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1 | ingob | 1 | /*####################################################################################### |
2 | Flight Control |
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3 | #######################################################################################*/ |
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4 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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5 | // + Copyright (c) 04.2007 Holger Buss |
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6 | // + Nur für den privaten Gebrauch |
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7 | // + www.MikroKopter.com |
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8 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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1051 | killagreg | 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. |
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11 | // + Sollten direkte oder indirekte kommerzielle Absichten verfolgt werden, ist mit uns (info@mikrokopter.de) Kontakt |
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12 | // + bzgl. der Nutzungsbedingungen aufzunehmen. |
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1 | ingob | 13 | // + Eine kommerzielle Nutzung ist z.B.Verkauf von MikroKoptern, Bestückung und Verkauf von Platinen oder Bausätzen, |
14 | // + Verkauf von Luftbildaufnahmen, usw. |
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15 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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1051 | killagreg | 16 | // + Werden Teile des Quellcodes (mit oder ohne Modifikation) weiterverwendet oder veröffentlicht, |
1 | ingob | 17 | // + unterliegen sie auch diesen Nutzungsbedingungen und diese Nutzungsbedingungen incl. Copyright müssen dann beiliegen |
18 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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19 | // + Sollte die Software (auch auszugesweise) oder sonstige Informationen des MikroKopter-Projekts |
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20 | // + auf anderen Webseiten oder sonstigen Medien veröffentlicht werden, muss unsere Webseite "http://www.mikrokopter.de" |
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21 | // + eindeutig als Ursprung verlinkt werden |
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22 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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23 | // + Keine Gewähr auf Fehlerfreiheit, Vollständigkeit oder Funktion |
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24 | // + Benutzung auf eigene Gefahr |
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25 | // + Wir übernehmen keinerlei Haftung für direkte oder indirekte Personen- oder Sachschäden |
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26 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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1051 | killagreg | 27 | // + Die Portierung der Software (oder Teile davon) auf andere Systeme (ausser der Hardware von www.mikrokopter.de) ist nur |
1 | ingob | 28 | // + mit unserer Zustimmung zulässig |
29 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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30 | // + Die Funktion printf_P() unterliegt ihrer eigenen Lizenz und ist hiervon nicht betroffen |
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31 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
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1051 | killagreg | 32 | // + Redistributions of source code (with or without modifications) must retain the above copyright notice, |
1 | ingob | 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 |
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35 | // + from this software without specific prior written permission. |
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1051 | killagreg | 36 | // + * The use of this project (hardware, software, binary files, sources and documentation) is only permittet |
1 | ingob | 37 | // + for non-commercial use (directly or indirectly) |
1051 | killagreg | 38 | // + Commercial use (for excample: selling of MikroKopters, selling of PCBs, assembly, ...) is only permitted |
1 | ingob | 39 | // + with our written permission |
1051 | killagreg | 40 | // + * If sources or documentations are redistributet on other webpages, out webpage (http://www.MikroKopter.de) must be |
41 | // + clearly linked as origin |
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831 | hbuss | 42 | // + * porting to systems other than hardware from www.mikrokopter.de is not allowed |
1 | ingob | 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 |
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45 | // + IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE |
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46 | // + ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER OR CONTRIBUTORS BE |
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47 | // + LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR |
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48 | // + CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF |
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49 | // + SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS |
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1322 | hbuss | 50 | // + INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN |
51 | // + CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) |
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1 | ingob | 52 | // + ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
1051 | killagreg | 53 | // + POSSIBILITY OF SUCH DAMAGE. |
1 | ingob | 54 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
55 | |||
56 | #include "main.h" |
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395 | hbuss | 57 | #include "eeprom.c" |
1320 | hbuss | 58 | #include "mymath.h" |
1 | ingob | 59 | |
1322 | hbuss | 60 | unsigned char h,m,s,BaroExpandActive = 0; |
173 | holgerb | 61 | volatile unsigned int I2CTimeout = 100; |
1153 | hbuss | 62 | int MesswertNick,MesswertRoll,MesswertGier,MesswertGierBias, RohMesswertNick,RohMesswertRoll; |
1166 | hbuss | 63 | int TrimNick, TrimRoll; |
1051 | killagreg | 64 | int AdNeutralGierBias; |
927 | hbuss | 65 | int AdNeutralNick = 0,AdNeutralRoll = 0,AdNeutralGier = 0,StartNeutralRoll = 0,StartNeutralNick = 0; |
66 | int Mittelwert_AccNick, Mittelwert_AccRoll,Mittelwert_AccHoch, NeutralAccX=0, NeutralAccY=0; |
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805 | hbuss | 67 | int NaviAccNick, NaviAccRoll,NaviCntAcc = 0; |
1 | ingob | 68 | volatile float NeutralAccZ = 0; |
69 | unsigned char CosinusNickWinkel = 0, CosinusRollWinkel = 0; |
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693 | hbuss | 70 | long IntegralNick = 0,IntegralNick2 = 0; |
71 | long IntegralRoll = 0,IntegralRoll2 = 0; |
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72 | long IntegralAccNick = 0,IntegralAccRoll = 0,IntegralAccZ = 0; |
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73 | long Integral_Gier = 0; |
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74 | long Mess_IntegralNick = 0,Mess_IntegralNick2 = 0; |
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75 | long Mess_IntegralRoll = 0,Mess_IntegralRoll2 = 0; |
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76 | long Mess_Integral_Gier = 0,Mess_Integral_Gier2 = 0; |
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77 | long MittelIntegralNick,MittelIntegralRoll,MittelIntegralNick2,MittelIntegralRoll2; |
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1 | ingob | 78 | volatile long Mess_Integral_Hoch = 0; |
1153 | hbuss | 79 | int KompassValue = 0; |
80 | int KompassStartwert = 0; |
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81 | int KompassRichtung = 0; |
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693 | hbuss | 82 | unsigned int KompassSignalSchlecht = 500; |
855 | hbuss | 83 | unsigned char MAX_GAS,MIN_GAS; |
1 | ingob | 84 | unsigned char HoehenReglerAktiv = 0; |
880 | hbuss | 85 | unsigned char TrichterFlug = 0; |
395 | hbuss | 86 | long Umschlag180Nick = 250000L, Umschlag180Roll = 250000L; |
693 | hbuss | 87 | long ErsatzKompass; |
88 | int ErsatzKompassInGrad; // Kompasswert in Grad |
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89 | int GierGyroFehler = 0; |
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1211 | hbuss | 90 | char GyroFaktor,GyroFaktorGier; |
91 | char IntegralFaktor,IntegralFaktorGier; |
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1153 | hbuss | 92 | int DiffNick,DiffRoll; |
1051 | killagreg | 93 | int Poti1 = 0, Poti2 = 0, Poti3 = 0, Poti4 = 0; |
1 | ingob | 94 | volatile unsigned char SenderOkay = 0; |
1243 | killagreg | 95 | volatile unsigned char SenderRSSI = 0; |
595 | hbuss | 96 | int StickNick = 0,StickRoll = 0,StickGier = 0,StickGas = 0; |
1 | ingob | 97 | char MotorenEin = 0; |
1246 | killagreg | 98 | long HoehenWert = 0; |
99 | long SollHoehe = 0; |
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498 | hbuss | 100 | int LageKorrekturRoll = 0,LageKorrekturNick = 0; |
1153 | hbuss | 101 | //float Ki = FAKTOR_I; |
102 | int Ki = 10300 / 33; |
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395 | hbuss | 103 | unsigned char Looping_Nick = 0,Looping_Roll = 0; |
104 | unsigned char Looping_Links = 0, Looping_Rechts = 0, Looping_Unten = 0, Looping_Oben = 0; |
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1 | ingob | 105 | |
106 | unsigned char Parameter_Luftdruck_D = 48; // Wert : 0-250 |
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107 | unsigned char Parameter_MaxHoehe = 251; // Wert : 0-250 |
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108 | unsigned char Parameter_Hoehe_P = 16; // Wert : 0-32 |
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109 | unsigned char Parameter_Hoehe_ACC_Wirkung = 58; // Wert : 0-250 |
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110 | unsigned char Parameter_KompassWirkung = 64; // Wert : 0-250 |
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1283 | hbuss | 111 | unsigned char Parameter_Hoehe_GPS_Z = 64; // Wert : 0-250 |
1111 | hbuss | 112 | unsigned char Parameter_Gyro_D = 8; // Wert : 0-250 |
173 | holgerb | 113 | unsigned char Parameter_Gyro_P = 150; // Wert : 10-250 |
1 | ingob | 114 | unsigned char Parameter_Gyro_I = 150; // Wert : 0-250 |
1322 | hbuss | 115 | unsigned char Parameter_Gyro_Gier_P = 150; // Wert : 10-250 |
116 | unsigned char Parameter_Gyro_Gier_I = 150; // Wert : 10-250 |
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1 | ingob | 117 | unsigned char Parameter_Gier_P = 2; // Wert : 1-20 |
118 | unsigned char Parameter_I_Faktor = 10; // Wert : 1-20 |
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119 | unsigned char Parameter_UserParam1 = 0; |
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120 | unsigned char Parameter_UserParam2 = 0; |
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121 | unsigned char Parameter_UserParam3 = 0; |
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122 | unsigned char Parameter_UserParam4 = 0; |
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499 | hbuss | 123 | unsigned char Parameter_UserParam5 = 0; |
124 | unsigned char Parameter_UserParam6 = 0; |
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125 | unsigned char Parameter_UserParam7 = 0; |
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126 | unsigned char Parameter_UserParam8 = 0; |
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1 | ingob | 127 | unsigned char Parameter_ServoNickControl = 100; |
1232 | hbuss | 128 | unsigned char Parameter_ServoRollControl = 100; |
173 | holgerb | 129 | unsigned char Parameter_LoopGasLimit = 70; |
1120 | hbuss | 130 | unsigned char Parameter_AchsKopplung1 = 90; |
131 | unsigned char Parameter_AchsKopplung2 = 65; |
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132 | unsigned char Parameter_CouplingYawCorrection = 64; |
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133 | //unsigned char Parameter_AchsGegenKopplung1 = 0; |
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499 | hbuss | 134 | unsigned char Parameter_DynamicStability = 100; |
921 | hbuss | 135 | unsigned char Parameter_J16Bitmask; // for the J16 Output |
136 | unsigned char Parameter_J16Timing; // for the J16 Output |
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137 | unsigned char Parameter_J17Bitmask; // for the J17 Output |
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138 | unsigned char Parameter_J17Timing; // for the J17 Output |
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139 | unsigned char Parameter_NaviGpsModeControl; // Parameters for the Naviboard |
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1051 | killagreg | 140 | unsigned char Parameter_NaviGpsGain; |
141 | unsigned char Parameter_NaviGpsP; |
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142 | unsigned char Parameter_NaviGpsI; |
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143 | unsigned char Parameter_NaviGpsD; |
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144 | unsigned char Parameter_NaviGpsACC; |
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993 | hbuss | 145 | unsigned char Parameter_NaviOperatingRadius; |
146 | unsigned char Parameter_NaviWindCorrection; |
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147 | unsigned char Parameter_NaviSpeedCompensation; |
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921 | hbuss | 148 | unsigned char Parameter_ExternalControl; |
1 | ingob | 149 | struct mk_param_struct EE_Parameter; |
492 | hbuss | 150 | signed int ExternStickNick = 0,ExternStickRoll = 0,ExternStickGier = 0, ExternHoehenValue = -20; |
614 | hbuss | 151 | int MaxStickNick = 0,MaxStickRoll = 0; |
871 | hbuss | 152 | unsigned int modell_fliegt = 0; |
1209 | hbuss | 153 | volatile unsigned char MikroKopterFlags = 0; |
1121 | hbuss | 154 | long GIER_GRAD_FAKTOR = 1291; |
1153 | hbuss | 155 | signed int KopplungsteilNickRoll,KopplungsteilRollNick; |
1209 | hbuss | 156 | unsigned char RequiredMotors = 4; |
157 | unsigned char Motor[MAX_MOTORS]; |
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158 | signed int tmp_motorwert[MAX_MOTORS]; |
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1328 | hbuss | 159 | unsigned char LoadHandler = 0; |
1309 | hbuss | 160 | #define LIMIT_MIN(value, min) {if(value < min) value = min;} |
161 | #define LIMIT_MAX(value, max) {if(value > max) value = max;} |
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162 | #define LIMIT_MIN_MAX(value, min, max) {if(value < min) value = min; else if(value > max) value = max;} |
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1155 | hbuss | 163 | |
1166 | hbuss | 164 | int MotorSmoothing(int neu, int alt) |
165 | { |
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166 | int motor; |
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167 | if(neu > alt) motor = (1*(int)alt + neu) / 2; |
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168 | else motor = neu - (alt - neu)*1; |
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169 | //if(Poti2 < 20) return(neu); |
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170 | return(motor); |
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171 | } |
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172 | |||
1232 | hbuss | 173 | void Piep(unsigned char Anzahl, unsigned int dauer) |
1 | ingob | 174 | { |
1232 | hbuss | 175 | if(MotorenEin) return; //auf keinen Fall im Flug! |
1 | ingob | 176 | while(Anzahl--) |
177 | { |
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1232 | hbuss | 178 | beeptime = dauer; |
179 | while(beeptime); |
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180 | Delay_ms(dauer * 2); |
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1 | ingob | 181 | } |
182 | } |
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183 | |||
184 | //############################################################################ |
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185 | // Nullwerte ermitteln |
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186 | void SetNeutral(void) |
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187 | //############################################################################ |
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188 | { |
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1111 | hbuss | 189 | unsigned char i; |
190 | unsigned int gier_neutral=0, nick_neutral=0, roll_neutral=0; |
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1320 | hbuss | 191 | HEF4017R_ON; |
1051 | killagreg | 192 | NeutralAccX = 0; |
1 | ingob | 193 | NeutralAccY = 0; |
194 | NeutralAccZ = 0; |
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1051 | killagreg | 195 | AdNeutralNick = 0; |
196 | AdNeutralRoll = 0; |
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1 | ingob | 197 | AdNeutralGier = 0; |
927 | hbuss | 198 | AdNeutralGierBias = 0; |
395 | hbuss | 199 | Parameter_AchsKopplung1 = 0; |
1120 | hbuss | 200 | Parameter_AchsKopplung2 = 0; |
1036 | hbuss | 201 | ExpandBaro = 0; |
1051 | killagreg | 202 | CalibrierMittelwert(); |
395 | hbuss | 203 | Delay_ms_Mess(100); |
1 | ingob | 204 | CalibrierMittelwert(); |
205 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
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1051 | killagreg | 206 | { |
1 | ingob | 207 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
208 | } |
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1166 | hbuss | 209 | #define NEUTRAL_FILTER 32 |
210 | for(i=0; i<NEUTRAL_FILTER; i++) |
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1111 | hbuss | 211 | { |
212 | Delay_ms_Mess(10); |
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1216 | killagreg | 213 | gier_neutral += AdWertGier; |
1166 | hbuss | 214 | nick_neutral += AdWertNick; |
215 | roll_neutral += AdWertRoll; |
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1111 | hbuss | 216 | } |
1173 | hbuss | 217 | AdNeutralNick= (nick_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
218 | AdNeutralRoll= (roll_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
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219 | AdNeutralGier= (gier_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER); |
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1111 | hbuss | 220 | AdNeutralGierBias = AdNeutralGier; |
401 | hbuss | 221 | StartNeutralRoll = AdNeutralRoll; |
222 | StartNeutralNick = AdNeutralNick; |
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1051 | killagreg | 223 | if(eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_NICK]) > 4) |
513 | hbuss | 224 | { |
1171 | hbuss | 225 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
226 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
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513 | hbuss | 227 | NeutralAccZ = Aktuell_az; |
228 | } |
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1051 | killagreg | 229 | else |
513 | hbuss | 230 | { |
231 | NeutralAccX = (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_NICK]) * 256 + (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_NICK+1]); |
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232 | NeutralAccY = (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL]) * 256 + (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL+1]); |
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233 | NeutralAccZ = (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_Z]) * 256 + (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_Z+1]); |
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234 | } |
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1051 | killagreg | 235 | |
1 | ingob | 236 | MesswertNick = 0; |
237 | MesswertRoll = 0; |
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238 | MesswertGier = 0; |
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1111 | hbuss | 239 | Delay_ms_Mess(100); |
1174 | hbuss | 240 | Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
241 | Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
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1173 | hbuss | 242 | IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
243 | IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
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244 | Mess_IntegralNick2 = IntegralNick; |
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245 | Mess_IntegralRoll2 = IntegralRoll; |
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246 | Mess_Integral_Gier = 0; |
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1 | ingob | 247 | StartLuftdruck = Luftdruck; |
1253 | killagreg | 248 | VarioMeter = 0; |
1 | ingob | 249 | Mess_Integral_Hoch = 0; |
250 | KompassStartwert = KompassValue; |
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251 | GPS_Neutral(); |
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1051 | killagreg | 252 | beeptime = 50; |
882 | hbuss | 253 | Umschlag180Nick = ((long) EE_Parameter.WinkelUmschlagNick * 2500L) + 15000L; |
254 | Umschlag180Roll = ((long) EE_Parameter.WinkelUmschlagRoll * 2500L) + 15000L; |
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492 | hbuss | 255 | ExternHoehenValue = 0; |
693 | hbuss | 256 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
257 | GierGyroFehler = 0; |
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723 | hbuss | 258 | SendVersionToNavi = 1; |
921 | hbuss | 259 | LED_Init(); |
260 | MikroKopterFlags |= FLAG_CALIBRATE; |
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992 | hbuss | 261 | FromNaviCtrl_Value.Kalman_K = -1; |
1173 | hbuss | 262 | FromNaviCtrl_Value.Kalman_MaxDrift = 0; |
992 | hbuss | 263 | FromNaviCtrl_Value.Kalman_MaxFusion = 32; |
1172 | hbuss | 264 | Poti1 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110; |
265 | Poti2 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110; |
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266 | Poti3 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110; |
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267 | Poti4 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110; |
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1171 | hbuss | 268 | SenderOkay = 100; |
1320 | hbuss | 269 | if(ServoActive) |
270 | { |
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271 | HEF4017R_ON; |
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272 | DDRD |=0x80; // enable J7 -> Servo signal |
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273 | } |
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1 | ingob | 274 | } |
275 | |||
276 | //############################################################################ |
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395 | hbuss | 277 | // Bearbeitet die Messwerte |
1 | ingob | 278 | void Mittelwert(void) |
279 | //############################################################################ |
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1051 | killagreg | 280 | { |
1111 | hbuss | 281 | static signed long tmpl,tmpl2,tmpl3,tmpl4; |
282 | static signed int oldNick, oldRoll, d2Roll, d2Nick; |
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1153 | hbuss | 283 | signed long winkel_nick, winkel_roll; |
1171 | hbuss | 284 | |
1111 | hbuss | 285 | MesswertGier = (signed int) AdNeutralGier - AdWertGier; |
286 | // MesswertGierBias = (signed int) AdNeutralGierBias - AdWertGier; |
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1171 | hbuss | 287 | MesswertNick = (signed int) AdWertNickFilter / 8; |
288 | MesswertRoll = (signed int) AdWertRollFilter / 8; |
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1153 | hbuss | 289 | RohMesswertNick = MesswertNick; |
290 | RohMesswertRoll = MesswertRoll; |
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1166 | hbuss | 291 | |
395 | hbuss | 292 | // Beschleunigungssensor ++++++++++++++++++++++++++++++++++++++++++++++++ |
1166 | hbuss | 293 | Mittelwert_AccNick = ((long)Mittelwert_AccNick * 3 + ((ACC_AMPLIFY * (long)AdWertAccNick))) / 4L; |
294 | Mittelwert_AccRoll = ((long)Mittelwert_AccRoll * 3 + ((ACC_AMPLIFY * (long)AdWertAccRoll))) / 4L; |
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295 | Mittelwert_AccHoch = ((long)Mittelwert_AccHoch * 3 + ((long)AdWertAccHoch)) / 4L; |
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395 | hbuss | 296 | IntegralAccNick += ACC_AMPLIFY * AdWertAccNick; |
297 | IntegralAccRoll += ACC_AMPLIFY * AdWertAccRoll; |
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805 | hbuss | 298 | NaviAccNick += AdWertAccNick; |
299 | NaviAccRoll += AdWertAccRoll; |
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300 | NaviCntAcc++; |
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1153 | hbuss | 301 | IntegralAccZ += Aktuell_az - NeutralAccZ; |
302 | |||
1155 | hbuss | 303 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
304 | // ADC einschalten |
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1171 | hbuss | 305 | ANALOG_ON; |
1155 | hbuss | 306 | AdReady = 0; |
307 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
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308 | |||
1216 | killagreg | 309 | if(Mess_IntegralRoll > 93000L) winkel_roll = 93000L; |
310 | else if(Mess_IntegralRoll <-93000L) winkel_roll = -93000L; |
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1153 | hbuss | 311 | else winkel_roll = Mess_IntegralRoll; |
312 | |||
1216 | killagreg | 313 | if(Mess_IntegralNick > 93000L) winkel_nick = 93000L; |
314 | else if(Mess_IntegralNick <-93000L) winkel_nick = -93000L; |
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1153 | hbuss | 315 | else winkel_nick = Mess_IntegralNick; |
316 | |||
1120 | hbuss | 317 | // Gier ++++++++++++++++++++++++++++++++++++++++++++++++ |
1153 | hbuss | 318 | Mess_Integral_Gier += MesswertGier; |
319 | ErsatzKompass += MesswertGier; |
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395 | hbuss | 320 | // Kopplungsanteil +++++++++++++++++++++++++++++++++++++ |
321 | if(!Looping_Nick && !Looping_Roll && (EE_Parameter.GlobalConfig & CFG_ACHSENKOPPLUNG_AKTIV)) |
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322 | { |
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1153 | hbuss | 323 | tmpl3 = (MesswertRoll * winkel_nick) / 2048L; |
1120 | hbuss | 324 | tmpl3 *= Parameter_AchsKopplung2; //65 |
1111 | hbuss | 325 | tmpl3 /= 4096L; |
1153 | hbuss | 326 | tmpl4 = (MesswertNick * winkel_roll) / 2048L; |
1216 | killagreg | 327 | tmpl4 *= Parameter_AchsKopplung2; //65 |
1111 | hbuss | 328 | tmpl4 /= 4096L; |
1153 | hbuss | 329 | KopplungsteilNickRoll = tmpl3; |
330 | KopplungsteilRollNick = tmpl4; |
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1111 | hbuss | 331 | tmpl4 -= tmpl3; |
332 | ErsatzKompass += tmpl4; |
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1166 | hbuss | 333 | if(!Parameter_CouplingYawCorrection) Mess_Integral_Gier -= tmpl4/2; // Gier nachhelfen |
1111 | hbuss | 334 | |
1153 | hbuss | 335 | tmpl = ((MesswertGier + tmpl4) * winkel_nick) / 2048L; |
1111 | hbuss | 336 | tmpl *= Parameter_AchsKopplung1; // 90 |
880 | hbuss | 337 | tmpl /= 4096L; |
1153 | hbuss | 338 | tmpl2 = ((MesswertGier + tmpl4) * winkel_roll) / 2048L; |
395 | hbuss | 339 | tmpl2 *= Parameter_AchsKopplung1; |
880 | hbuss | 340 | tmpl2 /= 4096L; |
1225 | hbuss | 341 | if(abs(MesswertGier) > 64) if(labs(tmpl) > 128 || labs(tmpl2) > 128) TrichterFlug = 1; |
1153 | hbuss | 342 | //MesswertGier += (Parameter_CouplingYawCorrection * tmpl4) / 256; |
395 | hbuss | 343 | } |
1166 | hbuss | 344 | else tmpl = tmpl2 = KopplungsteilNickRoll = KopplungsteilRollNick = 0; |
1111 | hbuss | 345 | |
1166 | hbuss | 346 | TrimRoll = tmpl - tmpl2 / 100L; |
347 | TrimNick = -tmpl2 + tmpl / 100L; |
||
348 | |||
1111 | hbuss | 349 | // Kompasswert begrenzen ++++++++++++++++++++++++++++++++++++++++++++++++ |
350 | if(ErsatzKompass >= (360L * GIER_GRAD_FAKTOR)) ErsatzKompass -= 360L * GIER_GRAD_FAKTOR; // 360° Umschlag |
||
351 | if(ErsatzKompass < 0) ErsatzKompass += 360L * GIER_GRAD_FAKTOR; |
||
395 | hbuss | 352 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
1166 | hbuss | 353 | Mess_IntegralRoll2 += MesswertRoll + TrimRoll; |
354 | Mess_IntegralRoll += MesswertRoll + TrimRoll - LageKorrekturRoll; |
||
1051 | killagreg | 355 | if(Mess_IntegralRoll > Umschlag180Roll) |
395 | hbuss | 356 | { |
882 | hbuss | 357 | Mess_IntegralRoll = -(Umschlag180Roll - 25000L); |
395 | hbuss | 358 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
1051 | killagreg | 359 | } |
395 | hbuss | 360 | if(Mess_IntegralRoll <-Umschlag180Roll) |
361 | { |
||
882 | hbuss | 362 | Mess_IntegralRoll = (Umschlag180Roll - 25000L); |
395 | hbuss | 363 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
1051 | killagreg | 364 | } |
395 | hbuss | 365 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
1166 | hbuss | 366 | Mess_IntegralNick2 += MesswertNick + TrimNick; |
367 | Mess_IntegralNick += MesswertNick + TrimNick - LageKorrekturNick; |
||
1051 | killagreg | 368 | if(Mess_IntegralNick > Umschlag180Nick) |
882 | hbuss | 369 | { |
370 | Mess_IntegralNick = -(Umschlag180Nick - 25000L); |
||
371 | Mess_IntegralNick2 = Mess_IntegralNick; |
||
1051 | killagreg | 372 | } |
373 | if(Mess_IntegralNick <-Umschlag180Nick) |
||
395 | hbuss | 374 | { |
882 | hbuss | 375 | Mess_IntegralNick = (Umschlag180Nick - 25000L); |
395 | hbuss | 376 | Mess_IntegralNick2 = Mess_IntegralNick; |
1051 | killagreg | 377 | } |
1111 | hbuss | 378 | |
1 | ingob | 379 | Integral_Gier = Mess_Integral_Gier; |
380 | IntegralNick = Mess_IntegralNick; |
||
381 | IntegralRoll = Mess_IntegralRoll; |
||
1051 | killagreg | 382 | IntegralNick2 = Mess_IntegralNick2; |
1 | ingob | 383 | IntegralRoll2 = Mess_IntegralRoll2; |
384 | |||
1166 | hbuss | 385 | #define D_LIMIT 128 |
386 | |||
1171 | hbuss | 387 | MesswertNick = HiResNick / 8; |
388 | MesswertRoll = HiResRoll / 8; |
||
1166 | hbuss | 389 | |
1167 | hbuss | 390 | if(AdWertNick < 15) MesswertNick = -1000; if(AdWertNick < 7) MesswertNick = -2000; |
391 | if(PlatinenVersion == 10) { if(AdWertNick > 1010) MesswertNick = +1000; if(AdWertNick > 1017) MesswertNick = +2000; } |
||
392 | else { if(AdWertNick > 2000) MesswertNick = +1000; if(AdWertNick > 2015) MesswertNick = +2000; } |
||
393 | if(AdWertRoll < 15) MesswertRoll = -1000; if(AdWertRoll < 7) MesswertRoll = -2000; |
||
394 | if(PlatinenVersion == 10) { if(AdWertRoll > 1010) MesswertRoll = +1000; if(AdWertRoll > 1017) MesswertRoll = +2000; } |
||
395 | else { if(AdWertRoll > 2000) MesswertRoll = +1000; if(AdWertRoll > 2015) MesswertRoll = +2000; } |
||
396 | |||
1216 | killagreg | 397 | if(Parameter_Gyro_D) |
1111 | hbuss | 398 | { |
1166 | hbuss | 399 | d2Nick = HiResNick - oldNick; |
400 | oldNick = (oldNick + HiResNick)/2; |
||
1111 | hbuss | 401 | if(d2Nick > D_LIMIT) d2Nick = D_LIMIT; |
402 | else if(d2Nick < -D_LIMIT) d2Nick = -D_LIMIT; |
||
1166 | hbuss | 403 | MesswertNick += (d2Nick * (signed int) Parameter_Gyro_D) / 16; |
404 | d2Roll = HiResRoll - oldRoll; |
||
405 | oldRoll = (oldRoll + HiResRoll)/2; |
||
1111 | hbuss | 406 | if(d2Roll > D_LIMIT) d2Roll = D_LIMIT; |
407 | else if(d2Roll < -D_LIMIT) d2Roll = -D_LIMIT; |
||
1166 | hbuss | 408 | MesswertRoll += (d2Roll * (signed int) Parameter_Gyro_D) / 16; |
409 | HiResNick += (d2Nick * (signed int) Parameter_Gyro_D); |
||
410 | HiResRoll += (d2Roll * (signed int) Parameter_Gyro_D); |
||
1216 | killagreg | 411 | } |
1111 | hbuss | 412 | |
1166 | hbuss | 413 | if(RohMesswertRoll > 0) TrimRoll += ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
414 | else TrimRoll -= ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
||
415 | if(RohMesswertNick > 0) TrimNick += ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
||
416 | else TrimNick -= ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
||
1153 | hbuss | 417 | |
418 | if(EE_Parameter.GlobalConfig & CFG_DREHRATEN_BEGRENZER && !Looping_Nick && !Looping_Roll) |
||
419 | { |
||
420 | if(RohMesswertNick > 256) MesswertNick += 1 * (RohMesswertNick - 256); |
||
421 | else if(RohMesswertNick < -256) MesswertNick += 1 * (RohMesswertNick + 256); |
||
422 | if(RohMesswertRoll > 256) MesswertRoll += 1 * (RohMesswertRoll - 256); |
||
423 | else if(RohMesswertRoll < -256) MesswertRoll += 1 * (RohMesswertRoll + 256); |
||
424 | } |
||
425 | |||
1 | ingob | 426 | if(Poti1 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110) Poti1++; else if(Poti1 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110 && Poti1) Poti1--; |
427 | if(Poti2 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110) Poti2++; else if(Poti2 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110 && Poti2) Poti2--; |
||
428 | if(Poti3 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110) Poti3++; else if(Poti3 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110 && Poti3) Poti3--; |
||
429 | if(Poti4 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110) Poti4++; else if(Poti4 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110 && Poti4) Poti4--; |
||
430 | if(Poti1 < 0) Poti1 = 0; else if(Poti1 > 255) Poti1 = 255; |
||
431 | if(Poti2 < 0) Poti2 = 0; else if(Poti2 > 255) Poti2 = 255; |
||
432 | if(Poti3 < 0) Poti3 = 0; else if(Poti3 > 255) Poti3 = 255; |
||
433 | if(Poti4 < 0) Poti4 = 0; else if(Poti4 > 255) Poti4 = 255; |
||
434 | } |
||
435 | |||
436 | //############################################################################ |
||
437 | // Messwerte beim Ermitteln der Nullage |
||
438 | void CalibrierMittelwert(void) |
||
439 | //############################################################################ |
||
1051 | killagreg | 440 | { |
1021 | hbuss | 441 | if(PlatinenVersion == 13) SucheGyroOffset(); |
1 | ingob | 442 | // ADC auschalten, damit die Werte sich nicht während der Berechnung ändern |
443 | ANALOG_OFF; |
||
395 | hbuss | 444 | MesswertNick = AdWertNick; |
445 | MesswertRoll = AdWertRoll; |
||
446 | MesswertGier = AdWertGier; |
||
447 | Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
||
448 | Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
||
449 | Mittelwert_AccHoch = (long)AdWertAccHoch; |
||
450 | // ADC einschalten |
||
1051 | killagreg | 451 | ANALOG_ON; |
1 | ingob | 452 | if(Poti1 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110) Poti1++; else if(Poti1 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110 && Poti1) Poti1--; |
453 | if(Poti2 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110) Poti2++; else if(Poti2 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110 && Poti2) Poti2--; |
||
454 | if(Poti3 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110) Poti3++; else if(Poti3 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110 && Poti3) Poti3--; |
||
455 | if(Poti4 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110) Poti4++; else if(Poti4 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110 && Poti4) Poti4--; |
||
456 | if(Poti1 < 0) Poti1 = 0; else if(Poti1 > 255) Poti1 = 255; |
||
457 | if(Poti2 < 0) Poti2 = 0; else if(Poti2 > 255) Poti2 = 255; |
||
458 | if(Poti3 < 0) Poti3 = 0; else if(Poti3 > 255) Poti3 = 255; |
||
459 | if(Poti4 < 0) Poti4 = 0; else if(Poti4 > 255) Poti4 = 255; |
||
395 | hbuss | 460 | |
461 | Umschlag180Nick = (long) EE_Parameter.WinkelUmschlagNick * 2500L; |
||
720 | ingob | 462 | Umschlag180Roll = (long) EE_Parameter.WinkelUmschlagRoll * 2500L; |
1 | ingob | 463 | } |
464 | |||
465 | //############################################################################ |
||
466 | // Senden der Motorwerte per I2C-Bus |
||
467 | void SendMotorData(void) |
||
468 | //############################################################################ |
||
1051 | killagreg | 469 | { |
1209 | hbuss | 470 | unsigned char i; |
921 | hbuss | 471 | if(!MotorenEin) |
1 | ingob | 472 | { |
1212 | hbuss | 473 | MikroKopterFlags &= ~(FLAG_MOTOR_RUN | FLAG_FLY); |
1216 | killagreg | 474 | for(i=0;i<MAX_MOTORS;i++) |
475 | { |
||
476 | if(!PC_MotortestActive) MotorTest[i] = 0; |
||
1212 | hbuss | 477 | Motor[i] = MotorTest[i]; |
1216 | killagreg | 478 | } |
1212 | hbuss | 479 | if(PC_MotortestActive) PC_MotortestActive--; |
1216 | killagreg | 480 | } |
1212 | hbuss | 481 | else MikroKopterFlags |= FLAG_MOTOR_RUN; |
1111 | hbuss | 482 | |
1212 | hbuss | 483 | DebugOut.Analog[12] = Motor[0]; |
484 | DebugOut.Analog[13] = Motor[1]; |
||
485 | DebugOut.Analog[14] = Motor[3]; |
||
486 | DebugOut.Analog[15] = Motor[2]; |
||
1 | ingob | 487 | |
488 | //Start I2C Interrupt Mode |
||
489 | twi_state = 0; |
||
490 | motor = 0; |
||
1051 | killagreg | 491 | i2c_start(); |
1 | ingob | 492 | } |
493 | |||
494 | |||
495 | |||
496 | //############################################################################ |
||
497 | // Trägt ggf. das Poti als Parameter ein |
||
1051 | killagreg | 498 | void ParameterZuordnung(void) |
1 | ingob | 499 | //############################################################################ |
500 | { |
||
921 | hbuss | 501 | #define CHK_POTI_MM(b,a,min,max) { if(a > 250) { if(a == 251) b = Poti1; else if(a == 252) b = Poti2; else if(a == 253) b = Poti3; else if(a == 254) b = Poti4;} else b = a; if(b <= min) b = min; else if(b >= max) b = max;} |
502 | #define CHK_POTI(b,a,min,max) { if(a > 250) { if(a == 251) b = Poti1; else if(a == 252) b = Poti2; else if(a == 253) b = Poti3; else if(a == 254) b = Poti4;} else b = a; } |
||
1 | ingob | 503 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe,0,255); |
921 | hbuss | 504 | CHK_POTI_MM(Parameter_Luftdruck_D,EE_Parameter.Luftdruck_D,0,100); |
505 | CHK_POTI_MM(Parameter_Hoehe_P,EE_Parameter.Hoehe_P,0,100); |
||
1 | ingob | 506 | CHK_POTI(Parameter_Hoehe_ACC_Wirkung,EE_Parameter.Hoehe_ACC_Wirkung,0,255); |
1283 | hbuss | 507 | CHK_POTI(Parameter_Hoehe_GPS_Z,EE_Parameter.Hoehe_GPS_Z,0,255); |
1 | ingob | 508 | CHK_POTI(Parameter_KompassWirkung,EE_Parameter.KompassWirkung,0,255); |
921 | hbuss | 509 | CHK_POTI_MM(Parameter_Gyro_P,EE_Parameter.Gyro_P,10,255); |
1 | ingob | 510 | CHK_POTI(Parameter_Gyro_I,EE_Parameter.Gyro_I,0,255); |
1120 | hbuss | 511 | CHK_POTI(Parameter_Gyro_D,EE_Parameter.Gyro_D,0,255); |
1322 | hbuss | 512 | CHK_POTI(Parameter_Gyro_Gier_P,EE_Parameter.Gyro_Gier_P,10,255); |
513 | CHK_POTI(Parameter_Gyro_Gier_I,EE_Parameter.Gyro_Gier_I,0,255); |
||
1051 | killagreg | 514 | CHK_POTI(Parameter_I_Faktor,EE_Parameter.I_Faktor,0,255); |
515 | CHK_POTI(Parameter_UserParam1,EE_Parameter.UserParam1,0,255); |
||
516 | CHK_POTI(Parameter_UserParam2,EE_Parameter.UserParam2,0,255); |
||
517 | CHK_POTI(Parameter_UserParam3,EE_Parameter.UserParam3,0,255); |
||
518 | CHK_POTI(Parameter_UserParam4,EE_Parameter.UserParam4,0,255); |
||
519 | CHK_POTI(Parameter_UserParam5,EE_Parameter.UserParam5,0,255); |
||
520 | CHK_POTI(Parameter_UserParam6,EE_Parameter.UserParam6,0,255); |
||
521 | CHK_POTI(Parameter_UserParam7,EE_Parameter.UserParam7,0,255); |
||
522 | CHK_POTI(Parameter_UserParam8,EE_Parameter.UserParam8,0,255); |
||
1 | ingob | 523 | CHK_POTI(Parameter_ServoNickControl,EE_Parameter.ServoNickControl,0,255); |
1232 | hbuss | 524 | CHK_POTI(Parameter_ServoRollControl,EE_Parameter.ServoRollControl,0,255); |
173 | holgerb | 525 | CHK_POTI(Parameter_LoopGasLimit,EE_Parameter.LoopGasLimit,0,255); |
395 | hbuss | 526 | CHK_POTI(Parameter_AchsKopplung1, EE_Parameter.AchsKopplung1,0,255); |
1120 | hbuss | 527 | CHK_POTI(Parameter_AchsKopplung2, EE_Parameter.AchsKopplung2,0,255); |
528 | CHK_POTI(Parameter_CouplingYawCorrection,EE_Parameter.CouplingYawCorrection,0,255); |
||
529 | // CHK_POTI(Parameter_AchsGegenKopplung1,EE_Parameter.AchsGegenKopplung1,0,255); |
||
499 | hbuss | 530 | CHK_POTI(Parameter_DynamicStability,EE_Parameter.DynamicStability,0,255); |
921 | hbuss | 531 | CHK_POTI_MM(Parameter_J16Timing,EE_Parameter.J16Timing,1,255); |
532 | CHK_POTI_MM(Parameter_J17Timing,EE_Parameter.J17Timing,1,255); |
||
533 | CHK_POTI(Parameter_ExternalControl,EE_Parameter.ExternalControl,0,255); |
||
1153 | hbuss | 534 | Ki = 10300 / (Parameter_I_Faktor + 1); |
1 | ingob | 535 | MAX_GAS = EE_Parameter.Gas_Max; |
536 | MIN_GAS = EE_Parameter.Gas_Min; |
||
537 | } |
||
538 | |||
539 | |||
540 | //############################################################################ |
||
541 | // |
||
542 | void MotorRegler(void) |
||
543 | //############################################################################ |
||
544 | { |
||
1309 | hbuss | 545 | int pd_ergebnis_nick,pd_ergebnis_roll,tmp_int; |
1 | ingob | 546 | int GierMischanteil,GasMischanteil; |
547 | static long SummeNick=0,SummeRoll=0; |
||
548 | static long sollGier = 0,tmp_long,tmp_long2; |
||
395 | hbuss | 549 | static long IntegralFehlerNick = 0; |
550 | static long IntegralFehlerRoll = 0; |
||
1 | ingob | 551 | static unsigned int RcLostTimer; |
552 | static unsigned char delay_neutral = 0; |
||
553 | static unsigned char delay_einschalten = 0,delay_ausschalten = 0; |
||
554 | static char TimerWerteausgabe = 0; |
||
555 | static char NeueKompassRichtungMerken = 0; |
||
395 | hbuss | 556 | static long ausgleichNick, ausgleichRoll; |
1153 | hbuss | 557 | int IntegralNickMalFaktor,IntegralRollMalFaktor; |
1209 | hbuss | 558 | unsigned char i; |
1328 | hbuss | 559 | if(--LoadHandler == 0) LoadHandler = 5; // verteilt die Prozessorlast |
1051 | killagreg | 560 | Mittelwert(); |
1 | ingob | 561 | GRN_ON; |
1051 | killagreg | 562 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 563 | // Gaswert ermitteln |
1051 | killagreg | 564 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
565 | GasMischanteil = StickGas; |
||
831 | hbuss | 566 | if(GasMischanteil < MIN_GAS + 10) GasMischanteil = MIN_GAS + 10; |
1316 | hbuss | 567 | |
1051 | killagreg | 568 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
693 | hbuss | 569 | // Empfang schlecht |
1051 | killagreg | 570 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 571 | if(SenderOkay < 100) |
572 | { |
||
1051 | killagreg | 573 | if(RcLostTimer) RcLostTimer--; |
574 | else |
||
1 | ingob | 575 | { |
576 | MotorenEin = 0; |
||
1254 | killagreg | 577 | MikroKopterFlags &= ~FLAG_NOTLANDUNG; |
1051 | killagreg | 578 | } |
1 | ingob | 579 | ROT_ON; |
693 | hbuss | 580 | if(modell_fliegt > 1000) // wahrscheinlich in der Luft --> langsam absenken |
1 | ingob | 581 | { |
582 | GasMischanteil = EE_Parameter.NotGas; |
||
1254 | killagreg | 583 | MikroKopterFlags |= FLAG_NOTLANDUNG; |
744 | hbuss | 584 | PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
1051 | killagreg | 585 | PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
1 | ingob | 586 | PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
587 | PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
||
588 | PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] = 0; |
||
173 | holgerb | 589 | } |
1 | ingob | 590 | else MotorenEin = 0; |
591 | } |
||
1051 | killagreg | 592 | else |
593 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1 | ingob | 594 | // Emfang gut |
1051 | killagreg | 595 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 596 | if(SenderOkay > 140) |
597 | { |
||
1254 | killagreg | 598 | MikroKopterFlags &= ~FLAG_NOTLANDUNG; |
1 | ingob | 599 | RcLostTimer = EE_Parameter.NotGasZeit * 50; |
921 | hbuss | 600 | if(GasMischanteil > 40 && MotorenEin) |
1 | ingob | 601 | { |
602 | if(modell_fliegt < 0xffff) modell_fliegt++; |
||
603 | } |
||
871 | hbuss | 604 | if((modell_fliegt < 256)) |
1 | ingob | 605 | { |
606 | SummeNick = 0; |
||
607 | SummeRoll = 0; |
||
1051 | killagreg | 608 | if(modell_fliegt == 250) |
918 | hbuss | 609 | { |
1051 | killagreg | 610 | NeueKompassRichtungMerken = 1; |
918 | hbuss | 611 | sollGier = 0; |
1051 | killagreg | 612 | Mess_Integral_Gier = 0; |
927 | hbuss | 613 | // Mess_Integral_Gier2 = 0; |
1051 | killagreg | 614 | } |
921 | hbuss | 615 | } else MikroKopterFlags |= FLAG_FLY; |
1051 | killagreg | 616 | |
595 | hbuss | 617 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] > 80) && MotorenEin == 0) |
1 | ingob | 618 | { |
1051 | killagreg | 619 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 620 | // auf Nullwerte kalibrieren |
1051 | killagreg | 621 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 622 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) // Neutralwerte |
623 | { |
||
624 | if(++delay_neutral > 200) // nicht sofort |
||
625 | { |
||
626 | GRN_OFF; |
||
627 | MotorenEin = 0; |
||
628 | delay_neutral = 0; |
||
629 | modell_fliegt = 0; |
||
630 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) > 70) |
||
631 | { |
||
304 | ingob | 632 | unsigned char setting=1; |
1 | ingob | 633 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 1; |
634 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 2; |
||
635 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 3; |
||
636 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 4; |
||
637 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 5; |
||
1063 | killagreg | 638 | SetActiveParamSetNumber(setting); // aktiven Datensatz merken |
1 | ingob | 639 | } |
820 | hbuss | 640 | // else |
1051 | killagreg | 641 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 30 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -70) |
642 | { |
||
819 | hbuss | 643 | WinkelOut.CalcState = 1; |
644 | beeptime = 1000; |
||
645 | } |
||
646 | else |
||
1 | ingob | 647 | { |
819 | hbuss | 648 | ReadParameterSet(GetActiveParamSetNumber(), (unsigned char *) &EE_Parameter.Kanalbelegung[0], STRUCT_PARAM_LAENGE); |
649 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
||
650 | { |
||
1 | ingob | 651 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
1051 | killagreg | 652 | } |
1320 | hbuss | 653 | ServoActive = 0; |
819 | hbuss | 654 | SetNeutral(); |
1232 | hbuss | 655 | ServoActive = 1; |
656 | DDRD |=0x80; // enable J7 -> Servo signal |
||
657 | Piep(GetActiveParamSetNumber(),120); |
||
819 | hbuss | 658 | } |
1051 | killagreg | 659 | } |
1 | ingob | 660 | } |
1051 | killagreg | 661 | else |
513 | hbuss | 662 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) // ACC Neutralwerte speichern |
663 | { |
||
664 | if(++delay_neutral > 200) // nicht sofort |
||
665 | { |
||
666 | GRN_OFF; |
||
667 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_NICK],0xff); // Werte löschen |
||
668 | MotorenEin = 0; |
||
669 | delay_neutral = 0; |
||
670 | modell_fliegt = 0; |
||
671 | SetNeutral(); |
||
672 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_NICK],NeutralAccX / 256); // ACC-NeutralWerte speichern |
||
673 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_NICK+1],NeutralAccX % 256); // ACC-NeutralWerte speichern |
||
674 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL],NeutralAccY / 256); |
||
675 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL+1],NeutralAccY % 256); |
||
676 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_Z],(int)NeutralAccZ / 256); |
||
677 | eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_Z+1],(int)NeutralAccZ % 256); |
||
1232 | hbuss | 678 | Piep(GetActiveParamSetNumber(),120); |
1051 | killagreg | 679 | } |
513 | hbuss | 680 | } |
1 | ingob | 681 | else delay_neutral = 0; |
682 | } |
||
1051 | killagreg | 683 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 684 | // Gas ist unten |
1051 | killagreg | 685 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
595 | hbuss | 686 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] < 35-120) |
1 | ingob | 687 | { |
688 | // Starten |
||
689 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) |
||
690 | { |
||
1051 | killagreg | 691 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 692 | // Einschalten |
1051 | killagreg | 693 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 694 | if(++delay_einschalten > 200) |
695 | { |
||
696 | delay_einschalten = 200; |
||
697 | modell_fliegt = 1; |
||
698 | MotorenEin = 1; |
||
699 | sollGier = 0; |
||
1051 | killagreg | 700 | Mess_Integral_Gier = 0; |
1 | ingob | 701 | Mess_Integral_Gier2 = 0; |
1173 | hbuss | 702 | Mess_IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
703 | Mess_IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
||
1 | ingob | 704 | Mess_IntegralNick2 = IntegralNick; |
705 | Mess_IntegralRoll2 = IntegralRoll; |
||
706 | SummeNick = 0; |
||
707 | SummeRoll = 0; |
||
921 | hbuss | 708 | MikroKopterFlags |= FLAG_START; |
1051 | killagreg | 709 | } |
710 | } |
||
1 | ingob | 711 | else delay_einschalten = 0; |
712 | //Auf Neutralwerte setzen |
||
1051 | killagreg | 713 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 714 | // Auschalten |
1051 | killagreg | 715 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 716 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) |
717 | { |
||
718 | if(++delay_ausschalten > 200) // nicht sofort |
||
719 | { |
||
1298 | hbuss | 720 | MotorenEin = 0; |
721 | delay_ausschalten = 200; |
||
722 | modell_fliegt = 0; |
||
1051 | killagreg | 723 | } |
1 | ingob | 724 | } |
725 | else delay_ausschalten = 0; |
||
726 | } |
||
727 | } |
||
1051 | killagreg | 728 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 729 | // neue Werte von der Funke |
1051 | killagreg | 730 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1216 | killagreg | 731 | |
1254 | killagreg | 732 | if(!NewPpmData-- || (MikroKopterFlags & FLAG_NOTLANDUNG)) |
1 | ingob | 733 | { |
604 | hbuss | 734 | static int stick_nick,stick_roll; |
1 | ingob | 735 | ParameterZuordnung(); |
1051 | killagreg | 736 | stick_nick = (stick_nick * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_P) / 4; |
723 | hbuss | 737 | stick_nick += PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_D; |
805 | hbuss | 738 | StickNick = stick_nick - (GPS_Nick + GPS_Nick2); |
604 | hbuss | 739 | |
723 | hbuss | 740 | stick_roll = (stick_roll * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_P) / 4; |
741 | stick_roll += PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_D; |
||
805 | hbuss | 742 | StickRoll = stick_roll - (GPS_Roll + GPS_Roll2); |
723 | hbuss | 743 | |
1 | ingob | 744 | StickGier = -PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]; |
1120 | hbuss | 745 | if(StickGier > 2) StickGier -= 2; else |
746 | if(StickGier < -2) StickGier += 2; else StickGier = 0; |
||
747 | |||
1316 | hbuss | 748 | StickGas = (StickGas + PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] + 120) / 2; |
749 | |||
1153 | hbuss | 750 | GyroFaktor = (Parameter_Gyro_P + 10.0); |
751 | IntegralFaktor = Parameter_Gyro_I; |
||
1322 | hbuss | 752 | GyroFaktorGier = (Parameter_Gyro_Gier_P + 10.0); |
753 | IntegralFaktorGier = Parameter_Gyro_Gier_I; |
||
1 | ingob | 754 | |
595 | hbuss | 755 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
756 | //+ Analoge Steuerung per Seriell |
||
757 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
921 | hbuss | 758 | if(ExternControl.Config & 0x01 && Parameter_ExternalControl > 128) |
595 | hbuss | 759 | { |
760 | StickNick += (int) ExternControl.Nick * (int) EE_Parameter.Stick_P; |
||
761 | StickRoll += (int) ExternControl.Roll * (int) EE_Parameter.Stick_P; |
||
762 | StickGier += ExternControl.Gier; |
||
763 | ExternHoehenValue = (int) ExternControl.Hight * (int)EE_Parameter.Hoehe_Verstaerkung; |
||
764 | if(ExternControl.Gas < StickGas) StickGas = ExternControl.Gas; |
||
765 | } |
||
855 | hbuss | 766 | if(StickGas < 0) StickGas = 0; |
1316 | hbuss | 767 | |
1 | ingob | 768 | if(EE_Parameter.GlobalConfig & CFG_HEADING_HOLD) IntegralFaktor = 0; |
769 | if(GyroFaktor < 0) GyroFaktor = 0; |
||
770 | if(IntegralFaktor < 0) IntegralFaktor = 0; |
||
723 | hbuss | 771 | |
1051 | killagreg | 772 | if(abs(StickNick/STICK_GAIN) > MaxStickNick) |
928 | hbuss | 773 | { |
1051 | killagreg | 774 | MaxStickNick = abs(StickNick)/STICK_GAIN; |
928 | hbuss | 775 | if(MaxStickNick > 100) MaxStickNick = 100; |
1051 | killagreg | 776 | } |
928 | hbuss | 777 | else MaxStickNick--; |
1051 | killagreg | 778 | if(abs(StickRoll/STICK_GAIN) > MaxStickRoll) |
928 | hbuss | 779 | { |
1051 | killagreg | 780 | MaxStickRoll = abs(StickRoll)/STICK_GAIN; |
928 | hbuss | 781 | if(MaxStickRoll > 100) MaxStickRoll = 100; |
1051 | killagreg | 782 | } |
928 | hbuss | 783 | else MaxStickRoll--; |
1254 | killagreg | 784 | if(MikroKopterFlags & FLAG_NOTLANDUNG) {MaxStickNick = 0; MaxStickRoll = 0;} |
723 | hbuss | 785 | |
1051 | killagreg | 786 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
173 | holgerb | 787 | // Looping? |
1051 | killagreg | 788 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
993 | hbuss | 789 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_LINKS) Looping_Links = 1; |
1051 | killagreg | 790 | else |
791 | { |
||
395 | hbuss | 792 | { |
1051 | killagreg | 793 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Links = 0; |
794 | } |
||
795 | } |
||
993 | hbuss | 796 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_RECHTS) Looping_Rechts = 1; |
1051 | killagreg | 797 | else |
395 | hbuss | 798 | { |
799 | if(Looping_Rechts) // Hysterese |
||
800 | { |
||
801 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Rechts = 0; |
||
802 | } |
||
1051 | killagreg | 803 | } |
173 | holgerb | 804 | |
993 | hbuss | 805 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_OBEN) Looping_Oben = 1; |
1051 | killagreg | 806 | else |
807 | { |
||
395 | hbuss | 808 | if(Looping_Oben) // Hysterese |
809 | { |
||
1051 | killagreg | 810 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Oben = 0; |
811 | } |
||
812 | } |
||
993 | hbuss | 813 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_UNTEN) Looping_Unten = 1; |
1051 | killagreg | 814 | else |
395 | hbuss | 815 | { |
816 | if(Looping_Unten) // Hysterese |
||
817 | { |
||
818 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Unten = 0; |
||
819 | } |
||
1051 | killagreg | 820 | } |
395 | hbuss | 821 | |
822 | if(Looping_Links || Looping_Rechts) Looping_Roll = 1; else Looping_Roll = 0; |
||
1153 | hbuss | 823 | if(Looping_Oben || Looping_Unten) { Looping_Nick = 1; Looping_Roll = 0; Looping_Links = 0; Looping_Rechts = 0;} else Looping_Nick = 0; |
395 | hbuss | 824 | } // Ende neue Funken-Werte |
825 | |||
826 | if(Looping_Roll || Looping_Nick) |
||
827 | { |
||
173 | holgerb | 828 | if(GasMischanteil > EE_Parameter.LoopGasLimit) GasMischanteil = EE_Parameter.LoopGasLimit; |
1153 | hbuss | 829 | TrichterFlug = 1; |
173 | holgerb | 830 | } |
831 | |||
1051 | killagreg | 832 | |
833 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
834 | // Bei Empfangsausfall im Flug |
||
835 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1254 | killagreg | 836 | if(MikroKopterFlags & FLAG_NOTLANDUNG) |
1 | ingob | 837 | { |
838 | StickGier = 0; |
||
839 | StickNick = 0; |
||
840 | StickRoll = 0; |
||
1211 | hbuss | 841 | GyroFaktor = 90; |
842 | IntegralFaktor = 120; |
||
843 | GyroFaktorGier = 90; |
||
844 | IntegralFaktorGier = 120; |
||
173 | holgerb | 845 | Looping_Roll = 0; |
846 | Looping_Nick = 0; |
||
1051 | killagreg | 847 | } |
395 | hbuss | 848 | |
849 | |||
1051 | killagreg | 850 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 851 | // Integrale auf ACC-Signal abgleichen |
1051 | killagreg | 852 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
395 | hbuss | 853 | #define ABGLEICH_ANZAHL 256L |
854 | |||
855 | MittelIntegralNick += IntegralNick; // Für die Mittelwertbildung aufsummieren |
||
856 | MittelIntegralRoll += IntegralRoll; |
||
857 | MittelIntegralNick2 += IntegralNick2; |
||
858 | MittelIntegralRoll2 += IntegralRoll2; |
||
859 | |||
860 | if(Looping_Nick || Looping_Roll) |
||
861 | { |
||
862 | IntegralAccNick = 0; |
||
863 | IntegralAccRoll = 0; |
||
864 | MittelIntegralNick = 0; |
||
865 | MittelIntegralRoll = 0; |
||
866 | MittelIntegralNick2 = 0; |
||
867 | MittelIntegralRoll2 = 0; |
||
868 | Mess_IntegralNick2 = Mess_IntegralNick; |
||
869 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
||
870 | ZaehlMessungen = 0; |
||
498 | hbuss | 871 | LageKorrekturNick = 0; |
872 | LageKorrekturRoll = 0; |
||
395 | hbuss | 873 | } |
874 | |||
1051 | killagreg | 875 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1224 | hbuss | 876 | if(!Looping_Nick && !Looping_Roll && (Aktuell_az > 512 || MotorenEin)) |
469 | hbuss | 877 | { |
878 | long tmp_long, tmp_long2; |
||
1171 | hbuss | 879 | if(FromNaviCtrl_Value.Kalman_K != -1 /*&& !TrichterFlug*/) |
992 | hbuss | 880 | { |
881 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
||
1051 | killagreg | 882 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
883 | tmp_long = (tmp_long * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
||
884 | tmp_long2 = (tmp_long2 * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
||
992 | hbuss | 885 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
886 | { |
||
887 | tmp_long /= 2; |
||
888 | tmp_long2 /= 2; |
||
889 | } |
||
890 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
||
891 | { |
||
892 | tmp_long /= 3; |
||
893 | tmp_long2 /= 3; |
||
894 | } |
||
895 | if(tmp_long > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
||
896 | if(tmp_long < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
||
897 | if(tmp_long2 > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
||
898 | if(tmp_long2 < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
||
899 | } |
||
1051 | killagreg | 900 | else |
992 | hbuss | 901 | { |
902 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
||
1051 | killagreg | 903 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
992 | hbuss | 904 | tmp_long /= 16; |
905 | tmp_long2 /= 16; |
||
906 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
||
907 | { |
||
908 | tmp_long /= 3; |
||
909 | tmp_long2 /= 3; |
||
1216 | killagreg | 910 | } |
911 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
||
992 | hbuss | 912 | { |
913 | tmp_long /= 3; |
||
914 | tmp_long2 /= 3; |
||
915 | } |
||
1155 | hbuss | 916 | |
917 | #define AUSGLEICH 32 |
||
992 | hbuss | 918 | if(tmp_long > AUSGLEICH) tmp_long = AUSGLEICH; |
919 | if(tmp_long < -AUSGLEICH) tmp_long =-AUSGLEICH; |
||
920 | if(tmp_long2 > AUSGLEICH) tmp_long2 = AUSGLEICH; |
||
921 | if(tmp_long2 <-AUSGLEICH) tmp_long2 =-AUSGLEICH; |
||
922 | } |
||
1166 | hbuss | 923 | |
924 | //if(Poti2 > 20) { tmp_long = 0; tmp_long2 = 0;} |
||
1111 | hbuss | 925 | Mess_IntegralNick -= tmp_long; |
926 | Mess_IntegralRoll -= tmp_long2; |
||
469 | hbuss | 927 | } |
1051 | killagreg | 928 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
395 | hbuss | 929 | if(ZaehlMessungen >= ABGLEICH_ANZAHL) |
930 | { |
||
931 | static int cnt = 0; |
||
932 | static char last_n_p,last_n_n,last_r_p,last_r_n; |
||
933 | static long MittelIntegralNick_Alt,MittelIntegralRoll_Alt; |
||
1173 | hbuss | 934 | if(!Looping_Nick && !Looping_Roll && !TrichterFlug && EE_Parameter.Driftkomp) |
173 | holgerb | 935 | { |
395 | hbuss | 936 | MittelIntegralNick /= ABGLEICH_ANZAHL; |
937 | MittelIntegralRoll /= ABGLEICH_ANZAHL; |
||
938 | IntegralAccNick = (EE_Parameter.GyroAccFaktor * IntegralAccNick) / ABGLEICH_ANZAHL; |
||
939 | IntegralAccRoll = (EE_Parameter.GyroAccFaktor * IntegralAccRoll) / ABGLEICH_ANZAHL; |
||
940 | IntegralAccZ = IntegralAccZ / ABGLEICH_ANZAHL; |
||
492 | hbuss | 941 | #define MAX_I 0//(Poti2/10) |
395 | hbuss | 942 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
943 | IntegralFehlerNick = (long)(MittelIntegralNick - (long)IntegralAccNick); |
||
944 | ausgleichNick = IntegralFehlerNick / EE_Parameter.GyroAccAbgleich; |
||
1051 | killagreg | 945 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
946 | IntegralFehlerRoll = (long)(MittelIntegralRoll - (long)IntegralAccRoll); |
||
395 | hbuss | 947 | ausgleichRoll = IntegralFehlerRoll / EE_Parameter.GyroAccAbgleich; |
614 | hbuss | 948 | |
949 | LageKorrekturNick = ausgleichNick / ABGLEICH_ANZAHL; |
||
498 | hbuss | 950 | LageKorrekturRoll = ausgleichRoll / ABGLEICH_ANZAHL; |
395 | hbuss | 951 | |
992 | hbuss | 952 | if(((MaxStickNick > 64) || (MaxStickRoll > 64) || (abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25)) && (FromNaviCtrl_Value.Kalman_K == -1)) |
614 | hbuss | 953 | { |
954 | LageKorrekturNick /= 2; |
||
720 | ingob | 955 | LageKorrekturRoll /= 2; |
614 | hbuss | 956 | } |
498 | hbuss | 957 | |
1051 | killagreg | 958 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
395 | hbuss | 959 | // Gyro-Drift ermitteln |
1051 | killagreg | 960 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
395 | hbuss | 961 | MittelIntegralNick2 /= ABGLEICH_ANZAHL; |
962 | MittelIntegralRoll2 /= ABGLEICH_ANZAHL; |
||
1051 | killagreg | 963 | tmp_long = IntegralNick2 - IntegralNick; |
964 | tmp_long2 = IntegralRoll2 - IntegralRoll; |
||
395 | hbuss | 965 | //DebugOut.Analog[25] = MittelIntegralRoll2 / 26; |
966 | |||
967 | IntegralFehlerNick = tmp_long; |
||
968 | IntegralFehlerRoll = tmp_long2; |
||
969 | Mess_IntegralNick2 -= IntegralFehlerNick; |
||
970 | Mess_IntegralRoll2 -= IntegralFehlerRoll; |
||
971 | |||
1111 | hbuss | 972 | if(EE_Parameter.Driftkomp) |
973 | { |
||
927 | hbuss | 974 | if(GierGyroFehler > ABGLEICH_ANZAHL/2) { AdNeutralGier++; AdNeutralGierBias++; } |
975 | if(GierGyroFehler <-ABGLEICH_ANZAHL/2) { AdNeutralGier--; AdNeutralGierBias--; } |
||
1111 | hbuss | 976 | } |
693 | hbuss | 977 | GierGyroFehler = 0; |
720 | ingob | 978 | |
979 | |||
1243 | killagreg | 980 | #define FEHLER_LIMIT (ABGLEICH_ANZAHL / 2) |
981 | #define FEHLER_LIMIT1 (ABGLEICH_ANZAHL * 2) //4 |
||
1225 | hbuss | 982 | #define FEHLER_LIMIT2 (ABGLEICH_ANZAHL * 16) //16 |
492 | hbuss | 983 | #define BEWEGUNGS_LIMIT 20000 |
395 | hbuss | 984 | // Nick +++++++++++++++++++++++++++++++++++++++++++++++++ |
985 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
||
1225 | hbuss | 986 | if(labs(IntegralFehlerNick) > FEHLER_LIMIT1) cnt = 4; |
1173 | hbuss | 987 | if(labs(MittelIntegralNick_Alt - MittelIntegralNick) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
492 | hbuss | 988 | { |
1051 | killagreg | 989 | if(IntegralFehlerNick > FEHLER_LIMIT2) |
395 | hbuss | 990 | { |
1051 | killagreg | 991 | if(last_n_p) |
395 | hbuss | 992 | { |
1173 | hbuss | 993 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
492 | hbuss | 994 | ausgleichNick = IntegralFehlerNick / 8; |
401 | hbuss | 995 | if(ausgleichNick > 5000) ausgleichNick = 5000; |
498 | hbuss | 996 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1051 | killagreg | 997 | } |
395 | hbuss | 998 | else last_n_p = 1; |
999 | } else last_n_p = 0; |
||
1051 | killagreg | 1000 | if(IntegralFehlerNick < -FEHLER_LIMIT2) |
395 | hbuss | 1001 | { |
1002 | if(last_n_n) |
||
1051 | killagreg | 1003 | { |
1173 | hbuss | 1004 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
492 | hbuss | 1005 | ausgleichNick = IntegralFehlerNick / 8; |
401 | hbuss | 1006 | if(ausgleichNick < -5000) ausgleichNick = -5000; |
498 | hbuss | 1007 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
1051 | killagreg | 1008 | } |
395 | hbuss | 1009 | else last_n_n = 1; |
1010 | } else last_n_n = 0; |
||
1051 | killagreg | 1011 | } |
1012 | else |
||
847 | hbuss | 1013 | { |
1014 | cnt = 0; |
||
921 | hbuss | 1015 | KompassSignalSchlecht = 1000; |
1051 | killagreg | 1016 | } |
499 | hbuss | 1017 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1173 | hbuss | 1018 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
395 | hbuss | 1019 | if(IntegralFehlerNick > FEHLER_LIMIT) AdNeutralNick += cnt; |
1020 | if(IntegralFehlerNick < -FEHLER_LIMIT) AdNeutralNick -= cnt; |
||
401 | hbuss | 1021 | |
395 | hbuss | 1022 | // Roll +++++++++++++++++++++++++++++++++++++++++++++++++ |
492 | hbuss | 1023 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
1225 | hbuss | 1024 | if(labs(IntegralFehlerRoll) > FEHLER_LIMIT1) cnt = 4; |
498 | hbuss | 1025 | ausgleichRoll = 0; |
1173 | hbuss | 1026 | if(labs(MittelIntegralRoll_Alt - MittelIntegralRoll) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
492 | hbuss | 1027 | { |
1051 | killagreg | 1028 | if(IntegralFehlerRoll > FEHLER_LIMIT2) |
395 | hbuss | 1029 | { |
1051 | killagreg | 1030 | if(last_r_p) |
395 | hbuss | 1031 | { |
1173 | hbuss | 1032 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
492 | hbuss | 1033 | ausgleichRoll = IntegralFehlerRoll / 8; |
401 | hbuss | 1034 | if(ausgleichRoll > 5000) ausgleichRoll = 5000; |
498 | hbuss | 1035 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
1051 | killagreg | 1036 | } |
395 | hbuss | 1037 | else last_r_p = 1; |
1038 | } else last_r_p = 0; |
||
1051 | killagreg | 1039 | if(IntegralFehlerRoll < -FEHLER_LIMIT2) |
395 | hbuss | 1040 | { |
1051 | killagreg | 1041 | if(last_r_n) |
395 | hbuss | 1042 | { |
1173 | hbuss | 1043 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
492 | hbuss | 1044 | ausgleichRoll = IntegralFehlerRoll / 8; |
401 | hbuss | 1045 | if(ausgleichRoll < -5000) ausgleichRoll = -5000; |
498 | hbuss | 1046 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
395 | hbuss | 1047 | } |
1048 | else last_r_n = 1; |
||
1049 | } else last_r_n = 0; |
||
1051 | killagreg | 1050 | } else |
492 | hbuss | 1051 | { |
1052 | cnt = 0; |
||
921 | hbuss | 1053 | KompassSignalSchlecht = 1000; |
1051 | killagreg | 1054 | } |
499 | hbuss | 1055 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
1173 | hbuss | 1056 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
395 | hbuss | 1057 | if(IntegralFehlerRoll > FEHLER_LIMIT) AdNeutralRoll += cnt; |
1058 | if(IntegralFehlerRoll < -FEHLER_LIMIT) AdNeutralRoll -= cnt; |
||
173 | holgerb | 1059 | } |
1051 | killagreg | 1060 | else |
498 | hbuss | 1061 | { |
1062 | LageKorrekturRoll = 0; |
||
1063 | LageKorrekturNick = 0; |
||
880 | hbuss | 1064 | TrichterFlug = 0; |
498 | hbuss | 1065 | } |
1051 | killagreg | 1066 | |
498 | hbuss | 1067 | if(!IntegralFaktor) { LageKorrekturRoll = 0; LageKorrekturNick = 0;} // z.B. bei HH |
1051 | killagreg | 1068 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1069 | MittelIntegralNick_Alt = MittelIntegralNick; |
||
1070 | MittelIntegralRoll_Alt = MittelIntegralRoll; |
||
1071 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
395 | hbuss | 1072 | IntegralAccNick = 0; |
1073 | IntegralAccRoll = 0; |
||
1074 | IntegralAccZ = 0; |
||
1075 | MittelIntegralNick = 0; |
||
1076 | MittelIntegralRoll = 0; |
||
1077 | MittelIntegralNick2 = 0; |
||
1078 | MittelIntegralRoll2 = 0; |
||
1079 | ZaehlMessungen = 0; |
||
1173 | hbuss | 1080 | } // ZaehlMessungen >= ABGLEICH_ANZAHL |
395 | hbuss | 1081 | |
1173 | hbuss | 1082 | |
1051 | killagreg | 1083 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1084 | // Gieren |
1051 | killagreg | 1085 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
693 | hbuss | 1086 | // if(GasMischanteil < 35) { if(StickGier > 10) StickGier = 10; else if(StickGier < -10) StickGier = -10;}; |
1051 | killagreg | 1087 | if(abs(StickGier) > 15) // war 35 |
1 | ingob | 1088 | { |
921 | hbuss | 1089 | KompassSignalSchlecht = 1000; |
1051 | killagreg | 1090 | if(!(EE_Parameter.GlobalConfig & CFG_KOMPASS_FIX)) |
1091 | { |
||
1092 | NeueKompassRichtungMerken = 1; |
||
824 | hbuss | 1093 | }; |
1 | ingob | 1094 | } |
395 | hbuss | 1095 | tmp_int = (long) EE_Parameter.Gier_P * ((long)StickGier * abs(StickGier)) / 512L; // expo y = ax + bx² |
1051 | killagreg | 1096 | tmp_int += (EE_Parameter.Gier_P * StickGier) / 4; |
173 | holgerb | 1097 | sollGier = tmp_int; |
1051 | killagreg | 1098 | Mess_Integral_Gier -= tmp_int; |
395 | hbuss | 1099 | if(Mess_Integral_Gier > 50000) Mess_Integral_Gier = 50000; // begrenzen |
1100 | if(Mess_Integral_Gier <-50000) Mess_Integral_Gier =-50000; |
||
1051 | killagreg | 1101 | |
1102 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1 | ingob | 1103 | // Kompass |
1051 | killagreg | 1104 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1175 | hbuss | 1105 | //DebugOut.Analog[16] = KompassSignalSchlecht; |
819 | hbuss | 1106 | |
1051 | killagreg | 1107 | if(KompassValue && (EE_Parameter.GlobalConfig & CFG_KOMPASS_AKTIV)) |
1 | ingob | 1108 | { |
819 | hbuss | 1109 | int w,v,r,fehler,korrektur; |
1 | ingob | 1110 | w = abs(IntegralNick /512); // mit zunehmender Neigung den Einfluss drosseln |
1111 | v = abs(IntegralRoll /512); |
||
1112 | if(v > w) w = v; // grösste Neigung ermitteln |
||
824 | hbuss | 1113 | korrektur = w / 8 + 1; |
921 | hbuss | 1114 | fehler = ((540 + KompassValue - (ErsatzKompass/GIER_GRAD_FAKTOR)) % 360) - 180; |
1171 | hbuss | 1115 | if(abs(MesswertGier) > 128) |
1036 | hbuss | 1116 | { |
1117 | fehler = 0; |
||
1051 | killagreg | 1118 | } |
921 | hbuss | 1119 | if(!KompassSignalSchlecht && w < 25) |
1120 | { |
||
1121 | GierGyroFehler += fehler; |
||
1051 | killagreg | 1122 | if(NeueKompassRichtungMerken) |
1123 | { |
||
921 | hbuss | 1124 | beeptime = 200; |
847 | hbuss | 1125 | // KompassStartwert = KompassValue; |
1171 | hbuss | 1126 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
921 | hbuss | 1127 | KompassStartwert = (ErsatzKompass/GIER_GRAD_FAKTOR); |
1128 | NeueKompassRichtungMerken = 0; |
||
1129 | } |
||
1 | ingob | 1130 | } |
824 | hbuss | 1131 | ErsatzKompass += (fehler * 8) / korrektur; |
921 | hbuss | 1132 | w = (w * Parameter_KompassWirkung) / 32; // auf die Wirkung normieren |
1 | ingob | 1133 | w = Parameter_KompassWirkung - w; // Wirkung ggf drosseln |
921 | hbuss | 1134 | if(w >= 0) |
1 | ingob | 1135 | { |
1051 | killagreg | 1136 | if(!KompassSignalSchlecht) |
693 | hbuss | 1137 | { |
1051 | killagreg | 1138 | v = 64 + ((MaxStickNick + MaxStickRoll)) / 8; |
847 | hbuss | 1139 | r = ((540 + (ErsatzKompass/GIER_GRAD_FAKTOR) - KompassStartwert) % 360) - 180; |
1140 | // r = KompassRichtung; |
||
819 | hbuss | 1141 | v = (r * w) / v; // nach Kompass ausrichten |
1142 | w = 3 * Parameter_KompassWirkung; |
||
693 | hbuss | 1143 | if(v > w) v = w; // Begrenzen |
1051 | killagreg | 1144 | else |
693 | hbuss | 1145 | if(v < -w) v = -w; |
1146 | Mess_Integral_Gier += v; |
||
1051 | killagreg | 1147 | } |
693 | hbuss | 1148 | if(KompassSignalSchlecht) KompassSignalSchlecht--; |
1051 | killagreg | 1149 | } |
921 | hbuss | 1150 | else KompassSignalSchlecht = 500; // so lange das Signal taub stellen --> ca. 1 sek |
1051 | killagreg | 1151 | } |
1152 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1 | ingob | 1153 | |
1051 | killagreg | 1154 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1155 | // Debugwerte zuordnen |
1051 | killagreg | 1156 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1157 | if(!TimerWerteausgabe--) |
1158 | { |
||
395 | hbuss | 1159 | TimerWerteausgabe = 24; |
805 | hbuss | 1160 | |
1171 | hbuss | 1161 | DebugOut.Analog[0] = IntegralNick / (EE_Parameter.GyroAccFaktor * 4); |
1162 | DebugOut.Analog[1] = IntegralRoll / (EE_Parameter.GyroAccFaktor * 4); |
||
1163 | DebugOut.Analog[2] = Mittelwert_AccNick / 4; |
||
1164 | DebugOut.Analog[3] = Mittelwert_AccRoll / 4; |
||
1 | ingob | 1165 | DebugOut.Analog[4] = MesswertGier; |
1314 | killagreg | 1166 | DebugOut.Analog[5] = HoehenWert/5; |
1224 | hbuss | 1167 | DebugOut.Analog[6] = Aktuell_az;//(Mess_Integral_Hoch / 512);//Aktuell_az; |
1 | ingob | 1168 | DebugOut.Analog[8] = KompassValue; |
297 | holgerb | 1169 | DebugOut.Analog[9] = UBat; |
1283 | hbuss | 1170 | DebugOut.Analog[10] = SenderOkay; |
1051 | killagreg | 1171 | DebugOut.Analog[11] = ErsatzKompass / GIER_GRAD_FAKTOR; |
929 | hbuss | 1172 | //DebugOut.Analog[16] = Mittelwert_AccHoch; |
1083 | killagreg | 1173 | //DebugOut.Analog[17] = FromNaviCtrl_Value.Distance; |
1253 | killagreg | 1174 | DebugOut.Analog[18] = VarioMeter; |
819 | hbuss | 1175 | DebugOut.Analog[19] = WinkelOut.CalcState; |
1328 | hbuss | 1176 | DebugOut.Analog[20] = ServoNickValue; |
1322 | hbuss | 1177 | // DebugOut.Analog[22] = FromNaviCtrl_Value.GpsZ; |
1171 | hbuss | 1178 | // DebugOut.Analog[24] = MesswertNick/2; |
1179 | // DebugOut.Analog[25] = MesswertRoll/2; |
||
1322 | hbuss | 1180 | // DebugOut.Analog[27] = (int)FromNaviCtrl_Value.Kalman_MaxDrift; |
1172 | hbuss | 1181 | // DebugOut.Analog[28] = (int)FromNaviCtrl_Value.Kalman_MaxFusion; |
1182 | // DebugOut.Analog[29] = (int)FromNaviCtrl_Value.Kalman_K; |
||
1322 | hbuss | 1183 | //DebugOut.Analog[28] = I2CError; |
1215 | hbuss | 1184 | DebugOut.Analog[29] = FromNaviCtrl_Value.SerialDataOkay; |
1216 | killagreg | 1185 | DebugOut.Analog[30] = GPS_Nick; |
720 | ingob | 1186 | DebugOut.Analog[31] = GPS_Roll; |
1 | ingob | 1187 | } |
1188 | |||
1051 | killagreg | 1189 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1190 | // Drehgeschwindigkeit und -winkel zu einem Istwert zusammenfassen |
1051 | killagreg | 1191 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1216 | killagreg | 1192 | if(TrichterFlug) { SummeRoll = 0; SummeNick = 0;}; |
604 | hbuss | 1193 | |
1171 | hbuss | 1194 | if(!Looping_Nick) IntegralNickMalFaktor = (IntegralNick * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralNickMalFaktor = 0; |
1195 | if(!Looping_Roll) IntegralRollMalFaktor = (IntegralRoll * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralRollMalFaktor = 0; |
||
1153 | hbuss | 1196 | |
1167 | hbuss | 1197 | #define TRIM_MAX 200 |
1166 | hbuss | 1198 | if(TrimNick > TRIM_MAX) TrimNick = TRIM_MAX; else if(TrimNick <-TRIM_MAX) TrimNick =-TRIM_MAX; |
1199 | if(TrimRoll > TRIM_MAX) TrimRoll = TRIM_MAX; else if(TrimRoll <-TRIM_MAX) TrimRoll =-TRIM_MAX; |
||
1153 | hbuss | 1200 | |
1166 | hbuss | 1201 | MesswertNick = IntegralNickMalFaktor + (long)((long)MesswertNick * GyroFaktor + (long)TrimNick * 128L) / (256L / STICK_GAIN); |
1202 | MesswertRoll = IntegralRollMalFaktor + (long)((long)MesswertRoll * GyroFaktor + (long)TrimRoll * 128L) / (256L / STICK_GAIN); |
||
1211 | hbuss | 1203 | MesswertGier = (long)(MesswertGier * 2 * (long)GyroFaktorGier) / (256L / STICK_GAIN) + (long)(Integral_Gier * IntegralFaktorGier) / (2 * (44000 / STICK_GAIN)); |
1166 | hbuss | 1204 | |
1 | ingob | 1205 | // Maximalwerte abfangen |
1153 | hbuss | 1206 | // #define MAX_SENSOR (4096*STICK_GAIN) |
1207 | #define MAX_SENSOR (4096*4) |
||
1216 | killagreg | 1208 | if(MesswertNick > MAX_SENSOR) MesswertNick = MAX_SENSOR; |
1 | ingob | 1209 | if(MesswertNick < -MAX_SENSOR) MesswertNick = -MAX_SENSOR; |
1210 | if(MesswertRoll > MAX_SENSOR) MesswertRoll = MAX_SENSOR; |
||
1211 | if(MesswertRoll < -MAX_SENSOR) MesswertRoll = -MAX_SENSOR; |
||
1212 | if(MesswertGier > MAX_SENSOR) MesswertGier = MAX_SENSOR; |
||
1213 | if(MesswertGier < -MAX_SENSOR) MesswertGier = -MAX_SENSOR; |
||
1214 | |||
1051 | killagreg | 1215 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1216 | // Höhenregelung |
1217 | // Die Höhenregelung schwächt lediglich das Gas ab, erhöht es allerdings nicht |
||
1051 | killagreg | 1218 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1278 | hbuss | 1219 | if(UBat > BattLowVoltageWarning) GasMischanteil = (GasMischanteil * BattLowVoltageWarning) / UBat; // Gas auf das aktuelle Spannungvieveau beziehen |
855 | hbuss | 1220 | GasMischanteil *= STICK_GAIN; |
1309 | hbuss | 1221 | |
1222 | // if height control is activated |
||
1328 | hbuss | 1223 | J4High; |
1322 | hbuss | 1224 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG) && !(Looping_Roll || Looping_Nick)) // Höhenregelung |
1309 | hbuss | 1225 | { |
1328 | hbuss | 1226 | // #define HOOVER_GAS_AVERAGE 4096L // 4096 * 2ms = 8.2s averaging |
1227 | #define HOOVER_GAS_AVERAGE 1024L // 1024 * 10ms = 10s averaging |
||
1228 | #define HC_GAS_AVERAGE 2 // 2 * 10ms= 20ms averaging |
||
1309 | hbuss | 1229 | #define OPA_OFFSET_STEP 10 |
1230 | int HCGas, HeightDeviation; |
||
1231 | static int HeightTrimming = 0; // rate for change of height setpoint |
||
1232 | static int FilterHCGas = 0; |
||
1328 | hbuss | 1233 | static int StickGasHoover = 120, HooverGas = 0, HooverGasMin = 0, HooverGasMax = 1023, LastHCGas = 0; |
1309 | hbuss | 1234 | static unsigned long HooverGasFilter = 0; |
1322 | hbuss | 1235 | static unsigned char delay = 100, BaroAtUpperLimit = 0, BaroAtLowerLimit = 0; |
1320 | hbuss | 1236 | int CosAttitude; // for projection of hoover gas |
1309 | hbuss | 1237 | long tmp_long3; |
1320 | hbuss | 1238 | // const unsigned char GAS_TAB[31] = {128,128,128,129,129,130,131,132,133,135,136,138,140,142,145,148,151,154,158,162,167,172,178,184,191,199,208,218,229,241,255}; |
1309 | hbuss | 1239 | // get the current hooverpoint |
1328 | hbuss | 1240 | if(LoadHandler == 1) |
1241 | { |
||
1322 | hbuss | 1242 | DebugOut.Analog[21] = HooverGas; |
1309 | hbuss | 1243 | DebugOut.Analog[18] = VarioMeter; |
1244 | |||
1322 | hbuss | 1245 | // Expand the measurement |
1246 | // measurement of air pressure close to upper limit and no overflow in correction of the new OCR0A value occurs |
||
1247 | if(!BaroExpandActive) |
||
1248 | { |
||
1249 | if(MessLuftdruck > 920) |
||
1250 | { // increase offset |
||
1251 | if(OCR0A < (255 - OPA_OFFSET_STEP)) |
||
1252 | { |
||
1253 | ExpandBaro -= 1; |
||
1254 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // increase offset to shift ADC down |
||
1255 | beeptime = 300; |
||
1328 | hbuss | 1256 | BaroExpandActive = 50; |
1322 | hbuss | 1257 | } |
1258 | else |
||
1259 | { |
||
1260 | BaroAtLowerLimit = 1; |
||
1261 | } |
||
1262 | } |
||
1263 | // measurement of air pressure close to lower limit and |
||
1264 | else |
||
1265 | if(MessLuftdruck < 100) |
||
1266 | { // decrease offset |
||
1267 | if(OCR0A > OPA_OFFSET_STEP) |
||
1268 | { |
||
1269 | ExpandBaro += 1; |
||
1270 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // decrease offset to shift ADC up |
||
1271 | beeptime = 300; |
||
1328 | hbuss | 1272 | BaroExpandActive = 50; |
1322 | hbuss | 1273 | } |
1274 | else |
||
1275 | { |
||
1276 | BaroAtUpperLimit = 1; |
||
1277 | } |
||
1278 | } |
||
1279 | else |
||
1280 | { |
||
1281 | BaroAtUpperLimit = 0; |
||
1282 | BaroAtLowerLimit = 0; |
||
1283 | } |
||
1284 | } |
||
1285 | else // delay, because of expanding the Baro-Range |
||
1286 | { |
||
1287 | // now clear the D-values |
||
1288 | SummenHoehe = HoehenWert * SM_FILTER; |
||
1289 | VarioMeter = 0; |
||
1290 | BaroExpandActive--; |
||
1291 | } |
||
1328 | hbuss | 1292 | |
1293 | // if height control is activated by an rc channel |
||
1294 | if(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER) // Regler wird über Schalter gesteuert |
||
1295 | { // check if parameter is less than activation threshold |
||
1296 | if(Parameter_MaxHoehe < 50) // for 3 or 2-state switch height control is disabled in lowest position |
||
1297 | { //height control not active |
||
1298 | if(!delay--) |
||
1299 | { |
||
1300 | HoehenReglerAktiv = 0; // disable height control |
||
1301 | SollHoehe = HoehenWert; // update SetPoint with current reading |
||
1302 | delay = 1; |
||
1303 | } |
||
1304 | } |
||
1305 | else |
||
1306 | { //height control is activated |
||
1307 | HoehenReglerAktiv = 1; // enable height control |
||
1308 | delay = 40; |
||
1309 | } |
||
1051 | killagreg | 1310 | } |
1309 | hbuss | 1311 | else // no switchable height control |
1312 | { |
||
1313 | SollHoehe = ((int16_t) ExternHoehenValue + (int16_t) Parameter_MaxHoehe) * (int)EE_Parameter.Hoehe_Verstaerkung; |
||
1314 | HoehenReglerAktiv = 1; |
||
1051 | killagreg | 1315 | } |
1322 | hbuss | 1316 | |
1320 | hbuss | 1317 | // calculate cos of nick and roll angle used for projection of the vertical hoover gas |
1328 | hbuss | 1318 | J4Low; |
1320 | hbuss | 1319 | tmp_long = IntegralNick/GIER_GRAD_FAKTOR; // nick angle in deg |
1320 | tmp_long *= tmp_long; |
||
1321 | tmp_long2 = IntegralRoll/GIER_GRAD_FAKTOR; // roll angle in deg |
||
1322 | tmp_long2 *= tmp_long2; |
||
1323 | CosAttitude = (int16_t)c_sqrt(tmp_long + tmp_long2); // phytagoras gives effective attitude angle in deg |
||
1328 | hbuss | 1324 | DebugOut.Analog[16] = CosAttitude; |
1320 | hbuss | 1325 | LIMIT_MAX(CosAttitude, 60); // limit effective attitude angle |
1326 | CosAttitude = c_cos_8192(CosAttitude); // cos of actual attitude |
||
1328 | hbuss | 1327 | J4High; |
1309 | hbuss | 1328 | if(HoehenReglerAktiv && !(MikroKopterFlags & FLAG_NOTLANDUNG)) |
1329 | { |
||
1330 | #define HEIGHT_TRIM_UP 0x01 |
||
1331 | #define HEIGHT_TRIM_DOWN 0x02 |
||
1332 | static unsigned char HeightTrimmingFlag = 0x00; |
||
1333 | |||
1320 | hbuss | 1334 | #define HEIGHT_CONTROL_STICKTHRESHOLD 15 |
1309 | hbuss | 1335 | // Holger original version |
1336 | // start of height control algorithm |
||
1337 | // the height control is only an attenuation of the actual gas stick. |
||
1338 | // I.e. it will work only if the gas stick is higher than the hover gas |
||
1339 | // and the hover height will be allways larger than height setpoint. |
||
1314 | killagreg | 1340 | if((EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) || !(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER)) // Regler wird über Schalter gesteuert) |
1341 | { // old version |
||
1309 | hbuss | 1342 | HCGas = GasMischanteil; // take current stick gas as neutral point for the height control |
1343 | HeightTrimming = 0; |
||
1344 | } |
||
1314 | killagreg | 1345 | else |
1309 | hbuss | 1346 | { |
1347 | // alternative height control |
||
1348 | // PD-Control with respect to hoover point |
||
1349 | // the thrust loss out of horizontal attitude is compensated |
||
1350 | // the setpoint will be fine adjusted with the gas stick position |
||
1351 | if(MikroKopterFlags & FLAG_FLY) // trim setpoint only when flying |
||
1352 | { // gas stick is above hoover point |
||
1322 | hbuss | 1353 | if(StickGas > (StickGasHoover + HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtUpperLimit) |
1309 | hbuss | 1354 | { |
1355 | if(HeightTrimmingFlag & HEIGHT_TRIM_DOWN) |
||
1356 | { |
||
1357 | HeightTrimmingFlag &= ~HEIGHT_TRIM_DOWN; |
||
1358 | SollHoehe = HoehenWert; // update setpoint to current heigth |
||
1359 | } |
||
1360 | HeightTrimmingFlag |= HEIGHT_TRIM_UP; |
||
1320 | hbuss | 1361 | HeightTrimming += abs(StickGas - (StickGasHoover + HEIGHT_CONTROL_STICKTHRESHOLD)); |
1309 | hbuss | 1362 | } // gas stick is below hoover point |
1322 | hbuss | 1363 | else if(StickGas < (StickGasHoover - HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtLowerLimit ) |
1309 | hbuss | 1364 | { |
1365 | if(HeightTrimmingFlag & HEIGHT_TRIM_UP) |
||
1366 | { |
||
1367 | HeightTrimmingFlag &= ~HEIGHT_TRIM_UP; |
||
1368 | SollHoehe = HoehenWert; // update setpoint to current heigth |
||
1369 | } |
||
1370 | HeightTrimmingFlag |= HEIGHT_TRIM_DOWN; |
||
1320 | hbuss | 1371 | HeightTrimming -= abs(StickGas - (StickGasHoover - HEIGHT_CONTROL_STICKTHRESHOLD)); |
1309 | hbuss | 1372 | } |
1373 | else // Gas Stick in Hoover Range |
||
1374 | { |
||
1375 | if(HeightTrimmingFlag & (HEIGHT_TRIM_UP|HEIGHT_TRIM_DOWN)) |
||
1376 | { |
||
1377 | HeightTrimmingFlag &= ~(HEIGHT_TRIM_UP|HEIGHT_TRIM_DOWN); |
||
1378 | HeightTrimming = 0; |
||
1379 | SollHoehe = HoehenWert; // update setpoint to current height |
||
1380 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 500; |
||
1381 | } |
||
1382 | } |
||
1383 | // Trim height set point |
||
1328 | hbuss | 1384 | if(abs(HeightTrimming) > 256) |
1309 | hbuss | 1385 | { |
1328 | hbuss | 1386 | SollHoehe += (HeightTrimming * EE_Parameter.Hoehe_Verstaerkung)/(512 / 2); // move setpoint |
1309 | hbuss | 1387 | HeightTrimming = 0; |
1388 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 75; |
||
1320 | hbuss | 1389 | //update hoover gas stick value when setpoint is shifted |
1322 | hbuss | 1390 | // StickGasHoover = HooverGas/STICK_GAIN; // rescale back to stick value |
1391 | // StickGasHoover = (StickGasHoover * UBat) / BattLowVoltageWarning; |
||
1392 | // if(StickGasHoover < 70) StickGasHoover = 70; |
||
1393 | // else if(StickGasHoover > 150) StickGasHoover = 150; |
||
1309 | hbuss | 1394 | } |
1395 | } //if MikroKopterFlags & MKFLAG_FLY |
||
1320 | hbuss | 1396 | else |
1397 | { |
||
1322 | hbuss | 1398 | SollHoehe = HoehenWert - 400; |
1328 | hbuss | 1399 | if(EE_Parameter.Hoehe_StickNeutralPoint) StickGasHoover = EE_Parameter.Hoehe_StickNeutralPoint; |
1400 | else StickGasHoover = 120; |
||
1320 | hbuss | 1401 | } |
1309 | hbuss | 1402 | HCGas = HooverGas; // take hoover gas (neutral point) |
1403 | } |
||
1314 | killagreg | 1404 | |
1405 | if(HoehenWert > SollHoehe || !(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT)) |
||
1283 | hbuss | 1406 | { |
1309 | hbuss | 1407 | // ------------------------- P-Part ---------------------------- |
1312 | hbuss | 1408 | HeightDeviation = (int)(HoehenWert - SollHoehe); // positive when too high |
1309 | hbuss | 1409 | tmp_int = (HeightDeviation * (int)Parameter_Hoehe_P) / 16; // p-part |
1410 | HCGas -= tmp_int; |
||
1411 | // ------------------------- D-Part 1: Vario Meter ---------------------------- |
||
1412 | tmp_int = VarioMeter / 8; |
||
1413 | if(tmp_int > 8) tmp_int = 8; // limit quadratic part on upward movement to avoid to much gas reduction |
||
1414 | if(tmp_int > 0) tmp_int = VarioMeter + (tmp_int * tmp_int) / 4; |
||
1415 | else tmp_int = VarioMeter - (tmp_int * tmp_int) / 4; |
||
1416 | tmp_int = (Parameter_Luftdruck_D * (long)(tmp_int)) / 128L; // scale to d-gain parameter |
||
1417 | LIMIT_MIN_MAX(tmp_int, -127, 255); |
||
1418 | HCGas -= tmp_int; |
||
1419 | // ------------------------ D-Part 2: ACC-Z Integral ------------------------ |
||
1420 | tmp_int = ((Mess_Integral_Hoch / 128) * (long) Parameter_Hoehe_ACC_Wirkung) / (128 / STICK_GAIN); |
||
1421 | LIMIT_MIN_MAX(tmp_int, -127, 255); |
||
1422 | HCGas -= tmp_int; |
||
1328 | hbuss | 1423 | |
1309 | hbuss | 1424 | // limit deviation from hoover point within the target region |
1314 | killagreg | 1425 | if( (abs(HeightDeviation) < 150) && (!HeightTrimming) && (HooverGas > 0)) // height setpoint is not changed and hoover gas not zero |
1309 | hbuss | 1426 | { |
1427 | LIMIT_MIN_MAX(HCGas, HooverGasMin, HooverGasMax); // limit gas around the hoover point |
||
1428 | } |
||
1276 | hbuss | 1429 | |
1322 | hbuss | 1430 | if(BaroExpandActive) HCGas = HooverGas; |
1309 | hbuss | 1431 | // ------------------------ D-Part 3: GpsZ ---------------------------------- |
1432 | tmp_int = (Parameter_Hoehe_GPS_Z * (long)FromNaviCtrl_Value.GpsZ)/128L; |
||
1322 | hbuss | 1433 | LIMIT_MIN_MAX(tmp_int, -127, 255); |
1309 | hbuss | 1434 | HCGas -= tmp_int; |
1322 | hbuss | 1435 | |
1436 | // strech control output by inverse attitude projection 1/cos |
||
1437 | // + 1/cos(angle) ++++++++++++++++++++++++++ |
||
1320 | hbuss | 1438 | tmp_long3 = (int32_t)HCGas; |
1439 | tmp_long3 *= 8192L; |
||
1440 | tmp_long3 /= CosAttitude; |
||
1441 | HCGas = (int16_t)tmp_long3; |
||
1309 | hbuss | 1442 | // update height control gas averaging |
1443 | FilterHCGas = (FilterHCGas * (HC_GAS_AVERAGE - 1) + HCGas) / HC_GAS_AVERAGE; |
||
1444 | // limit height control gas pd-control output |
||
1445 | LIMIT_MIN_MAX(FilterHCGas, EE_Parameter.Hoehe_MinGas * STICK_GAIN, (MAX_GAS - 20) * STICK_GAIN); |
||
1446 | // set GasMischanteil to HeightControlGasFilter |
||
1314 | killagreg | 1447 | if(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) |
1448 | { // old version |
||
1309 | hbuss | 1449 | if(FilterHCGas > GasMischanteil) FilterHCGas = GasMischanteil; // nicht mehr als Gas |
1314 | killagreg | 1450 | } |
1309 | hbuss | 1451 | GasMischanteil = FilterHCGas; |
1314 | killagreg | 1452 | } |
1309 | hbuss | 1453 | }// EOF height control active |
1320 | hbuss | 1454 | else // HC not active |
1455 | { |
||
1456 | //update hoover gas stick value when HC is not active |
||
1322 | hbuss | 1457 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
1458 | { |
||
1459 | StickGasHoover = HooverGas/STICK_GAIN; // rescale back to stick value |
||
1460 | StickGasHoover = (StickGasHoover * UBat) / BattLowVoltageWarning; |
||
1461 | } |
||
1462 | else StickGasHoover = EE_Parameter.Hoehe_StickNeutralPoint; |
||
1463 | if(StickGasHoover < 70) StickGasHoover = 70; |
||
1464 | else if(StickGasHoover > 150) StickGasHoover = 150; |
||
1328 | hbuss | 1465 | FilterHCGas = GasMischanteil; |
1320 | hbuss | 1466 | } |
1283 | hbuss | 1467 | |
1309 | hbuss | 1468 | // Hoover gas estimation by averaging gas control output on small z-velocities |
1469 | // this is done only if height contol option is selected in global config and aircraft is flying |
||
1470 | if((MikroKopterFlags & FLAG_FLY) && !(MikroKopterFlags & FLAG_NOTLANDUNG)) |
||
1471 | { |
||
1472 | if(HooverGasFilter == 0) HooverGasFilter = HOOVER_GAS_AVERAGE * (unsigned long)(GasMischanteil); // init estimation |
||
1473 | if(abs(VarioMeter) < 100) // only on small vertical speed |
||
1474 | { |
||
1320 | hbuss | 1475 | tmp_long3 = (int32_t)GasMischanteil; // take current thrust |
1476 | tmp_long3 *= CosAttitude; // apply attitude projection |
||
1477 | tmp_long3 /= 8192; |
||
1478 | |||
1309 | hbuss | 1479 | // average vertical projected thrust |
1480 | if(modell_fliegt < 2000) // the first 4 seconds |
||
1481 | { // reduce the time constant of averaging by factor of 8 to get much faster a stable value |
||
1482 | HooverGasFilter -= HooverGasFilter/(HOOVER_GAS_AVERAGE/8L); |
||
1483 | HooverGasFilter += 8L * tmp_long3; |
||
1484 | } |
||
1485 | else if(modell_fliegt < 4000) // the first 8 seconds |
||
1486 | { // reduce the time constant of averaging by factor of 4 to get much faster a stable value |
||
1487 | HooverGasFilter -= HooverGasFilter/(HOOVER_GAS_AVERAGE/4L); |
||
1488 | HooverGasFilter += 4L * tmp_long3; |
||
1489 | } |
||
1490 | else if(modell_fliegt < 8000) // the first 16 seconds |
||
1491 | { // reduce the time constant of averaging by factor of 2 to get much faster a stable value |
||
1492 | HooverGasFilter -= HooverGasFilter/(HOOVER_GAS_AVERAGE/2L); |
||
1493 | HooverGasFilter += 2L * tmp_long3; |
||
1494 | } |
||
1495 | else //later |
||
1496 | { |
||
1497 | HooverGasFilter -= HooverGasFilter/HOOVER_GAS_AVERAGE; |
||
1498 | HooverGasFilter += tmp_long3; |
||
1499 | } |
||
1500 | HooverGas = (int16_t)(HooverGasFilter/HOOVER_GAS_AVERAGE); |
||
1501 | if(EE_Parameter.Hoehe_HoverBand) |
||
1502 | { |
||
1503 | int16_t band; |
||
1504 | band = HooverGas / EE_Parameter.Hoehe_HoverBand; // the higher the parameter the smaller the range |
||
1505 | HooverGasMin = HooverGas - band; |
||
1506 | HooverGasMax = HooverGas + band; |
||
1507 | } |
||
1508 | else |
||
1509 | { // no limit |
||
1510 | HooverGasMin = 0; |
||
1511 | HooverGasMax = 1023; |
||
1512 | } |
||
1513 | } |
||
1514 | } |
||
1328 | hbuss | 1515 | LastHCGas = GasMischanteil; |
1516 | } |
||
1517 | else |
||
1518 | { |
||
1519 | GasMischanteil = LastHCGas; |
||
1520 | } |
||
1322 | hbuss | 1521 | //DebugOut.Analog[26] = HooverGasMax; |
1309 | hbuss | 1522 | }// EOF ParamSet.GlobalConfig & CFG_HEIGHT_CONTROL |
1328 | hbuss | 1523 | J4Low; |
1309 | hbuss | 1524 | |
1525 | // limit gas to parameter setting |
||
1320 | hbuss | 1526 | LIMIT_MIN(GasMischanteil, (MIN_GAS + 10) * STICK_GAIN); |
855 | hbuss | 1527 | if(GasMischanteil > (MAX_GAS - 20) * STICK_GAIN) GasMischanteil = (MAX_GAS - 20) * STICK_GAIN; |
1111 | hbuss | 1528 | |
1051 | killagreg | 1529 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1320 | hbuss | 1530 | // all BL-Ctrl connected? |
1531 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1532 | if(MissingMotor) |
||
1533 | if(modell_fliegt > 1 && modell_fliegt < 50 && GasMischanteil > 0) |
||
1534 | { |
||
1535 | modell_fliegt = 1; |
||
1536 | GasMischanteil = MIN_GAS; |
||
1537 | } |
||
1538 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1 | ingob | 1539 | // + Mischer und PI-Regler |
1051 | killagreg | 1540 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
173 | holgerb | 1541 | DebugOut.Analog[7] = GasMischanteil; |
1051 | killagreg | 1542 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1543 | // Gier-Anteil |
1051 | killagreg | 1544 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
855 | hbuss | 1545 | GierMischanteil = MesswertGier - sollGier * STICK_GAIN; // Regler für Gier |
1546 | #define MIN_GIERGAS (40*STICK_GAIN) // unter diesem Gaswert trotzdem Gieren |
||
693 | hbuss | 1547 | if(GasMischanteil > MIN_GIERGAS) |
1548 | { |
||
1051 | killagreg | 1549 | if(GierMischanteil > (GasMischanteil / 2)) GierMischanteil = GasMischanteil / 2; |
1550 | if(GierMischanteil < -(GasMischanteil / 2)) GierMischanteil = -(GasMischanteil / 2); |
||
693 | hbuss | 1551 | } |
1051 | killagreg | 1552 | else |
693 | hbuss | 1553 | { |
1051 | killagreg | 1554 | if(GierMischanteil > (MIN_GIERGAS / 2)) GierMischanteil = MIN_GIERGAS / 2; |
1555 | if(GierMischanteil < -(MIN_GIERGAS / 2)) GierMischanteil = -(MIN_GIERGAS / 2); |
||
693 | hbuss | 1556 | } |
855 | hbuss | 1557 | tmp_int = MAX_GAS*STICK_GAIN; |
1051 | killagreg | 1558 | if(GierMischanteil > ((tmp_int - GasMischanteil))) GierMischanteil = ((tmp_int - GasMischanteil)); |
855 | hbuss | 1559 | if(GierMischanteil < -((tmp_int - GasMischanteil))) GierMischanteil = -((tmp_int - GasMischanteil)); |
513 | hbuss | 1560 | |
1051 | killagreg | 1561 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1 | ingob | 1562 | // Nick-Achse |
1051 | killagreg | 1563 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
723 | hbuss | 1564 | DiffNick = MesswertNick - StickNick; // Differenz bestimmen |
1153 | hbuss | 1565 | if(IntegralFaktor) SummeNick += IntegralNickMalFaktor - StickNick; // I-Anteil bei Winkelregelung |
1051 | killagreg | 1566 | else SummeNick += DiffNick; // I-Anteil bei HH |
855 | hbuss | 1567 | if(SummeNick > (STICK_GAIN * 16000L)) SummeNick = (STICK_GAIN * 16000L); |
1568 | if(SummeNick < -(16000L * STICK_GAIN)) SummeNick = -(16000L * STICK_GAIN); |
||
1153 | hbuss | 1569 | pd_ergebnis_nick = DiffNick + SummeNick / Ki; // PI-Regler für Nick |
1 | ingob | 1570 | // Motor Vorn |
499 | hbuss | 1571 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
1153 | hbuss | 1572 | if(pd_ergebnis_nick > tmp_int) pd_ergebnis_nick = tmp_int; |
1573 | if(pd_ergebnis_nick < -tmp_int) pd_ergebnis_nick = -tmp_int; |
||
173 | holgerb | 1574 | |
1153 | hbuss | 1575 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1576 | // Roll-Achse |
||
1577 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1578 | DiffRoll = MesswertRoll - StickRoll; // Differenz bestimmen |
||
1579 | if(IntegralFaktor) SummeRoll += IntegralRollMalFaktor - StickRoll;// I-Anteil bei Winkelregelung |
||
1580 | else SummeRoll += DiffRoll; // I-Anteil bei HH |
||
1581 | if(SummeRoll > (STICK_GAIN * 16000L)) SummeRoll = (STICK_GAIN * 16000L); |
||
1582 | if(SummeRoll < -(16000L * STICK_GAIN)) SummeRoll = -(16000L * STICK_GAIN); |
||
1583 | pd_ergebnis_roll = DiffRoll + SummeRoll / Ki; // PI-Regler für Roll |
||
1584 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
||
1585 | if(pd_ergebnis_roll > tmp_int) pd_ergebnis_roll = tmp_int; |
||
1586 | if(pd_ergebnis_roll < -tmp_int) pd_ergebnis_roll = -tmp_int; |
||
1587 | |||
1588 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
1209 | hbuss | 1589 | // Universal Mixer |
1155 | hbuss | 1590 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
1216 | killagreg | 1591 | for(i=0; i<MAX_MOTORS; i++) |
1209 | hbuss | 1592 | { |
1593 | signed int tmp_int; |
||
1594 | if(Mixer.Motor[i][0] > 0) |
||
1595 | { |
||
1596 | tmp_int = ((long)GasMischanteil * Mixer.Motor[i][0]) / 64L; |
||
1597 | tmp_int += ((long)pd_ergebnis_nick * Mixer.Motor[i][1]) / 64L; |
||
1598 | tmp_int += ((long)pd_ergebnis_roll * Mixer.Motor[i][2]) / 64L; |
||
1599 | tmp_int += ((long)GierMischanteil * Mixer.Motor[i][3]) / 64L; |
||
1600 | tmp_motorwert[i] = MotorSmoothing(tmp_int,tmp_motorwert[i]); // Filter |
||
1216 | killagreg | 1601 | tmp_int = tmp_motorwert[i] / STICK_GAIN; |
1209 | hbuss | 1602 | CHECK_MIN_MAX(tmp_int,MIN_GAS,MAX_GAS); |
1216 | killagreg | 1603 | Motor[i] = tmp_int; |
1209 | hbuss | 1604 | } |
1605 | else Motor[i] = 0; |
||
1606 | } |
||
1167 | hbuss | 1607 | /* |
1153 | hbuss | 1608 | if(Poti1 > 20) Motor1 = 0; |
1609 | if(Poti1 > 90) Motor6 = 0; |
||
1610 | if(Poti1 > 140) Motor2 = 0; |
||
1175 | hbuss | 1611 | //if(Poti1 > 200) Motor7 = 0; |
1167 | hbuss | 1612 | */ |
1111 | hbuss | 1613 | } |