorSmoothing |
1674 | 1672 | ||
1675 | if(Poti2 > 50) |
1673 | if(Poti2 > 50) |
1676 | { |
1674 | { |
1677 | if(tmp_int > tmp_motorwert[i]) tmp_int = (tmp_motorwert[i] + tmp_int) / 2; // MotorSmoothing |
1675 | if(tmp_int > tmp_motorwert[i]) tmp_int = (tmp_motorwert[i] + tmp_int) / 2; // MotorSmoothing |
1678 | else if(Poti2 > 150) tmp_int = 2 * tmp_int - tmp_motorwert[i]; // MotorSmoothing |
1676 | else if(Poti2 > 150) tmp_int = 2 * tmp_int - tmp_motorwert[i]; // MotorSmoothing |
1679 | } |
1677 | } |
1680 | */ |
1678 | */ |
1681 | LIMIT_MIN_MAX(tmp_int,MIN_GAS * 8,MAX_GAS * 8); |
1679 | LIMIT_MIN_MAX(tmp_int,MIN_GAS * 8,MAX_GAS * 8); |
1682 | Motor[i].SetPoint = tmp_int / 8; |
1680 | Motor[i].SetPoint = tmp_int / 8; |
1683 | Motor[i].SetPointLowerBits = tmp_int % 8; |
1681 | Motor[i].SetPointLowerBits = tmp_int % 8; |
1684 | tmp_motorwert[i] = tmp_int; |
1682 | tmp_motorwert[i] = tmp_int; |
1685 | } |
1683 | } |
1686 | else |
1684 | else |
1687 | { |
1685 | { |
1688 | Motor[i].SetPoint = 0; |
1686 | Motor[i].SetPoint = 0; |
1689 | Motor[i].SetPointLowerBits = 0; |
1687 | Motor[i].SetPointLowerBits = 0; |
1690 | } |
1688 | } |
1691 | } |
1689 | } |
1692 | } |
1690 | } |
1693 | 1691 |