Rev 1839 | Rev 1855 | Go to most recent revision | Details | Compare with Previous | Last modification | View Log | RSS feed
| Rev | Author | Line No. | Line |
|---|---|---|---|
| 1 | ingob | 1 | /*####################################################################################### |
| 2 | Flight Control |
||
| 3 | #######################################################################################*/ |
||
| 4 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1338 | ingob | 5 | // + Copyright (c) Holger Buss, Ingo Busker |
| 6 | // + Nur für den privaten Gebrauch / NON-COMMERCIAL USE ONLY |
||
| 1 | ingob | 7 | // + www.MikroKopter.com |
| 8 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 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. |
||
| 11 | // + Sollten direkte oder indirekte kommerzielle Absichten verfolgt werden, ist mit uns (info@mikrokopter.de) Kontakt |
||
| 12 | // + bzgl. der Nutzungsbedingungen aufzunehmen. |
||
| 1 | ingob | 13 | // + Eine kommerzielle Nutzung ist z.B.Verkauf von MikroKoptern, Bestückung und Verkauf von Platinen oder Bausätzen, |
| 14 | // + Verkauf von Luftbildaufnahmen, usw. |
||
| 15 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 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 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 19 | // + Sollte die Software (auch auszugesweise) oder sonstige Informationen des MikroKopter-Projekts |
||
| 20 | // + auf anderen Webseiten oder sonstigen Medien veröffentlicht werden, muss unsere Webseite "http://www.mikrokopter.de" |
||
| 21 | // + eindeutig als Ursprung verlinkt werden |
||
| 22 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 23 | // + Keine Gewähr auf Fehlerfreiheit, Vollständigkeit oder Funktion |
||
| 24 | // + Benutzung auf eigene Gefahr |
||
| 25 | // + Wir übernehmen keinerlei Haftung für direkte oder indirekte Personen- oder Sachschäden |
||
| 26 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1338 | ingob | 27 | // + Die Portierung oder Nutzung 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 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 30 | // + Die Funktion printf_P() unterliegt ihrer eigenen Lizenz und ist hiervon nicht betroffen |
||
| 31 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 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 |
||
| 35 | // + from this software without specific prior written permission. |
||
| 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 |
||
| 1338 | ingob | 42 | // + * porting the sources to other systems or using the software on other systems (except 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 |
||
| 45 | // + IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE |
||
| 46 | // + ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER OR CONTRIBUTORS BE |
||
| 47 | // + LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR |
||
| 48 | // + CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF |
||
| 49 | // + SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS |
||
| 1322 | hbuss | 50 | // + INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN |
| 51 | // + CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) |
||
| 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" |
||
| 1320 | hbuss | 57 | #include "mymath.h" |
| 1330 | killagreg | 58 | #include "isqrt.h" |
| 1 | ingob | 59 | |
| 1352 | hbuss | 60 | unsigned char h,m,s; |
| 61 | unsigned int BaroExpandActive = 0; |
||
| 1153 | hbuss | 62 | int MesswertNick,MesswertRoll,MesswertGier,MesswertGierBias, RohMesswertNick,RohMesswertRoll; |
| 1166 | hbuss | 63 | int TrimNick, TrimRoll; |
| 927 | hbuss | 64 | int AdNeutralNick = 0,AdNeutralRoll = 0,AdNeutralGier = 0,StartNeutralRoll = 0,StartNeutralNick = 0; |
| 1703 | holgerb | 65 | int Mittelwert_AccNick, Mittelwert_AccRoll; |
| 1643 | holgerb | 66 | unsigned int NeutralAccX=0, NeutralAccY=0; |
| 805 | hbuss | 67 | int NaviAccNick, NaviAccRoll,NaviCntAcc = 0; |
| 1639 | holgerb | 68 | int NeutralAccZ = 0; |
| 1683 | killagreg | 69 | unsigned char ControlHeading = 0;// in 2° |
| 693 | hbuss | 70 | long IntegralNick = 0,IntegralNick2 = 0; |
| 71 | long IntegralRoll = 0,IntegralRoll2 = 0; |
||
| 72 | long IntegralAccNick = 0,IntegralAccRoll = 0,IntegralAccZ = 0; |
||
| 73 | long Integral_Gier = 0; |
||
| 74 | long Mess_IntegralNick = 0,Mess_IntegralNick2 = 0; |
||
| 75 | long Mess_IntegralRoll = 0,Mess_IntegralRoll2 = 0; |
||
| 76 | long Mess_Integral_Gier = 0,Mess_Integral_Gier2 = 0; |
||
| 77 | long MittelIntegralNick,MittelIntegralRoll,MittelIntegralNick2,MittelIntegralRoll2; |
||
| 1685 | holgerb | 78 | long SummeNick=0,SummeRoll=0; |
| 1 | ingob | 79 | volatile long Mess_Integral_Hoch = 0; |
| 1840 | holgerb | 80 | int KompassValue = -1; |
| 1837 | holgerb | 81 | int KompassSollWert = 0; |
| 1153 | hbuss | 82 | int KompassRichtung = 0; |
| 1839 | holgerb | 83 | char CalculateCompassTimer = 100; |
| 84 | unsigned char KompassFusion = 32; |
||
| 85 | unsigned int KompassSignalSchlecht = 50; |
||
| 855 | hbuss | 86 | unsigned char MAX_GAS,MIN_GAS; |
| 1 | ingob | 87 | unsigned char HoehenReglerAktiv = 0; |
| 880 | hbuss | 88 | unsigned char TrichterFlug = 0; |
| 395 | hbuss | 89 | long Umschlag180Nick = 250000L, Umschlag180Roll = 250000L; |
| 693 | hbuss | 90 | long ErsatzKompass; |
| 91 | int ErsatzKompassInGrad; // Kompasswert in Grad |
||
| 92 | int GierGyroFehler = 0; |
||
| 1211 | hbuss | 93 | char GyroFaktor,GyroFaktorGier; |
| 94 | char IntegralFaktor,IntegralFaktorGier; |
||
| 1153 | hbuss | 95 | int DiffNick,DiffRoll; |
| 1377 | hbuss | 96 | //int Poti1 = 0, Poti2 = 0, Poti3 = 0, Poti4 = 0, Poti5 = 0, Poti6 = 0, Poti7 = 0, Poti8 = 0; |
| 1391 | killagreg | 97 | unsigned char Poti[9] = {0,0,0,0,0,0,0,0}; |
| 1 | ingob | 98 | volatile unsigned char SenderOkay = 0; |
| 595 | hbuss | 99 | int StickNick = 0,StickRoll = 0,StickGier = 0,StickGas = 0; |
| 1698 | holgerb | 100 | char MotorenEin = 0,StartTrigger = 0; |
| 1246 | killagreg | 101 | long HoehenWert = 0; |
| 102 | long SollHoehe = 0; |
||
| 1840 | holgerb | 103 | int CompassGierSetpoint = 0; |
| 1692 | holgerb | 104 | int LageKorrekturRoll = 0,LageKorrekturNick = 0, HoverGas = 0; |
| 1153 | hbuss | 105 | //float Ki = FAKTOR_I; |
| 1676 | holgerb | 106 | int Ki = 10300 / 33; |
| 395 | hbuss | 107 | unsigned char Looping_Nick = 0,Looping_Roll = 0; |
| 108 | unsigned char Looping_Links = 0, Looping_Rechts = 0, Looping_Unten = 0, Looping_Oben = 0; |
||
| 1 | ingob | 109 | |
| 110 | unsigned char Parameter_Luftdruck_D = 48; // Wert : 0-250 |
||
| 111 | unsigned char Parameter_MaxHoehe = 251; // Wert : 0-250 |
||
| 112 | unsigned char Parameter_Hoehe_P = 16; // Wert : 0-32 |
||
| 113 | unsigned char Parameter_Hoehe_ACC_Wirkung = 58; // Wert : 0-250 |
||
| 114 | unsigned char Parameter_KompassWirkung = 64; // Wert : 0-250 |
||
| 1283 | hbuss | 115 | unsigned char Parameter_Hoehe_GPS_Z = 64; // Wert : 0-250 |
| 1111 | hbuss | 116 | unsigned char Parameter_Gyro_D = 8; // Wert : 0-250 |
| 173 | holgerb | 117 | unsigned char Parameter_Gyro_P = 150; // Wert : 10-250 |
| 1 | ingob | 118 | unsigned char Parameter_Gyro_I = 150; // Wert : 0-250 |
| 1322 | hbuss | 119 | unsigned char Parameter_Gyro_Gier_P = 150; // Wert : 10-250 |
| 120 | unsigned char Parameter_Gyro_Gier_I = 150; // Wert : 10-250 |
||
| 1 | ingob | 121 | unsigned char Parameter_Gier_P = 2; // Wert : 1-20 |
| 122 | unsigned char Parameter_I_Faktor = 10; // Wert : 1-20 |
||
| 123 | unsigned char Parameter_UserParam1 = 0; |
||
| 124 | unsigned char Parameter_UserParam2 = 0; |
||
| 125 | unsigned char Parameter_UserParam3 = 0; |
||
| 126 | unsigned char Parameter_UserParam4 = 0; |
||
| 499 | hbuss | 127 | unsigned char Parameter_UserParam5 = 0; |
| 128 | unsigned char Parameter_UserParam6 = 0; |
||
| 129 | unsigned char Parameter_UserParam7 = 0; |
||
| 130 | unsigned char Parameter_UserParam8 = 0; |
||
| 1 | ingob | 131 | unsigned char Parameter_ServoNickControl = 100; |
| 1232 | hbuss | 132 | unsigned char Parameter_ServoRollControl = 100; |
| 173 | holgerb | 133 | unsigned char Parameter_LoopGasLimit = 70; |
| 1120 | hbuss | 134 | unsigned char Parameter_AchsKopplung1 = 90; |
| 135 | unsigned char Parameter_AchsKopplung2 = 65; |
||
| 136 | unsigned char Parameter_CouplingYawCorrection = 64; |
||
| 137 | //unsigned char Parameter_AchsGegenKopplung1 = 0; |
||
| 499 | hbuss | 138 | unsigned char Parameter_DynamicStability = 100; |
| 921 | hbuss | 139 | unsigned char Parameter_J16Bitmask; // for the J16 Output |
| 140 | unsigned char Parameter_J16Timing; // for the J16 Output |
||
| 141 | unsigned char Parameter_J17Bitmask; // for the J17 Output |
||
| 142 | unsigned char Parameter_J17Timing; // for the J17 Output |
||
| 143 | unsigned char Parameter_NaviGpsModeControl; // Parameters for the Naviboard |
||
| 1051 | killagreg | 144 | unsigned char Parameter_NaviGpsGain; |
| 145 | unsigned char Parameter_NaviGpsP; |
||
| 146 | unsigned char Parameter_NaviGpsI; |
||
| 147 | unsigned char Parameter_NaviGpsD; |
||
| 148 | unsigned char Parameter_NaviGpsACC; |
||
| 993 | hbuss | 149 | unsigned char Parameter_NaviOperatingRadius; |
| 150 | unsigned char Parameter_NaviWindCorrection; |
||
| 151 | unsigned char Parameter_NaviSpeedCompensation; |
||
| 921 | hbuss | 152 | unsigned char Parameter_ExternalControl; |
| 1403 | hbuss | 153 | unsigned char Parameter_Servo3,Parameter_Servo4,Parameter_Servo5; |
| 1668 | holgerb | 154 | unsigned char CareFree = 0; |
| 1760 | holgerb | 155 | const signed char sintab[31] = { 0, 2, 4, 6, 7, 8, 8, 8, 7, 6, 4, 2, 0, -2, -4, -6, -7, -8, -8, -8, -7, -6, -4, -2, 0, 2, 4, 6, 7, 8, 8}; |
| 1622 | killagreg | 156 | |
| 492 | hbuss | 157 | signed int ExternStickNick = 0,ExternStickRoll = 0,ExternStickGier = 0, ExternHoehenValue = -20; |
| 614 | hbuss | 158 | int MaxStickNick = 0,MaxStickRoll = 0; |
| 871 | hbuss | 159 | unsigned int modell_fliegt = 0; |
| 1765 | killagreg | 160 | volatile unsigned char FC_StatusFlags = 0; |
| 1121 | hbuss | 161 | long GIER_GRAD_FAKTOR = 1291; |
| 1153 | hbuss | 162 | signed int KopplungsteilNickRoll,KopplungsteilRollNick; |
| 1209 | hbuss | 163 | signed int tmp_motorwert[MAX_MOTORS]; |
| 1591 | holgerb | 164 | char VarioCharacter = ' '; |
| 165 | |||
| 1391 | killagreg | 166 | #define LIMIT_MIN(value, min) {if(value <= min) value = min;} |
| 167 | #define LIMIT_MAX(value, max) {if(value >= max) value = max;} |
||
| 168 | #define LIMIT_MIN_MAX(value, min, max) {if(value <= min) value = min; else if(value >= max) value = max;} |
||
| 1155 | hbuss | 169 | |
| 1622 | killagreg | 170 | |
| 1639 | holgerb | 171 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 172 | // Debugwerte zuordnen |
||
| 173 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 174 | void CopyDebugValues(void) |
||
| 175 | { |
||
| 176 | DebugOut.Analog[0] = IntegralNick / (EE_Parameter.GyroAccFaktor * 4); |
||
| 177 | DebugOut.Analog[1] = IntegralRoll / (EE_Parameter.GyroAccFaktor * 4); |
||
| 178 | DebugOut.Analog[2] = Mittelwert_AccNick / 4; |
||
| 179 | DebugOut.Analog[3] = Mittelwert_AccRoll / 4; |
||
| 1660 | holgerb | 180 | DebugOut.Analog[4] = (signed int) AdNeutralGier - AdWertGier; |
| 1639 | holgerb | 181 | DebugOut.Analog[5] = HoehenWert/5; |
| 1703 | holgerb | 182 | DebugOut.Analog[6] = AdWertAccHoch;//(Mess_Integral_Hoch / 512);// Aktuell_az; |
| 1639 | holgerb | 183 | DebugOut.Analog[8] = KompassValue; |
| 184 | DebugOut.Analog[9] = UBat; |
||
| 185 | DebugOut.Analog[10] = SenderOkay; |
||
| 186 | DebugOut.Analog[11] = ErsatzKompass / GIER_GRAD_FAKTOR; |
||
| 1702 | holgerb | 187 | DebugOut.Analog[12] = Motor[0].SetPoint; |
| 188 | DebugOut.Analog[13] = Motor[1].SetPoint; |
||
| 189 | DebugOut.Analog[14] = Motor[2].SetPoint; |
||
| 190 | DebugOut.Analog[15] = Motor[3].SetPoint; |
||
| 1639 | holgerb | 191 | DebugOut.Analog[20] = ServoNickValue; |
| 192 | DebugOut.Analog[22] = Capacity.ActualCurrent; |
||
| 193 | DebugOut.Analog[23] = Capacity.UsedCapacity; |
||
| 194 | // DebugOut.Analog[22] = FromNaviCtrl_Value.GpsZ; |
||
| 1682 | holgerb | 195 | // DebugOut.Analog[29] = FromNaviCtrl_Value.SerialDataOkay; |
| 1839 | holgerb | 196 | DebugOut.Analog[27] = KompassSollWert; |
| 1682 | holgerb | 197 | DebugOut.Analog[29] = Capacity.MinOfMaxPWM; |
| 1639 | holgerb | 198 | DebugOut.Analog[30] = GPS_Nick; |
| 199 | DebugOut.Analog[31] = GPS_Roll; |
||
| 1702 | holgerb | 200 | if(VersionInfo.HardwareError[0] || VersionInfo.HardwareError[1]) DebugOut.Status[1] |= 1; else DebugOut.Status[1] &= 0xfe; |
| 1760 | holgerb | 201 | |
| 1787 | holgerb | 202 | //if(Capacity.MinOfMaxPWM < 250/* && modell_fliegt > 500*/) { beeptime = 1000; DebugOut.Analog[25]++; } |
| 1639 | holgerb | 203 | } |
| 204 | |||
| 1760 | holgerb | 205 | |
| 206 | |||
| 1232 | hbuss | 207 | void Piep(unsigned char Anzahl, unsigned int dauer) |
| 1 | ingob | 208 | { |
| 1232 | hbuss | 209 | if(MotorenEin) return; //auf keinen Fall im Flug! |
| 1 | ingob | 210 | while(Anzahl--) |
| 211 | { |
||
| 1232 | hbuss | 212 | beeptime = dauer; |
| 213 | while(beeptime); |
||
| 214 | Delay_ms(dauer * 2); |
||
| 1 | ingob | 215 | } |
| 216 | } |
||
| 217 | |||
| 218 | //############################################################################ |
||
| 1622 | killagreg | 219 | // Messwerte beim Ermitteln der Nullage |
| 220 | void CalibrierMittelwert(void) |
||
| 221 | //############################################################################ |
||
| 222 | { |
||
| 223 | unsigned char i; |
||
| 224 | if(PlatinenVersion == 13) SucheGyroOffset(); |
||
| 225 | // ADC auschalten, damit die Werte sich nicht während der Berechnung ändern |
||
| 226 | ANALOG_OFF; |
||
| 227 | MesswertNick = AdWertNick; |
||
| 228 | MesswertRoll = AdWertRoll; |
||
| 229 | MesswertGier = AdWertGier; |
||
| 1703 | holgerb | 230 | Mittelwert_AccNick = ACC_AMPLIFY * AdWertAccNick; |
| 231 | Mittelwert_AccRoll = ACC_AMPLIFY * AdWertAccRoll; |
||
| 1622 | killagreg | 232 | // ADC einschalten |
| 233 | ANALOG_ON; |
||
| 234 | for(i=0;i<8;i++) |
||
| 235 | { |
||
| 236 | int tmp; |
||
| 237 | tmp = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
||
| 238 | LIMIT_MIN_MAX(tmp, 0, 255); |
||
| 239 | if(Poti[i] > tmp) Poti[i]--; else if(Poti[i] < tmp) Poti[i]++; |
||
| 240 | } |
||
| 241 | Umschlag180Nick = (long) EE_Parameter.WinkelUmschlagNick * 2500L; |
||
| 242 | Umschlag180Roll = (long) EE_Parameter.WinkelUmschlagRoll * 2500L; |
||
| 243 | } |
||
| 244 | |||
| 245 | //############################################################################ |
||
| 1 | ingob | 246 | // Nullwerte ermitteln |
| 1622 | killagreg | 247 | void SetNeutral(unsigned char AccAdjustment) |
| 1 | ingob | 248 | //############################################################################ |
| 249 | { |
||
| 1622 | killagreg | 250 | unsigned char i; |
| 251 | unsigned int gier_neutral=0, nick_neutral=0, roll_neutral=0; |
||
| 1702 | holgerb | 252 | VersionInfo.HardwareError[0] = 0; |
| 1320 | hbuss | 253 | HEF4017R_ON; |
| 1051 | killagreg | 254 | NeutralAccX = 0; |
| 1 | ingob | 255 | NeutralAccY = 0; |
| 256 | NeutralAccZ = 0; |
||
| 1622 | killagreg | 257 | |
| 1051 | killagreg | 258 | AdNeutralNick = 0; |
| 259 | AdNeutralRoll = 0; |
||
| 1 | ingob | 260 | AdNeutralGier = 0; |
| 1622 | killagreg | 261 | |
| 395 | hbuss | 262 | Parameter_AchsKopplung1 = 0; |
| 1120 | hbuss | 263 | Parameter_AchsKopplung2 = 0; |
| 1622 | killagreg | 264 | |
| 1036 | hbuss | 265 | ExpandBaro = 0; |
| 1622 | killagreg | 266 | |
| 1051 | killagreg | 267 | CalibrierMittelwert(); |
| 395 | hbuss | 268 | Delay_ms_Mess(100); |
| 1622 | killagreg | 269 | |
| 1 | ingob | 270 | CalibrierMittelwert(); |
| 1622 | killagreg | 271 | |
| 1 | ingob | 272 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
| 1051 | killagreg | 273 | { |
| 1 | ingob | 274 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
| 275 | } |
||
| 1166 | hbuss | 276 | #define NEUTRAL_FILTER 32 |
| 277 | for(i=0; i<NEUTRAL_FILTER; i++) |
||
| 1111 | hbuss | 278 | { |
| 279 | Delay_ms_Mess(10); |
||
| 1216 | killagreg | 280 | gier_neutral += AdWertGier; |
| 1166 | hbuss | 281 | nick_neutral += AdWertNick; |
| 282 | roll_neutral += AdWertRoll; |
||
| 1111 | hbuss | 283 | } |
| 1173 | hbuss | 284 | AdNeutralNick= (nick_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
| 285 | AdNeutralRoll= (roll_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
||
| 286 | AdNeutralGier= (gier_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER); |
||
| 1622 | killagreg | 287 | |
| 401 | hbuss | 288 | StartNeutralRoll = AdNeutralRoll; |
| 289 | StartNeutralNick = AdNeutralNick; |
||
| 1622 | killagreg | 290 | |
| 291 | if(AccAdjustment) |
||
| 292 | { |
||
| 293 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
||
| 294 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
||
| 295 | NeutralAccZ = Aktuell_az; |
||
| 296 | |||
| 297 | // Save ACC neutral settings to eeprom |
||
| 1639 | holgerb | 298 | SetParamWord(PID_ACC_NICK, (uint16_t)NeutralAccX); |
| 299 | SetParamWord(PID_ACC_ROLL, (uint16_t)NeutralAccY); |
||
| 1622 | killagreg | 300 | SetParamWord(PID_ACC_TOP, (uint16_t)NeutralAccZ); |
| 513 | hbuss | 301 | } |
| 1051 | killagreg | 302 | else |
| 513 | hbuss | 303 | { |
| 1622 | killagreg | 304 | // restore from eeprom |
| 305 | NeutralAccX = (int16_t)GetParamWord(PID_ACC_NICK); |
||
| 306 | NeutralAccY = (int16_t)GetParamWord(PID_ACC_ROLL); |
||
| 307 | NeutralAccZ = (int16_t)GetParamWord(PID_ACC_TOP); |
||
| 308 | // strange settings? |
||
| 1638 | holgerb | 309 | if(((unsigned int) NeutralAccX > 2048) || ((unsigned int) NeutralAccY > 2048) || ((unsigned int) NeutralAccZ > 1024)) |
| 1622 | killagreg | 310 | { |
| 311 | printf("\n\rACC not calibrated!\r\n"); |
||
| 312 | NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
||
| 313 | NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
||
| 314 | NeutralAccZ = Aktuell_az; |
||
| 315 | } |
||
| 513 | hbuss | 316 | } |
| 1051 | killagreg | 317 | |
| 1 | ingob | 318 | MesswertNick = 0; |
| 319 | MesswertRoll = 0; |
||
| 320 | MesswertGier = 0; |
||
| 1111 | hbuss | 321 | Delay_ms_Mess(100); |
| 1703 | holgerb | 322 | Mittelwert_AccNick = ACC_AMPLIFY * AdWertAccNick; |
| 323 | Mittelwert_AccRoll = ACC_AMPLIFY * AdWertAccRoll; |
||
| 1173 | hbuss | 324 | IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
| 325 | IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
||
| 326 | Mess_IntegralNick2 = IntegralNick; |
||
| 327 | Mess_IntegralRoll2 = IntegralRoll; |
||
| 328 | Mess_Integral_Gier = 0; |
||
| 1 | ingob | 329 | StartLuftdruck = Luftdruck; |
| 1253 | killagreg | 330 | VarioMeter = 0; |
| 1 | ingob | 331 | Mess_Integral_Hoch = 0; |
| 1837 | holgerb | 332 | KompassSollWert = KompassValue; |
| 1839 | holgerb | 333 | KompassSignalSchlecht = 100; |
| 1 | ingob | 334 | GPS_Neutral(); |
| 1051 | killagreg | 335 | beeptime = 50; |
| 882 | hbuss | 336 | Umschlag180Nick = ((long) EE_Parameter.WinkelUmschlagNick * 2500L) + 15000L; |
| 337 | Umschlag180Roll = ((long) EE_Parameter.WinkelUmschlagRoll * 2500L) + 15000L; |
||
| 492 | hbuss | 338 | ExternHoehenValue = 0; |
| 693 | hbuss | 339 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
| 340 | GierGyroFehler = 0; |
||
| 723 | hbuss | 341 | SendVersionToNavi = 1; |
| 921 | hbuss | 342 | LED_Init(); |
| 1765 | killagreg | 343 | FC_StatusFlags |= FC_STATUS_CALIBRATE; |
| 992 | hbuss | 344 | FromNaviCtrl_Value.Kalman_K = -1; |
| 1173 | hbuss | 345 | FromNaviCtrl_Value.Kalman_MaxDrift = 0; |
| 992 | hbuss | 346 | FromNaviCtrl_Value.Kalman_MaxFusion = 32; |
| 1391 | killagreg | 347 | |
| 348 | for(i=0;i<8;i++) |
||
| 1377 | hbuss | 349 | { |
| 350 | Poti[i] = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
||
| 351 | } |
||
| 1171 | hbuss | 352 | SenderOkay = 100; |
| 1320 | hbuss | 353 | if(ServoActive) |
| 354 | { |
||
| 355 | HEF4017R_ON; |
||
| 356 | DDRD |=0x80; // enable J7 -> Servo signal |
||
| 357 | } |
||
| 1702 | holgerb | 358 | |
| 1765 | killagreg | 359 | if((AdNeutralNick < 150 * 16) || (AdNeutralNick > 850 * 16)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_NICK; }; |
| 360 | if((AdNeutralRoll < 150 * 16) || (AdNeutralRoll > 850 * 16)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_ROLL; }; |
||
| 361 | if((AdNeutralGier < 150 * 2) || (AdNeutralGier > 850 * 2)) { VersionInfo.HardwareError[0] |= FC_ERROR0_GYRO_YAW; }; |
||
| 362 | if((NeutralAccX < 300) || (NeutralAccX > 750)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_NICK; }; |
||
| 363 | if((NeutralAccY < 300) || (NeutralAccY > 750)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_ROLL; }; |
||
| 364 | if((NeutralAccZ < 512) || (NeutralAccZ > 850)) { VersionInfo.HardwareError[0] |= FC_ERROR0_ACC_TOP; }; |
||
| 1 | ingob | 365 | } |
| 366 | |||
| 1702 | holgerb | 367 | |
| 1 | ingob | 368 | //############################################################################ |
| 395 | hbuss | 369 | // Bearbeitet die Messwerte |
| 1 | ingob | 370 | void Mittelwert(void) |
| 371 | //############################################################################ |
||
| 1051 | killagreg | 372 | { |
| 1111 | hbuss | 373 | static signed long tmpl,tmpl2,tmpl3,tmpl4; |
| 374 | static signed int oldNick, oldRoll, d2Roll, d2Nick; |
||
| 1153 | hbuss | 375 | signed long winkel_nick, winkel_roll; |
| 1111 | hbuss | 376 | MesswertGier = (signed int) AdNeutralGier - AdWertGier; |
| 1171 | hbuss | 377 | MesswertNick = (signed int) AdWertNickFilter / 8; |
| 378 | MesswertRoll = (signed int) AdWertRollFilter / 8; |
||
| 1153 | hbuss | 379 | RohMesswertNick = MesswertNick; |
| 380 | RohMesswertRoll = MesswertRoll; |
||
| 1166 | hbuss | 381 | |
| 395 | hbuss | 382 | // Beschleunigungssensor ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1703 | holgerb | 383 | Mittelwert_AccNick = (Mittelwert_AccNick * 3 + ((ACC_AMPLIFY * AdWertAccNick))) / 4L; |
| 384 | Mittelwert_AccRoll = (Mittelwert_AccRoll * 3 + ((ACC_AMPLIFY * AdWertAccRoll))) / 4L; |
||
| 395 | hbuss | 385 | IntegralAccNick += ACC_AMPLIFY * AdWertAccNick; |
| 386 | IntegralAccRoll += ACC_AMPLIFY * AdWertAccRoll; |
||
| 805 | hbuss | 387 | NaviAccNick += AdWertAccNick; |
| 388 | NaviAccRoll += AdWertAccRoll; |
||
| 389 | NaviCntAcc++; |
||
| 1153 | hbuss | 390 | IntegralAccZ += Aktuell_az - NeutralAccZ; |
| 391 | |||
| 1155 | hbuss | 392 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
| 393 | // ADC einschalten |
||
| 1171 | hbuss | 394 | ANALOG_ON; |
| 1155 | hbuss | 395 | AdReady = 0; |
| 396 | //++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 397 | |||
| 1216 | killagreg | 398 | if(Mess_IntegralRoll > 93000L) winkel_roll = 93000L; |
| 399 | else if(Mess_IntegralRoll <-93000L) winkel_roll = -93000L; |
||
| 1153 | hbuss | 400 | else winkel_roll = Mess_IntegralRoll; |
| 401 | |||
| 1216 | killagreg | 402 | if(Mess_IntegralNick > 93000L) winkel_nick = 93000L; |
| 403 | else if(Mess_IntegralNick <-93000L) winkel_nick = -93000L; |
||
| 1153 | hbuss | 404 | else winkel_nick = Mess_IntegralNick; |
| 405 | |||
| 1120 | hbuss | 406 | // Gier ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1153 | hbuss | 407 | Mess_Integral_Gier += MesswertGier; |
| 408 | ErsatzKompass += MesswertGier; |
||
| 395 | hbuss | 409 | // Kopplungsanteil +++++++++++++++++++++++++++++++++++++ |
| 410 | if(!Looping_Nick && !Looping_Roll && (EE_Parameter.GlobalConfig & CFG_ACHSENKOPPLUNG_AKTIV)) |
||
| 411 | { |
||
| 1153 | hbuss | 412 | tmpl3 = (MesswertRoll * winkel_nick) / 2048L; |
| 1120 | hbuss | 413 | tmpl3 *= Parameter_AchsKopplung2; //65 |
| 1111 | hbuss | 414 | tmpl3 /= 4096L; |
| 1153 | hbuss | 415 | tmpl4 = (MesswertNick * winkel_roll) / 2048L; |
| 1216 | killagreg | 416 | tmpl4 *= Parameter_AchsKopplung2; //65 |
| 1111 | hbuss | 417 | tmpl4 /= 4096L; |
| 1153 | hbuss | 418 | KopplungsteilNickRoll = tmpl3; |
| 419 | KopplungsteilRollNick = tmpl4; |
||
| 1111 | hbuss | 420 | tmpl4 -= tmpl3; |
| 421 | ErsatzKompass += tmpl4; |
||
| 1166 | hbuss | 422 | if(!Parameter_CouplingYawCorrection) Mess_Integral_Gier -= tmpl4/2; // Gier nachhelfen |
| 1111 | hbuss | 423 | |
| 1153 | hbuss | 424 | tmpl = ((MesswertGier + tmpl4) * winkel_nick) / 2048L; |
| 1111 | hbuss | 425 | tmpl *= Parameter_AchsKopplung1; // 90 |
| 880 | hbuss | 426 | tmpl /= 4096L; |
| 1153 | hbuss | 427 | tmpl2 = ((MesswertGier + tmpl4) * winkel_roll) / 2048L; |
| 395 | hbuss | 428 | tmpl2 *= Parameter_AchsKopplung1; |
| 1662 | killagreg | 429 | tmpl2 /= 4096L; |
| 1225 | hbuss | 430 | if(abs(MesswertGier) > 64) if(labs(tmpl) > 128 || labs(tmpl2) > 128) TrichterFlug = 1; |
| 1153 | hbuss | 431 | //MesswertGier += (Parameter_CouplingYawCorrection * tmpl4) / 256; |
| 395 | hbuss | 432 | } |
| 1166 | hbuss | 433 | else tmpl = tmpl2 = KopplungsteilNickRoll = KopplungsteilRollNick = 0; |
| 1658 | holgerb | 434 | TrimRoll = tmpl - tmpl2 / 100L; |
| 435 | TrimNick = -tmpl2 + tmpl / 100L; |
||
| 1111 | hbuss | 436 | // Kompasswert begrenzen ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 437 | if(ErsatzKompass >= (360L * GIER_GRAD_FAKTOR)) ErsatzKompass -= 360L * GIER_GRAD_FAKTOR; // 360° Umschlag |
||
| 438 | if(ErsatzKompass < 0) ErsatzKompass += 360L * GIER_GRAD_FAKTOR; |
||
| 395 | hbuss | 439 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1166 | hbuss | 440 | Mess_IntegralRoll2 += MesswertRoll + TrimRoll; |
| 441 | Mess_IntegralRoll += MesswertRoll + TrimRoll - LageKorrekturRoll; |
||
| 1051 | killagreg | 442 | if(Mess_IntegralRoll > Umschlag180Roll) |
| 395 | hbuss | 443 | { |
| 882 | hbuss | 444 | Mess_IntegralRoll = -(Umschlag180Roll - 25000L); |
| 395 | hbuss | 445 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
| 1051 | killagreg | 446 | } |
| 395 | hbuss | 447 | if(Mess_IntegralRoll <-Umschlag180Roll) |
| 448 | { |
||
| 882 | hbuss | 449 | Mess_IntegralRoll = (Umschlag180Roll - 25000L); |
| 395 | hbuss | 450 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
| 1051 | killagreg | 451 | } |
| 395 | hbuss | 452 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1166 | hbuss | 453 | Mess_IntegralNick2 += MesswertNick + TrimNick; |
| 454 | Mess_IntegralNick += MesswertNick + TrimNick - LageKorrekturNick; |
||
| 1051 | killagreg | 455 | if(Mess_IntegralNick > Umschlag180Nick) |
| 882 | hbuss | 456 | { |
| 457 | Mess_IntegralNick = -(Umschlag180Nick - 25000L); |
||
| 458 | Mess_IntegralNick2 = Mess_IntegralNick; |
||
| 1051 | killagreg | 459 | } |
| 460 | if(Mess_IntegralNick <-Umschlag180Nick) |
||
| 395 | hbuss | 461 | { |
| 882 | hbuss | 462 | Mess_IntegralNick = (Umschlag180Nick - 25000L); |
| 395 | hbuss | 463 | Mess_IntegralNick2 = Mess_IntegralNick; |
| 1051 | killagreg | 464 | } |
| 1111 | hbuss | 465 | |
| 1 | ingob | 466 | Integral_Gier = Mess_Integral_Gier; |
| 467 | IntegralNick = Mess_IntegralNick; |
||
| 468 | IntegralRoll = Mess_IntegralRoll; |
||
| 1051 | killagreg | 469 | IntegralNick2 = Mess_IntegralNick2; |
| 1 | ingob | 470 | IntegralRoll2 = Mess_IntegralRoll2; |
| 471 | |||
| 1166 | hbuss | 472 | #define D_LIMIT 128 |
| 473 | |||
| 1171 | hbuss | 474 | MesswertNick = HiResNick / 8; |
| 475 | MesswertRoll = HiResRoll / 8; |
||
| 1166 | hbuss | 476 | |
| 1167 | hbuss | 477 | if(AdWertNick < 15) MesswertNick = -1000; if(AdWertNick < 7) MesswertNick = -2000; |
| 478 | if(PlatinenVersion == 10) { if(AdWertNick > 1010) MesswertNick = +1000; if(AdWertNick > 1017) MesswertNick = +2000; } |
||
| 479 | else { if(AdWertNick > 2000) MesswertNick = +1000; if(AdWertNick > 2015) MesswertNick = +2000; } |
||
| 480 | if(AdWertRoll < 15) MesswertRoll = -1000; if(AdWertRoll < 7) MesswertRoll = -2000; |
||
| 481 | if(PlatinenVersion == 10) { if(AdWertRoll > 1010) MesswertRoll = +1000; if(AdWertRoll > 1017) MesswertRoll = +2000; } |
||
| 482 | else { if(AdWertRoll > 2000) MesswertRoll = +1000; if(AdWertRoll > 2015) MesswertRoll = +2000; } |
||
| 483 | |||
| 1216 | killagreg | 484 | if(Parameter_Gyro_D) |
| 1111 | hbuss | 485 | { |
| 1166 | hbuss | 486 | d2Nick = HiResNick - oldNick; |
| 487 | oldNick = (oldNick + HiResNick)/2; |
||
| 1111 | hbuss | 488 | if(d2Nick > D_LIMIT) d2Nick = D_LIMIT; |
| 489 | else if(d2Nick < -D_LIMIT) d2Nick = -D_LIMIT; |
||
| 1791 | holgerb | 490 | |
| 1166 | hbuss | 491 | d2Roll = HiResRoll - oldRoll; |
| 492 | oldRoll = (oldRoll + HiResRoll)/2; |
||
| 1111 | hbuss | 493 | if(d2Roll > D_LIMIT) d2Roll = D_LIMIT; |
| 494 | else if(d2Roll < -D_LIMIT) d2Roll = -D_LIMIT; |
||
| 1791 | holgerb | 495 | |
| 496 | MesswertNick += (d2Nick * (signed int) Parameter_Gyro_D) / 16; |
||
| 1166 | hbuss | 497 | MesswertRoll += (d2Roll * (signed int) Parameter_Gyro_D) / 16; |
| 498 | HiResNick += (d2Nick * (signed int) Parameter_Gyro_D); |
||
| 499 | HiResRoll += (d2Roll * (signed int) Parameter_Gyro_D); |
||
| 1216 | killagreg | 500 | } |
| 1111 | hbuss | 501 | |
| 1166 | hbuss | 502 | if(RohMesswertRoll > 0) TrimRoll += ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
| 503 | else TrimRoll -= ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
||
| 504 | if(RohMesswertNick > 0) TrimNick += ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
||
| 505 | else TrimNick -= ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
||
| 1153 | hbuss | 506 | |
| 507 | if(EE_Parameter.GlobalConfig & CFG_DREHRATEN_BEGRENZER && !Looping_Nick && !Looping_Roll) |
||
| 508 | { |
||
| 509 | if(RohMesswertNick > 256) MesswertNick += 1 * (RohMesswertNick - 256); |
||
| 510 | else if(RohMesswertNick < -256) MesswertNick += 1 * (RohMesswertNick + 256); |
||
| 511 | if(RohMesswertRoll > 256) MesswertRoll += 1 * (RohMesswertRoll - 256); |
||
| 512 | else if(RohMesswertRoll < -256) MesswertRoll += 1 * (RohMesswertRoll + 256); |
||
| 513 | } |
||
| 1 | ingob | 514 | } |
| 515 | |||
| 516 | //############################################################################ |
||
| 517 | // Senden der Motorwerte per I2C-Bus |
||
| 518 | void SendMotorData(void) |
||
| 519 | //############################################################################ |
||
| 1051 | killagreg | 520 | { |
| 1209 | hbuss | 521 | unsigned char i; |
| 921 | hbuss | 522 | if(!MotorenEin) |
| 1 | ingob | 523 | { |
| 1765 | killagreg | 524 | FC_StatusFlags &= ~(FC_STATUS_MOTOR_RUN | FC_STATUS_FLY); |
| 1216 | killagreg | 525 | for(i=0;i<MAX_MOTORS;i++) |
| 526 | { |
||
| 527 | if(!PC_MotortestActive) MotorTest[i] = 0; |
||
| 1638 | holgerb | 528 | Motor[i].SetPoint = MotorTest[i]; |
| 529 | Motor[i].SetPointLowerBits = 0; |
||
| 530 | /* |
||
| 1760 | holgerb | 531 | Motor[i].SetPoint = MotorTest[i] / 4; // testing the high resolution |
| 532 | Motor[i].SetPointLowerBits = MotorTest[i] % 4; |
||
| 1638 | holgerb | 533 | */ |
| 1216 | killagreg | 534 | } |
| 1212 | hbuss | 535 | if(PC_MotortestActive) PC_MotortestActive--; |
| 1216 | killagreg | 536 | } |
| 1765 | killagreg | 537 | else FC_StatusFlags |= FC_STATUS_MOTOR_RUN; |
| 1744 | holgerb | 538 | |
| 1765 | killagreg | 539 | if(I2C_TransferActive) |
| 1744 | holgerb | 540 | { |
| 1760 | holgerb | 541 | I2C_TransferActive = 0; // enable for the next time |
| 1765 | killagreg | 542 | } |
| 543 | else |
||
| 1744 | holgerb | 544 | { |
| 545 | motor_write = 0; |
||
| 1760 | holgerb | 546 | I2C_Start(TWI_STATE_MOTOR_TX); //Start I2C Interrupt Mode |
| 1765 | killagreg | 547 | } |
| 1 | ingob | 548 | } |
| 549 | |||
| 550 | |||
| 551 | |||
| 552 | //############################################################################ |
||
| 553 | // Trägt ggf. das Poti als Parameter ein |
||
| 1051 | killagreg | 554 | void ParameterZuordnung(void) |
| 1 | ingob | 555 | //############################################################################ |
| 556 | { |
||
| 1787 | holgerb | 557 | unsigned char tmp,i; |
| 1839 | holgerb | 558 | static unsigned char carefree_old = 2; |
| 1391 | killagreg | 559 | #define CHK_POTI(b,a) {if(a < 248) b = a; else b = Poti[255 - a];} |
| 560 | #define CHK_POTI_MM(b,a,min,max) {CHK_POTI(b,a); LIMIT_MIN_MAX(b, min, max);} |
||
| 1787 | holgerb | 561 | for(i=0;i<8;i++) |
| 562 | { |
||
| 563 | int tmp2; |
||
| 564 | tmp2 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1 + i]] + 110; |
||
| 565 | if(tmp2 > 255) tmp2 = 255; else if(tmp2 < 0) tmp2 = 0; |
||
| 566 | if(tmp2 != Poti[i]) |
||
| 567 | { |
||
| 568 | Poti[i] += (tmp2 - Poti[i]) / 4; |
||
| 569 | if(Poti[i] > tmp2) Poti[i]--; |
||
| 570 | else Poti[i]++; |
||
| 571 | } |
||
| 572 | } |
||
| 921 | hbuss | 573 | CHK_POTI_MM(Parameter_Luftdruck_D,EE_Parameter.Luftdruck_D,0,100); |
| 574 | CHK_POTI_MM(Parameter_Hoehe_P,EE_Parameter.Hoehe_P,0,100); |
||
| 575 | CHK_POTI_MM(Parameter_Gyro_P,EE_Parameter.Gyro_P,10,255); |
||
| 576 | CHK_POTI_MM(Parameter_J16Timing,EE_Parameter.J16Timing,1,255); |
||
| 577 | CHK_POTI_MM(Parameter_J17Timing,EE_Parameter.J17Timing,1,255); |
||
| 1403 | hbuss | 578 | CHK_POTI(Parameter_Servo3,EE_Parameter.Servo3); |
| 579 | CHK_POTI(Parameter_Servo4,EE_Parameter.Servo4); |
||
| 580 | CHK_POTI(Parameter_Servo5,EE_Parameter.Servo5); |
||
| 1377 | hbuss | 581 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
| 1403 | hbuss | 582 | CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe); |
| 1377 | hbuss | 583 | CHK_POTI(Parameter_Hoehe_ACC_Wirkung,EE_Parameter.Hoehe_ACC_Wirkung); |
| 584 | CHK_POTI(Parameter_Hoehe_GPS_Z,EE_Parameter.Hoehe_GPS_Z); |
||
| 585 | CHK_POTI(Parameter_KompassWirkung,EE_Parameter.KompassWirkung); |
||
| 586 | CHK_POTI(Parameter_Gyro_I,EE_Parameter.Gyro_I); |
||
| 587 | CHK_POTI(Parameter_Gyro_D,EE_Parameter.Gyro_D); |
||
| 588 | CHK_POTI(Parameter_Gyro_Gier_P,EE_Parameter.Gyro_Gier_P); |
||
| 589 | CHK_POTI(Parameter_Gyro_Gier_I,EE_Parameter.Gyro_Gier_I); |
||
| 590 | CHK_POTI(Parameter_I_Faktor,EE_Parameter.I_Faktor); |
||
| 591 | CHK_POTI(Parameter_UserParam1,EE_Parameter.UserParam1); |
||
| 592 | CHK_POTI(Parameter_UserParam2,EE_Parameter.UserParam2); |
||
| 593 | CHK_POTI(Parameter_UserParam3,EE_Parameter.UserParam3); |
||
| 594 | CHK_POTI(Parameter_UserParam4,EE_Parameter.UserParam4); |
||
| 595 | CHK_POTI(Parameter_UserParam5,EE_Parameter.UserParam5); |
||
| 596 | CHK_POTI(Parameter_UserParam6,EE_Parameter.UserParam6); |
||
| 597 | CHK_POTI(Parameter_UserParam7,EE_Parameter.UserParam7); |
||
| 598 | CHK_POTI(Parameter_UserParam8,EE_Parameter.UserParam8); |
||
| 599 | CHK_POTI(Parameter_ServoNickControl,EE_Parameter.ServoNickControl); |
||
| 600 | CHK_POTI(Parameter_ServoRollControl,EE_Parameter.ServoRollControl); |
||
| 601 | CHK_POTI(Parameter_LoopGasLimit,EE_Parameter.LoopGasLimit); |
||
| 1668 | holgerb | 602 | CHK_POTI(Parameter_AchsKopplung1,EE_Parameter.AchsKopplung1); |
| 603 | CHK_POTI(Parameter_AchsKopplung2,EE_Parameter.AchsKopplung2); |
||
| 1377 | hbuss | 604 | CHK_POTI(Parameter_CouplingYawCorrection,EE_Parameter.CouplingYawCorrection); |
| 605 | // CHK_POTI(Parameter_AchsGegenKopplung1,EE_Parameter.AchsGegenKopplung1,0,255); |
||
| 606 | CHK_POTI(Parameter_DynamicStability,EE_Parameter.DynamicStability); |
||
| 607 | CHK_POTI(Parameter_ExternalControl,EE_Parameter.ExternalControl); |
||
| 1676 | holgerb | 608 | Ki = 10300 / (Parameter_I_Faktor + 1); |
| 1 | ingob | 609 | MAX_GAS = EE_Parameter.Gas_Max; |
| 1662 | killagreg | 610 | MIN_GAS = EE_Parameter.Gas_Min; |
| 1668 | holgerb | 611 | |
| 612 | tmp = EE_Parameter.OrientationModeControl; |
||
| 1690 | holgerb | 613 | if(tmp > 50) |
| 1668 | holgerb | 614 | { |
| 1682 | holgerb | 615 | #ifdef SWITCH_LEARNS_CAREFREE |
| 1839 | holgerb | 616 | if(!CareFree) ControlHeading = (((int) EE_Parameter.OrientationAngle * 15 + KompassValue) % 360) / 2; |
| 1682 | holgerb | 617 | #endif |
| 618 | CareFree = 1; |
||
| 1839 | holgerb | 619 | if(tmp >= 248 && Poti[255 - tmp] < 50) CareFree = 0; |
| 620 | if(carefree_old == 0 && CareFree) beeptime = 1000; |
||
| 621 | if(carefree_old == 1 && !CareFree) beeptime = 200; |
||
| 622 | carefree_old = CareFree; |
||
| 623 | if(FromNaviCtrl.CompassValue < 0 && CareFree) VersionInfo.HardwareError[0] |= FC_ERROR0_CAREFREE; else VersionInfo.HardwareError[0] &= ~FC_ERROR0_CAREFREE; |
||
| 1669 | killagreg | 624 | } |
| 1839 | holgerb | 625 | else |
| 626 | { |
||
| 627 | CareFree = 0; |
||
| 628 | carefree_old = 0; |
||
| 629 | } |
||
| 1668 | holgerb | 630 | |
| 1691 | holgerb | 631 | if(FromNaviCtrl.CompassValue < 0 && MotorenEin && CareFree && BeepMuster == 0xffff) // ungültiger Kompasswert |
| 1690 | holgerb | 632 | { |
| 633 | beeptime = 15000; |
||
| 634 | BeepMuster = 0xA400; |
||
| 635 | CareFree = 0; |
||
| 1765 | killagreg | 636 | } |
| 1702 | holgerb | 637 | |
| 1668 | holgerb | 638 | if(CareFree) {if(Parameter_AchsKopplung1 < 210) Parameter_AchsKopplung1 += 30;} |
| 1 | ingob | 639 | } |
| 640 | |||
| 641 | //############################################################################ |
||
| 642 | // |
||
| 643 | void MotorRegler(void) |
||
| 644 | //############################################################################ |
||
| 645 | { |
||
| 1330 | killagreg | 646 | int pd_ergebnis_nick,pd_ergebnis_roll,tmp_int, tmp_int2; |
| 1 | ingob | 647 | int GierMischanteil,GasMischanteil; |
| 648 | static long sollGier = 0,tmp_long,tmp_long2; |
||
| 395 | hbuss | 649 | static long IntegralFehlerNick = 0; |
| 650 | static long IntegralFehlerRoll = 0; |
||
| 1 | ingob | 651 | static unsigned int RcLostTimer; |
| 652 | static unsigned char delay_neutral = 0; |
||
| 653 | static unsigned char delay_einschalten = 0,delay_ausschalten = 0; |
||
| 1622 | killagreg | 654 | static unsigned char calibration_done = 0; |
| 1 | ingob | 655 | static char NeueKompassRichtungMerken = 0; |
| 395 | hbuss | 656 | static long ausgleichNick, ausgleichRoll; |
| 1153 | hbuss | 657 | int IntegralNickMalFaktor,IntegralRollMalFaktor; |
| 1209 | hbuss | 658 | unsigned char i; |
| 1051 | killagreg | 659 | Mittelwert(); |
| 1 | ingob | 660 | GRN_ON; |
| 1051 | killagreg | 661 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 662 | // Gaswert ermitteln |
| 1051 | killagreg | 663 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 664 | GasMischanteil = StickGas; |
||
| 831 | hbuss | 665 | if(GasMischanteil < MIN_GAS + 10) GasMischanteil = MIN_GAS + 10; |
| 1330 | killagreg | 666 | |
| 1051 | killagreg | 667 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 693 | hbuss | 668 | // Empfang schlecht |
| 1051 | killagreg | 669 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 670 | if(SenderOkay < 100) |
| 671 | { |
||
| 1051 | killagreg | 672 | if(RcLostTimer) RcLostTimer--; |
| 673 | else |
||
| 1 | ingob | 674 | { |
| 675 | MotorenEin = 0; |
||
| 1765 | killagreg | 676 | FC_StatusFlags &= ~FC_STATUS_EMERGENCY_LANDING; |
| 1051 | killagreg | 677 | } |
| 1 | ingob | 678 | ROT_ON; |
| 693 | hbuss | 679 | if(modell_fliegt > 1000) // wahrscheinlich in der Luft --> langsam absenken |
| 1 | ingob | 680 | { |
| 681 | GasMischanteil = EE_Parameter.NotGas; |
||
| 1765 | killagreg | 682 | FC_StatusFlags |= FC_STATUS_EMERGENCY_LANDING; |
| 744 | hbuss | 683 | PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
| 1051 | killagreg | 684 | PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
| 1 | ingob | 685 | PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
| 686 | PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
||
| 687 | PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] = 0; |
||
| 173 | holgerb | 688 | } |
| 1 | ingob | 689 | else MotorenEin = 0; |
| 690 | } |
||
| 1051 | killagreg | 691 | else |
| 692 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1 | ingob | 693 | // Emfang gut |
| 1051 | killagreg | 694 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 695 | if(SenderOkay > 140) |
| 696 | { |
||
| 1765 | killagreg | 697 | FC_StatusFlags &= ~FC_STATUS_EMERGENCY_LANDING; |
| 1 | ingob | 698 | RcLostTimer = EE_Parameter.NotGasZeit * 50; |
| 921 | hbuss | 699 | if(GasMischanteil > 40 && MotorenEin) |
| 1 | ingob | 700 | { |
| 701 | if(modell_fliegt < 0xffff) modell_fliegt++; |
||
| 702 | } |
||
| 871 | hbuss | 703 | if((modell_fliegt < 256)) |
| 1 | ingob | 704 | { |
| 705 | SummeNick = 0; |
||
| 706 | SummeRoll = 0; |
||
| 1682 | holgerb | 707 | sollGier = 0; |
| 708 | Mess_Integral_Gier = 0; |
||
| 1765 | killagreg | 709 | } else FC_StatusFlags |= FC_STATUS_FLY; |
| 1051 | killagreg | 710 | |
| 595 | hbuss | 711 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] > 80) && MotorenEin == 0) |
| 1 | ingob | 712 | { |
| 1051 | killagreg | 713 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 714 | // auf Nullwerte kalibrieren |
| 1051 | killagreg | 715 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 716 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) // Neutralwerte |
| 717 | { |
||
| 718 | if(++delay_neutral > 200) // nicht sofort |
||
| 719 | { |
||
| 720 | GRN_OFF; |
||
| 721 | MotorenEin = 0; |
||
| 722 | delay_neutral = 0; |
||
| 723 | modell_fliegt = 0; |
||
| 724 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) > 70) |
||
| 725 | { |
||
| 304 | ingob | 726 | unsigned char setting=1; |
| 1 | ingob | 727 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 1; |
| 728 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 2; |
||
| 729 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 3; |
||
| 730 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 4; |
||
| 731 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 5; |
||
| 1622 | killagreg | 732 | SetActiveParamSet(setting); // aktiven Datensatz merken |
| 1 | ingob | 733 | } |
| 1051 | killagreg | 734 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 30 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -70) |
| 735 | { |
||
| 819 | hbuss | 736 | WinkelOut.CalcState = 1; |
| 737 | beeptime = 1000; |
||
| 738 | } |
||
| 739 | else |
||
| 1 | ingob | 740 | { |
| 1622 | killagreg | 741 | ParamSet_ReadFromEEProm(GetActiveParamSet()); |
| 1413 | killagreg | 742 | LipoDetection(0); |
| 1626 | killagreg | 743 | LIBFC_ReceiverInit(EE_Parameter.Receiver); |
| 819 | hbuss | 744 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
| 745 | { |
||
| 1 | ingob | 746 | if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
| 1051 | killagreg | 747 | } |
| 1330 | killagreg | 748 | ServoActive = 0; |
| 1622 | killagreg | 749 | SetNeutral(0); |
| 1765 | killagreg | 750 | calibration_done = 1; |
| 1232 | hbuss | 751 | ServoActive = 1; |
| 752 | DDRD |=0x80; // enable J7 -> Servo signal |
||
| 1622 | killagreg | 753 | Piep(GetActiveParamSet(),120); |
| 819 | hbuss | 754 | } |
| 1051 | killagreg | 755 | } |
| 1 | ingob | 756 | } |
| 1051 | killagreg | 757 | else |
| 513 | hbuss | 758 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) // ACC Neutralwerte speichern |
| 759 | { |
||
| 760 | if(++delay_neutral > 200) // nicht sofort |
||
| 761 | { |
||
| 762 | GRN_OFF; |
||
| 763 | MotorenEin = 0; |
||
| 764 | delay_neutral = 0; |
||
| 765 | modell_fliegt = 0; |
||
| 1622 | killagreg | 766 | SetNeutral(1); |
| 767 | calibration_done = 1; |
||
| 768 | Piep(GetActiveParamSet(),120); |
||
| 1051 | killagreg | 769 | } |
| 513 | hbuss | 770 | } |
| 1 | ingob | 771 | else delay_neutral = 0; |
| 772 | } |
||
| 1051 | killagreg | 773 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 774 | // Gas ist unten |
| 1051 | killagreg | 775 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1760 | holgerb | 776 | |
| 595 | hbuss | 777 | if(PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] < 35-120) |
| 1 | ingob | 778 | { |
| 1521 | killagreg | 779 | // Motoren Starten |
| 780 | if(!MotorenEin) |
||
| 781 | { |
||
| 1760 | holgerb | 782 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) && (PPM_in[EE_Parameter.MotorSafetySwitch] < -75 || EE_Parameter.MotorSafetySwitch == 0)) |
| 1521 | killagreg | 783 | { |
| 1051 | killagreg | 784 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 785 | // Einschalten |
| 1051 | killagreg | 786 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1521 | killagreg | 787 | if(++delay_einschalten > 200) |
| 788 | { |
||
| 789 | delay_einschalten = 0; |
||
| 1834 | holgerb | 790 | if(!VersionInfo.HardwareError[0] && calibration_done && !NC_ErrorCode) |
| 1622 | killagreg | 791 | { |
| 792 | modell_fliegt = 1; |
||
| 793 | MotorenEin = 1; |
||
| 794 | sollGier = 0; |
||
| 795 | Mess_Integral_Gier = 0; |
||
| 796 | Mess_Integral_Gier2 = 0; |
||
| 797 | Mess_IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
||
| 798 | Mess_IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
||
| 799 | Mess_IntegralNick2 = IntegralNick; |
||
| 800 | Mess_IntegralRoll2 = IntegralRoll; |
||
| 801 | SummeNick = 0; |
||
| 802 | SummeRoll = 0; |
||
| 1765 | killagreg | 803 | FC_StatusFlags |= FC_STATUS_START; |
| 1669 | killagreg | 804 | ControlHeading = (((int) EE_Parameter.OrientationAngle * 15 + KompassValue) % 360) / 2; |
| 1840 | holgerb | 805 | NeueKompassRichtungMerken = 100; // 2 sekunden |
| 1622 | killagreg | 806 | } |
| 807 | else |
||
| 808 | { |
||
| 809 | beeptime = 1500; // indicate missing calibration |
||
| 810 | } |
||
| 1521 | killagreg | 811 | } |
| 812 | } |
||
| 813 | else delay_einschalten = 0; |
||
| 814 | } |
||
| 1051 | killagreg | 815 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 816 | // Auschalten |
| 1051 | killagreg | 817 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1521 | killagreg | 818 | else // only if motors are running |
| 819 | { |
||
| 1760 | holgerb | 820 | if((PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) && (PPM_in[EE_Parameter.MotorSafetySwitch] < -75 || EE_Parameter.MotorSafetySwitch == 0)) |
| 1521 | killagreg | 821 | { |
| 822 | if(++delay_ausschalten > 200) // nicht sofort |
||
| 823 | { |
||
| 824 | MotorenEin = 0; |
||
| 825 | delay_ausschalten = 0; |
||
| 826 | modell_fliegt = 0; |
||
| 827 | } |
||
| 828 | } |
||
| 829 | else delay_ausschalten = 0; |
||
| 830 | } |
||
| 1 | ingob | 831 | } |
| 832 | } |
||
| 1051 | killagreg | 833 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 834 | // neue Werte von der Funke |
| 1051 | killagreg | 835 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1216 | killagreg | 836 | |
| 1765 | killagreg | 837 | if(!NewPpmData-- || (FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
| 1 | ingob | 838 | { |
| 604 | hbuss | 839 | static int stick_nick,stick_roll; |
| 1 | ingob | 840 | ParameterZuordnung(); |
| 1051 | killagreg | 841 | stick_nick = (stick_nick * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_P) / 4; |
| 723 | hbuss | 842 | stick_nick += PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] * EE_Parameter.Stick_D; |
| 843 | stick_roll = (stick_roll * 3 + PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_P) / 4; |
||
| 844 | stick_roll += PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] * EE_Parameter.Stick_D; |
||
| 845 | |||
| 1707 | holgerb | 846 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 847 | // CareFree und freie Wahl der vorderen Richtung |
||
| 848 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1668 | holgerb | 849 | if(CareFree) |
| 1658 | holgerb | 850 | { |
| 1664 | holgerb | 851 | signed int nick, roll; |
| 852 | nick = stick_nick / 4; |
||
| 853 | roll = stick_roll / 4; |
||
| 854 | StickNick = ((FromNC_Rotate_C * nick) + (FromNC_Rotate_S * roll)) / (32 / 4); |
||
| 855 | StickRoll = ((FromNC_Rotate_C * roll) - (FromNC_Rotate_S * nick)) / (32 / 4); |
||
| 1658 | holgerb | 856 | } |
| 1662 | killagreg | 857 | else |
| 1658 | holgerb | 858 | { |
| 1668 | holgerb | 859 | FromNC_Rotate_C = sintab[EE_Parameter.OrientationAngle + 6]; |
| 860 | FromNC_Rotate_S = sintab[EE_Parameter.OrientationAngle]; |
||
| 861 | StickNick = ((FromNC_Rotate_C * stick_nick) + (FromNC_Rotate_S * stick_roll)) / 8; |
||
| 862 | StickRoll = ((FromNC_Rotate_C * stick_roll) - (FromNC_Rotate_S * stick_nick)) / 8; |
||
| 1658 | holgerb | 863 | } |
| 1662 | killagreg | 864 | |
| 1 | ingob | 865 | StickGier = -PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]; |
| 1840 | holgerb | 866 | if(StickGier > 4) StickGier -= 4; else |
| 867 | if(StickGier < -4) StickGier += 4; else StickGier = 0; |
||
| 1120 | hbuss | 868 | |
| 1658 | holgerb | 869 | StickNick -= (GPS_Nick + GPS_Nick2); |
| 870 | StickRoll -= (GPS_Roll + GPS_Roll2); |
||
| 1350 | hbuss | 871 | StickGas = PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] + 120; |
| 1330 | killagreg | 872 | |
| 1153 | hbuss | 873 | GyroFaktor = (Parameter_Gyro_P + 10.0); |
| 874 | IntegralFaktor = Parameter_Gyro_I; |
||
| 1322 | hbuss | 875 | GyroFaktorGier = (Parameter_Gyro_Gier_P + 10.0); |
| 876 | IntegralFaktorGier = Parameter_Gyro_Gier_I; |
||
| 1 | ingob | 877 | |
| 595 | hbuss | 878 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 879 | //+ Analoge Steuerung per Seriell |
||
| 880 | //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 921 | hbuss | 881 | if(ExternControl.Config & 0x01 && Parameter_ExternalControl > 128) |
| 595 | hbuss | 882 | { |
| 883 | StickNick += (int) ExternControl.Nick * (int) EE_Parameter.Stick_P; |
||
| 884 | StickRoll += (int) ExternControl.Roll * (int) EE_Parameter.Stick_P; |
||
| 885 | StickGier += ExternControl.Gier; |
||
| 886 | ExternHoehenValue = (int) ExternControl.Hight * (int)EE_Parameter.Hoehe_Verstaerkung; |
||
| 887 | if(ExternControl.Gas < StickGas) StickGas = ExternControl.Gas; |
||
| 888 | } |
||
| 855 | hbuss | 889 | if(StickGas < 0) StickGas = 0; |
| 1330 | killagreg | 890 | |
| 1 | ingob | 891 | if(EE_Parameter.GlobalConfig & CFG_HEADING_HOLD) IntegralFaktor = 0; |
| 723 | hbuss | 892 | |
| 1051 | killagreg | 893 | if(abs(StickNick/STICK_GAIN) > MaxStickNick) |
| 928 | hbuss | 894 | { |
| 1051 | killagreg | 895 | MaxStickNick = abs(StickNick)/STICK_GAIN; |
| 928 | hbuss | 896 | if(MaxStickNick > 100) MaxStickNick = 100; |
| 1051 | killagreg | 897 | } |
| 928 | hbuss | 898 | else MaxStickNick--; |
| 1051 | killagreg | 899 | if(abs(StickRoll/STICK_GAIN) > MaxStickRoll) |
| 928 | hbuss | 900 | { |
| 1051 | killagreg | 901 | MaxStickRoll = abs(StickRoll)/STICK_GAIN; |
| 928 | hbuss | 902 | if(MaxStickRoll > 100) MaxStickRoll = 100; |
| 1051 | killagreg | 903 | } |
| 928 | hbuss | 904 | else MaxStickRoll--; |
| 1765 | killagreg | 905 | if(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING) {MaxStickNick = 0; MaxStickRoll = 0;} |
| 723 | hbuss | 906 | |
| 1051 | killagreg | 907 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 173 | holgerb | 908 | // Looping? |
| 1051 | killagreg | 909 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 993 | hbuss | 910 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_LINKS) Looping_Links = 1; |
| 1051 | killagreg | 911 | else |
| 912 | { |
||
| 395 | hbuss | 913 | { |
| 1051 | killagreg | 914 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Links = 0; |
| 915 | } |
||
| 916 | } |
||
| 993 | hbuss | 917 | if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_RECHTS) Looping_Rechts = 1; |
| 1051 | killagreg | 918 | else |
| 395 | hbuss | 919 | { |
| 920 | if(Looping_Rechts) // Hysterese |
||
| 921 | { |
||
| 922 | if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Rechts = 0; |
||
| 923 | } |
||
| 1051 | killagreg | 924 | } |
| 173 | holgerb | 925 | |
| 993 | hbuss | 926 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_OBEN) Looping_Oben = 1; |
| 1051 | killagreg | 927 | else |
| 928 | { |
||
| 395 | hbuss | 929 | if(Looping_Oben) // Hysterese |
| 930 | { |
||
| 1051 | killagreg | 931 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Oben = 0; |
| 932 | } |
||
| 933 | } |
||
| 993 | hbuss | 934 | if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_UNTEN) Looping_Unten = 1; |
| 1051 | killagreg | 935 | else |
| 395 | hbuss | 936 | { |
| 937 | if(Looping_Unten) // Hysterese |
||
| 938 | { |
||
| 939 | if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Unten = 0; |
||
| 940 | } |
||
| 1051 | killagreg | 941 | } |
| 395 | hbuss | 942 | |
| 943 | if(Looping_Links || Looping_Rechts) Looping_Roll = 1; else Looping_Roll = 0; |
||
| 1153 | hbuss | 944 | if(Looping_Oben || Looping_Unten) { Looping_Nick = 1; Looping_Roll = 0; Looping_Links = 0; Looping_Rechts = 0;} else Looping_Nick = 0; |
| 395 | hbuss | 945 | } // Ende neue Funken-Werte |
| 946 | |||
| 947 | if(Looping_Roll || Looping_Nick) |
||
| 948 | { |
||
| 173 | holgerb | 949 | if(GasMischanteil > EE_Parameter.LoopGasLimit) GasMischanteil = EE_Parameter.LoopGasLimit; |
| 1153 | hbuss | 950 | TrichterFlug = 1; |
| 173 | holgerb | 951 | } |
| 952 | |||
| 1051 | killagreg | 953 | |
| 954 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 955 | // Bei Empfangsausfall im Flug |
||
| 956 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1765 | killagreg | 957 | if(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING) |
| 1 | ingob | 958 | { |
| 959 | StickGier = 0; |
||
| 960 | StickNick = 0; |
||
| 961 | StickRoll = 0; |
||
| 1211 | hbuss | 962 | GyroFaktor = 90; |
| 963 | IntegralFaktor = 120; |
||
| 964 | GyroFaktorGier = 90; |
||
| 965 | IntegralFaktorGier = 120; |
||
| 173 | holgerb | 966 | Looping_Roll = 0; |
| 967 | Looping_Nick = 0; |
||
| 1051 | killagreg | 968 | } |
| 395 | hbuss | 969 | |
| 970 | |||
| 1051 | killagreg | 971 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 972 | // Integrale auf ACC-Signal abgleichen |
| 1051 | killagreg | 973 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 974 | #define ABGLEICH_ANZAHL 256L |
| 975 | |||
| 976 | MittelIntegralNick += IntegralNick; // Für die Mittelwertbildung aufsummieren |
||
| 977 | MittelIntegralRoll += IntegralRoll; |
||
| 978 | MittelIntegralNick2 += IntegralNick2; |
||
| 979 | MittelIntegralRoll2 += IntegralRoll2; |
||
| 980 | |||
| 981 | if(Looping_Nick || Looping_Roll) |
||
| 982 | { |
||
| 983 | IntegralAccNick = 0; |
||
| 984 | IntegralAccRoll = 0; |
||
| 985 | MittelIntegralNick = 0; |
||
| 986 | MittelIntegralRoll = 0; |
||
| 987 | MittelIntegralNick2 = 0; |
||
| 988 | MittelIntegralRoll2 = 0; |
||
| 989 | Mess_IntegralNick2 = Mess_IntegralNick; |
||
| 990 | Mess_IntegralRoll2 = Mess_IntegralRoll; |
||
| 991 | ZaehlMessungen = 0; |
||
| 498 | hbuss | 992 | LageKorrekturNick = 0; |
| 993 | LageKorrekturRoll = 0; |
||
| 395 | hbuss | 994 | } |
| 995 | |||
| 1051 | killagreg | 996 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1224 | hbuss | 997 | if(!Looping_Nick && !Looping_Roll && (Aktuell_az > 512 || MotorenEin)) |
| 469 | hbuss | 998 | { |
| 999 | long tmp_long, tmp_long2; |
||
| 1839 | holgerb | 1000 | if(FromNaviCtrl_Value.Kalman_K > 0 /*&& !TrichterFlug*/) |
| 992 | hbuss | 1001 | { |
| 1002 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
||
| 1051 | killagreg | 1003 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
| 1004 | tmp_long = (tmp_long * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
||
| 1005 | tmp_long2 = (tmp_long2 * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
||
| 1839 | holgerb | 1006 | KompassFusion = FromNaviCtrl_Value.Kalman_K; |
| 992 | hbuss | 1007 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
| 1008 | { |
||
| 1009 | tmp_long /= 2; |
||
| 1010 | tmp_long2 /= 2; |
||
| 1011 | } |
||
| 1012 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
||
| 1013 | { |
||
| 1014 | tmp_long /= 3; |
||
| 1015 | tmp_long2 /= 3; |
||
| 1016 | } |
||
| 1017 | if(tmp_long > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 1018 | if(tmp_long < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 1019 | if(tmp_long2 > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 1020 | if(tmp_long2 < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
||
| 1021 | } |
||
| 1051 | killagreg | 1022 | else |
| 992 | hbuss | 1023 | { |
| 1024 | tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
||
| 1051 | killagreg | 1025 | tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
| 992 | hbuss | 1026 | tmp_long /= 16; |
| 1027 | tmp_long2 /= 16; |
||
| 1028 | if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
||
| 1029 | { |
||
| 1030 | tmp_long /= 3; |
||
| 1031 | tmp_long2 /= 3; |
||
| 1216 | killagreg | 1032 | } |
| 1033 | if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
||
| 992 | hbuss | 1034 | { |
| 1035 | tmp_long /= 3; |
||
| 1036 | tmp_long2 /= 3; |
||
| 1037 | } |
||
| 1839 | holgerb | 1038 | KompassFusion = 25; |
| 1155 | hbuss | 1039 | #define AUSGLEICH 32 |
| 992 | hbuss | 1040 | if(tmp_long > AUSGLEICH) tmp_long = AUSGLEICH; |
| 1041 | if(tmp_long < -AUSGLEICH) tmp_long =-AUSGLEICH; |
||
| 1042 | if(tmp_long2 > AUSGLEICH) tmp_long2 = AUSGLEICH; |
||
| 1043 | if(tmp_long2 <-AUSGLEICH) tmp_long2 =-AUSGLEICH; |
||
| 1044 | } |
||
| 1166 | hbuss | 1045 | |
| 1111 | hbuss | 1046 | Mess_IntegralNick -= tmp_long; |
| 1047 | Mess_IntegralRoll -= tmp_long2; |
||
| 469 | hbuss | 1048 | } |
| 1051 | killagreg | 1049 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 1050 | if(ZaehlMessungen >= ABGLEICH_ANZAHL) |
| 1051 | { |
||
| 1052 | static int cnt = 0; |
||
| 1053 | static char last_n_p,last_n_n,last_r_p,last_r_n; |
||
| 1054 | static long MittelIntegralNick_Alt,MittelIntegralRoll_Alt; |
||
| 1173 | hbuss | 1055 | if(!Looping_Nick && !Looping_Roll && !TrichterFlug && EE_Parameter.Driftkomp) |
| 173 | holgerb | 1056 | { |
| 395 | hbuss | 1057 | MittelIntegralNick /= ABGLEICH_ANZAHL; |
| 1058 | MittelIntegralRoll /= ABGLEICH_ANZAHL; |
||
| 1059 | IntegralAccNick = (EE_Parameter.GyroAccFaktor * IntegralAccNick) / ABGLEICH_ANZAHL; |
||
| 1060 | IntegralAccRoll = (EE_Parameter.GyroAccFaktor * IntegralAccRoll) / ABGLEICH_ANZAHL; |
||
| 1061 | IntegralAccZ = IntegralAccZ / ABGLEICH_ANZAHL; |
||
| 1707 | holgerb | 1062 | #define MAX_I 0 |
| 395 | hbuss | 1063 | // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1064 | IntegralFehlerNick = (long)(MittelIntegralNick - (long)IntegralAccNick); |
||
| 1065 | ausgleichNick = IntegralFehlerNick / EE_Parameter.GyroAccAbgleich; |
||
| 1051 | killagreg | 1066 | // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1067 | IntegralFehlerRoll = (long)(MittelIntegralRoll - (long)IntegralAccRoll); |
||
| 395 | hbuss | 1068 | ausgleichRoll = IntegralFehlerRoll / EE_Parameter.GyroAccAbgleich; |
| 614 | hbuss | 1069 | |
| 1070 | LageKorrekturNick = ausgleichNick / ABGLEICH_ANZAHL; |
||
| 498 | hbuss | 1071 | LageKorrekturRoll = ausgleichRoll / ABGLEICH_ANZAHL; |
| 395 | hbuss | 1072 | |
| 992 | hbuss | 1073 | if(((MaxStickNick > 64) || (MaxStickRoll > 64) || (abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25)) && (FromNaviCtrl_Value.Kalman_K == -1)) |
| 614 | hbuss | 1074 | { |
| 1075 | LageKorrekturNick /= 2; |
||
| 720 | ingob | 1076 | LageKorrekturRoll /= 2; |
| 614 | hbuss | 1077 | } |
| 498 | hbuss | 1078 | |
| 1051 | killagreg | 1079 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 1080 | // Gyro-Drift ermitteln |
| 1051 | killagreg | 1081 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 395 | hbuss | 1082 | MittelIntegralNick2 /= ABGLEICH_ANZAHL; |
| 1083 | MittelIntegralRoll2 /= ABGLEICH_ANZAHL; |
||
| 1051 | killagreg | 1084 | tmp_long = IntegralNick2 - IntegralNick; |
| 1085 | tmp_long2 = IntegralRoll2 - IntegralRoll; |
||
| 395 | hbuss | 1086 | |
| 1087 | IntegralFehlerNick = tmp_long; |
||
| 1088 | IntegralFehlerRoll = tmp_long2; |
||
| 1089 | Mess_IntegralNick2 -= IntegralFehlerNick; |
||
| 1090 | Mess_IntegralRoll2 -= IntegralFehlerRoll; |
||
| 1091 | |||
| 1111 | hbuss | 1092 | if(EE_Parameter.Driftkomp) |
| 1093 | { |
||
| 1622 | killagreg | 1094 | if(GierGyroFehler > ABGLEICH_ANZAHL/2) { AdNeutralGier++; } |
| 1095 | if(GierGyroFehler <-ABGLEICH_ANZAHL/2) { AdNeutralGier--; } |
||
| 1111 | hbuss | 1096 | } |
| 693 | hbuss | 1097 | GierGyroFehler = 0; |
| 720 | ingob | 1098 | |
| 1243 | killagreg | 1099 | #define FEHLER_LIMIT (ABGLEICH_ANZAHL / 2) |
| 1100 | #define FEHLER_LIMIT1 (ABGLEICH_ANZAHL * 2) //4 |
||
| 1225 | hbuss | 1101 | #define FEHLER_LIMIT2 (ABGLEICH_ANZAHL * 16) //16 |
| 492 | hbuss | 1102 | #define BEWEGUNGS_LIMIT 20000 |
| 395 | hbuss | 1103 | // Nick +++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1104 | cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
||
| 1225 | hbuss | 1105 | if(labs(IntegralFehlerNick) > FEHLER_LIMIT1) cnt = 4; |
| 1173 | hbuss | 1106 | if(labs(MittelIntegralNick_Alt - MittelIntegralNick) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
| 492 | hbuss | 1107 | { |
| 1051 | killagreg | 1108 | if(IntegralFehlerNick > FEHLER_LIMIT2) |
| 395 | hbuss | 1109 | { |
| 1051 | killagreg | 1110 | if(last_n_p) |
| 395 | hbuss | 1111 | { |
| 1173 | hbuss | 1112 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1113 | ausgleichNick = IntegralFehlerNick / 8; |
| 401 | hbuss | 1114 | if(ausgleichNick > 5000) ausgleichNick = 5000; |
| 498 | hbuss | 1115 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
| 1051 | killagreg | 1116 | } |
| 395 | hbuss | 1117 | else last_n_p = 1; |
| 1118 | } else last_n_p = 0; |
||
| 1051 | killagreg | 1119 | if(IntegralFehlerNick < -FEHLER_LIMIT2) |
| 395 | hbuss | 1120 | { |
| 1121 | if(last_n_n) |
||
| 1051 | killagreg | 1122 | { |
| 1173 | hbuss | 1123 | cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1124 | ausgleichNick = IntegralFehlerNick / 8; |
| 401 | hbuss | 1125 | if(ausgleichNick < -5000) ausgleichNick = -5000; |
| 498 | hbuss | 1126 | LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
| 1051 | killagreg | 1127 | } |
| 395 | hbuss | 1128 | else last_n_n = 1; |
| 1129 | } else last_n_n = 0; |
||
| 1051 | killagreg | 1130 | } |
| 1131 | else |
||
| 847 | hbuss | 1132 | { |
| 1133 | cnt = 0; |
||
| 1839 | holgerb | 1134 | KompassSignalSchlecht = 100; |
| 1051 | killagreg | 1135 | } |
| 499 | hbuss | 1136 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
| 1173 | hbuss | 1137 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
| 395 | hbuss | 1138 | if(IntegralFehlerNick > FEHLER_LIMIT) AdNeutralNick += cnt; |
| 1139 | if(IntegralFehlerNick < -FEHLER_LIMIT) AdNeutralNick -= cnt; |
||
| 401 | hbuss | 1140 | |
| 395 | hbuss | 1141 | // Roll +++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1695 | holgerb | 1142 | cnt = 1;// + labs(IntegralFehlerRoll) / 4096; |
| 1225 | hbuss | 1143 | if(labs(IntegralFehlerRoll) > FEHLER_LIMIT1) cnt = 4; |
| 1173 | hbuss | 1144 | if(labs(MittelIntegralRoll_Alt - MittelIntegralRoll) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
| 492 | hbuss | 1145 | { |
| 1051 | killagreg | 1146 | if(IntegralFehlerRoll > FEHLER_LIMIT2) |
| 395 | hbuss | 1147 | { |
| 1051 | killagreg | 1148 | if(last_r_p) |
| 395 | hbuss | 1149 | { |
| 1173 | hbuss | 1150 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1151 | ausgleichRoll = IntegralFehlerRoll / 8; |
| 401 | hbuss | 1152 | if(ausgleichRoll > 5000) ausgleichRoll = 5000; |
| 498 | hbuss | 1153 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
| 1051 | killagreg | 1154 | } |
| 395 | hbuss | 1155 | else last_r_p = 1; |
| 1156 | } else last_r_p = 0; |
||
| 1051 | killagreg | 1157 | if(IntegralFehlerRoll < -FEHLER_LIMIT2) |
| 395 | hbuss | 1158 | { |
| 1051 | killagreg | 1159 | if(last_r_n) |
| 395 | hbuss | 1160 | { |
| 1173 | hbuss | 1161 | cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
| 492 | hbuss | 1162 | ausgleichRoll = IntegralFehlerRoll / 8; |
| 401 | hbuss | 1163 | if(ausgleichRoll < -5000) ausgleichRoll = -5000; |
| 498 | hbuss | 1164 | LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
| 395 | hbuss | 1165 | } |
| 1166 | else last_r_n = 1; |
||
| 1167 | } else last_r_n = 0; |
||
| 1051 | killagreg | 1168 | } else |
| 492 | hbuss | 1169 | { |
| 1170 | cnt = 0; |
||
| 1839 | holgerb | 1171 | KompassSignalSchlecht = 100; |
| 1051 | killagreg | 1172 | } |
| 499 | hbuss | 1173 | if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
| 1173 | hbuss | 1174 | if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
| 395 | hbuss | 1175 | if(IntegralFehlerRoll > FEHLER_LIMIT) AdNeutralRoll += cnt; |
| 1176 | if(IntegralFehlerRoll < -FEHLER_LIMIT) AdNeutralRoll -= cnt; |
||
| 173 | holgerb | 1177 | } |
| 1051 | killagreg | 1178 | else |
| 498 | hbuss | 1179 | { |
| 1180 | LageKorrekturRoll = 0; |
||
| 1181 | LageKorrekturNick = 0; |
||
| 880 | hbuss | 1182 | TrichterFlug = 0; |
| 498 | hbuss | 1183 | } |
| 1051 | killagreg | 1184 | |
| 498 | hbuss | 1185 | if(!IntegralFaktor) { LageKorrekturRoll = 0; LageKorrekturNick = 0;} // z.B. bei HH |
| 1051 | killagreg | 1186 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1187 | MittelIntegralNick_Alt = MittelIntegralNick; |
||
| 1188 | MittelIntegralRoll_Alt = MittelIntegralRoll; |
||
| 1189 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 395 | hbuss | 1190 | IntegralAccNick = 0; |
| 1191 | IntegralAccRoll = 0; |
||
| 1192 | IntegralAccZ = 0; |
||
| 1193 | MittelIntegralNick = 0; |
||
| 1194 | MittelIntegralRoll = 0; |
||
| 1195 | MittelIntegralNick2 = 0; |
||
| 1196 | MittelIntegralRoll2 = 0; |
||
| 1197 | ZaehlMessungen = 0; |
||
| 1173 | hbuss | 1198 | } // ZaehlMessungen >= ABGLEICH_ANZAHL |
| 395 | hbuss | 1199 | |
| 1051 | killagreg | 1200 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1201 | // Gieren |
| 1051 | killagreg | 1202 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1840 | holgerb | 1203 | if(abs(StickGier) > 3) // war 15 |
| 1 | ingob | 1204 | { |
| 1839 | holgerb | 1205 | // KompassSignalSchlecht = 1000; |
| 1051 | killagreg | 1206 | if(!(EE_Parameter.GlobalConfig & CFG_KOMPASS_FIX)) |
| 1207 | { |
||
| 1840 | holgerb | 1208 | NeueKompassRichtungMerken = 50; // eine Sekunde zum Einloggen |
| 824 | hbuss | 1209 | }; |
| 1 | ingob | 1210 | } |
| 395 | hbuss | 1211 | tmp_int = (long) EE_Parameter.Gier_P * ((long)StickGier * abs(StickGier)) / 512L; // expo y = ax + bx² |
| 1051 | killagreg | 1212 | tmp_int += (EE_Parameter.Gier_P * StickGier) / 4; |
| 1840 | holgerb | 1213 | tmp_int += CompassGierSetpoint; |
| 173 | holgerb | 1214 | sollGier = tmp_int; |
| 1051 | killagreg | 1215 | Mess_Integral_Gier -= tmp_int; |
| 395 | hbuss | 1216 | if(Mess_Integral_Gier > 50000) Mess_Integral_Gier = 50000; // begrenzen |
| 1217 | if(Mess_Integral_Gier <-50000) Mess_Integral_Gier =-50000; |
||
| 1051 | killagreg | 1218 | |
| 1219 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1 | ingob | 1220 | // Kompass |
| 1051 | killagreg | 1221 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1840 | holgerb | 1222 | if(KompassValue >= 0 && (EE_Parameter.GlobalConfig & CFG_KOMPASS_AKTIV)) |
| 1 | ingob | 1223 | { |
| 1839 | holgerb | 1224 | if(CalculateCompassTimer-- == 1) |
| 1225 | { |
||
| 1226 | int w,v,r,fehler,korrektur; // wird von der SPI-Routine auf 1 gesetzt |
||
| 1227 | CalculateCompassTimer = 13; // falls keine Navi-Daten |
||
| 1840 | holgerb | 1228 | // max. Korrekturwert schätzen |
| 1 | ingob | 1229 | w = abs(IntegralNick /512); // mit zunehmender Neigung den Einfluss drosseln |
| 1230 | v = abs(IntegralRoll /512); |
||
| 1231 | if(v > w) w = v; // grösste Neigung ermitteln |
||
| 1839 | holgerb | 1232 | korrektur = w / 4 + 1; |
| 1840 | holgerb | 1233 | // Kompassfehlerwert bestimmen |
| 1234 | fehler = ((540 + KompassValue - (ErsatzKompass/GIER_GRAD_FAKTOR)) % 360) - 180; |
||
| 1235 | // GIER_GRAD_FAKTOR ist ca. 1200 |
||
| 1662 | killagreg | 1236 | |
| 1840 | holgerb | 1237 | // Kompasswert einloggen |
| 1238 | if(KompassSignalSchlecht) KompassSignalSchlecht--; |
||
| 1239 | else |
||
| 1240 | if(w < 25) |
||
| 921 | hbuss | 1241 | { |
| 1242 | GierGyroFehler += fehler; |
||
| 1051 | killagreg | 1243 | if(NeueKompassRichtungMerken) |
| 1244 | { |
||
| 1839 | holgerb | 1245 | if(--NeueKompassRichtungMerken == 0) |
| 1246 | { |
||
| 1247 | ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
||
| 1248 | KompassSollWert = (ErsatzKompass/GIER_GRAD_FAKTOR); |
||
| 1249 | } |
||
| 921 | hbuss | 1250 | } |
| 1 | ingob | 1251 | } |
| 1840 | holgerb | 1252 | // Kompass fusionieren |
| 1839 | holgerb | 1253 | if(!KompassSignalSchlecht) ErsatzKompass += (fehler * KompassFusion) / korrektur; |
| 1254 | |||
| 1840 | holgerb | 1255 | // MK Gieren |
| 1839 | holgerb | 1256 | if(!NeueKompassRichtungMerken) |
| 1257 | { |
||
| 1840 | holgerb | 1258 | r = ((540 + (KompassSollWert - ErsatzKompass/GIER_GRAD_FAKTOR)) % 360) - 180; |
| 1259 | DebugOut.Analog[19] = r; |
||
| 1839 | holgerb | 1260 | v = r * (Parameter_KompassWirkung/2); // nach Kompass ausrichten |
| 1840 | holgerb | 1261 | // if(abs(r) > 20) v *= 2; // über 20° -> doppelt so schnell |
| 1262 | CompassGierSetpoint = v / 16; |
||
| 1263 | } |
||
| 1264 | else CompassGierSetpoint = 0; |
||
| 1839 | holgerb | 1265 | |
| 1266 | /* |
||
| 1840 | holgerb | 1267 | DebugOut.Analog[16] = fehler; |
| 1268 | DebugOut.Analog[17] = korrektur; |
||
| 1269 | */ |
||
| 1270 | DebugOut.Analog[25] = CompassGierSetpoint; |
||
| 1271 | DebugOut.Analog[18] = KompassFusion; |
||
| 1272 | |||
| 1273 | /* |
||
| 921 | hbuss | 1274 | w = (w * Parameter_KompassWirkung) / 32; // auf die Wirkung normieren |
| 1 | ingob | 1275 | w = Parameter_KompassWirkung - w; // Wirkung ggf drosseln |
| 921 | hbuss | 1276 | if(w >= 0) |
| 1 | ingob | 1277 | { |
| 1051 | killagreg | 1278 | if(!KompassSignalSchlecht) |
| 693 | hbuss | 1279 | { |
| 1051 | killagreg | 1280 | v = 64 + ((MaxStickNick + MaxStickRoll)) / 8; |
| 1839 | holgerb | 1281 | DebugOut.Analog[16] = korrektur; |
| 1837 | holgerb | 1282 | r = ((540 + (ErsatzKompass/GIER_GRAD_FAKTOR) - KompassSollWert) % 360) - 180; |
| 819 | hbuss | 1283 | v = (r * w) / v; // nach Kompass ausrichten |
| 1284 | w = 3 * Parameter_KompassWirkung; |
||
| 693 | hbuss | 1285 | if(v > w) v = w; // Begrenzen |
| 1051 | killagreg | 1286 | else |
| 693 | hbuss | 1287 | if(v < -w) v = -w; |
| 1839 | holgerb | 1288 | // Mess_Integral_Gier += v; |
| 1051 | killagreg | 1289 | } |
| 693 | hbuss | 1290 | if(KompassSignalSchlecht) KompassSignalSchlecht--; |
| 1051 | killagreg | 1291 | } |
| 921 | hbuss | 1292 | else KompassSignalSchlecht = 500; // so lange das Signal taub stellen --> ca. 1 sek |
| 1839 | holgerb | 1293 | */ |
| 1294 | } // CalculateCompassTimer |
||
| 1051 | killagreg | 1295 | } |
| 1840 | holgerb | 1296 | else CompassGierSetpoint = 0; |
| 1051 | killagreg | 1297 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1298 | // Drehgeschwindigkeit und -winkel zu einem Istwert zusammenfassen |
| 1051 | killagreg | 1299 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1216 | killagreg | 1300 | if(TrichterFlug) { SummeRoll = 0; SummeNick = 0;}; |
| 604 | hbuss | 1301 | |
| 1171 | hbuss | 1302 | if(!Looping_Nick) IntegralNickMalFaktor = (IntegralNick * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralNickMalFaktor = 0; |
| 1303 | if(!Looping_Roll) IntegralRollMalFaktor = (IntegralRoll * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralRollMalFaktor = 0; |
||
| 1153 | hbuss | 1304 | |
| 1167 | hbuss | 1305 | #define TRIM_MAX 200 |
| 1166 | hbuss | 1306 | if(TrimNick > TRIM_MAX) TrimNick = TRIM_MAX; else if(TrimNick <-TRIM_MAX) TrimNick =-TRIM_MAX; |
| 1307 | if(TrimRoll > TRIM_MAX) TrimRoll = TRIM_MAX; else if(TrimRoll <-TRIM_MAX) TrimRoll =-TRIM_MAX; |
||
| 1153 | hbuss | 1308 | |
| 1166 | hbuss | 1309 | MesswertNick = IntegralNickMalFaktor + (long)((long)MesswertNick * GyroFaktor + (long)TrimNick * 128L) / (256L / STICK_GAIN); |
| 1310 | MesswertRoll = IntegralRollMalFaktor + (long)((long)MesswertRoll * GyroFaktor + (long)TrimRoll * 128L) / (256L / STICK_GAIN); |
||
| 1211 | hbuss | 1311 | MesswertGier = (long)(MesswertGier * 2 * (long)GyroFaktorGier) / (256L / STICK_GAIN) + (long)(Integral_Gier * IntegralFaktorGier) / (2 * (44000 / STICK_GAIN)); |
| 1166 | hbuss | 1312 | |
| 1 | ingob | 1313 | // Maximalwerte abfangen |
| 1153 | hbuss | 1314 | // #define MAX_SENSOR (4096*STICK_GAIN) |
| 1685 | holgerb | 1315 | #define MAX_SENSOR (4096) |
| 1216 | killagreg | 1316 | if(MesswertNick > MAX_SENSOR) MesswertNick = MAX_SENSOR; |
| 1 | ingob | 1317 | if(MesswertNick < -MAX_SENSOR) MesswertNick = -MAX_SENSOR; |
| 1318 | if(MesswertRoll > MAX_SENSOR) MesswertRoll = MAX_SENSOR; |
||
| 1319 | if(MesswertRoll < -MAX_SENSOR) MesswertRoll = -MAX_SENSOR; |
||
| 1320 | if(MesswertGier > MAX_SENSOR) MesswertGier = MAX_SENSOR; |
||
| 1321 | if(MesswertGier < -MAX_SENSOR) MesswertGier = -MAX_SENSOR; |
||
| 1322 | |||
| 1051 | killagreg | 1323 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1324 | // Höhenregelung |
| 1325 | // Die Höhenregelung schwächt lediglich das Gas ab, erhöht es allerdings nicht |
||
| 1051 | killagreg | 1326 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1374 | hbuss | 1327 | if(UBat > BattLowVoltageWarning) GasMischanteil = ((unsigned int)GasMischanteil * BattLowVoltageWarning) / UBat; // Gas auf das aktuelle Spannungvieveau beziehen |
| 855 | hbuss | 1328 | GasMischanteil *= STICK_GAIN; |
| 1309 | hbuss | 1329 | // if height control is activated |
| 1322 | hbuss | 1330 | if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG) && !(Looping_Roll || Looping_Nick)) // Höhenregelung |
| 1309 | hbuss | 1331 | { |
| 1698 | holgerb | 1332 | #define HOVER_GAS_AVERAGE 16384L // 16384 * 2ms = 32s averaging |
| 1332 | hbuss | 1333 | #define HC_GAS_AVERAGE 4 // 4 * 2ms= 8ms averaging |
| 1638 | holgerb | 1334 | |
| 1335 | #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
||
| 1336 | #define OPA_OFFSET_STEP 15 |
||
| 1642 | killagreg | 1337 | #else |
| 1638 | holgerb | 1338 | #define OPA_OFFSET_STEP 10 |
| 1339 | #endif |
||
| 1697 | holgerb | 1340 | int HCGas, HeightDeviation = 0,GasReduction = 0; |
| 1309 | hbuss | 1341 | static int HeightTrimming = 0; // rate for change of height setpoint |
| 1342 | static int FilterHCGas = 0; |
||
| 1692 | holgerb | 1343 | static int StickGasHover = 120, HoverGasMin = 0, HoverGasMax = 1023; |
| 1587 | killagreg | 1344 | static unsigned long HoverGasFilter = 0; |
| 1322 | hbuss | 1345 | static unsigned char delay = 100, BaroAtUpperLimit = 0, BaroAtLowerLimit = 0; |
| 1320 | hbuss | 1346 | int CosAttitude; // for projection of hoover gas |
| 1330 | killagreg | 1347 | |
| 1309 | hbuss | 1348 | // get the current hooverpoint |
| 1587 | killagreg | 1349 | DebugOut.Analog[21] = HoverGas; |
| 1642 | killagreg | 1350 | |
| 1322 | hbuss | 1351 | // Expand the measurement |
| 1352 | // measurement of air pressure close to upper limit and no overflow in correction of the new OCR0A value occurs |
||
| 1353 | if(!BaroExpandActive) |
||
| 1354 | { |
||
| 1355 | if(MessLuftdruck > 920) |
||
| 1356 | { // increase offset |
||
| 1330 | killagreg | 1357 | if(OCR0A < (255 - OPA_OFFSET_STEP)) |
| 1322 | hbuss | 1358 | { |
| 1359 | ExpandBaro -= 1; |
||
| 1360 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // increase offset to shift ADC down |
||
| 1361 | beeptime = 300; |
||
| 1352 | hbuss | 1362 | BaroExpandActive = 350; |
| 1330 | killagreg | 1363 | } |
| 1364 | else |
||
| 1322 | hbuss | 1365 | { |
| 1366 | BaroAtLowerLimit = 1; |
||
| 1367 | } |
||
| 1368 | } |
||
| 1369 | // measurement of air pressure close to lower limit and |
||
| 1330 | killagreg | 1370 | else |
| 1322 | hbuss | 1371 | if(MessLuftdruck < 100) |
| 1372 | { // decrease offset |
||
| 1330 | killagreg | 1373 | if(OCR0A > OPA_OFFSET_STEP) |
| 1322 | hbuss | 1374 | { |
| 1375 | ExpandBaro += 1; |
||
| 1376 | OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // decrease offset to shift ADC up |
||
| 1377 | beeptime = 300; |
||
| 1352 | hbuss | 1378 | BaroExpandActive = 350; |
| 1330 | killagreg | 1379 | } |
| 1380 | else |
||
| 1322 | hbuss | 1381 | { |
| 1382 | BaroAtUpperLimit = 1; |
||
| 1383 | } |
||
| 1384 | } |
||
| 1330 | killagreg | 1385 | else |
| 1322 | hbuss | 1386 | { |
| 1387 | BaroAtUpperLimit = 0; |
||
| 1388 | BaroAtLowerLimit = 0; |
||
| 1389 | } |
||
| 1390 | } |
||
| 1391 | else // delay, because of expanding the Baro-Range |
||
| 1392 | { |
||
| 1393 | // now clear the D-values |
||
| 1394 | SummenHoehe = HoehenWert * SM_FILTER; |
||
| 1395 | VarioMeter = 0; |
||
| 1396 | BaroExpandActive--; |
||
| 1397 | } |
||
| 1328 | hbuss | 1398 | |
| 1399 | // if height control is activated by an rc channel |
||
| 1400 | if(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER) // Regler wird über Schalter gesteuert |
||
| 1401 | { // check if parameter is less than activation threshold |
||
| 1402 | if(Parameter_MaxHoehe < 50) // for 3 or 2-state switch height control is disabled in lowest position |
||
| 1403 | { //height control not active |
||
| 1404 | if(!delay--) |
||
| 1405 | { |
||
| 1406 | HoehenReglerAktiv = 0; // disable height control |
||
| 1407 | SollHoehe = HoehenWert; // update SetPoint with current reading |
||
| 1408 | delay = 1; |
||
| 1409 | } |
||
| 1410 | } |
||
| 1411 | else |
||
| 1412 | { //height control is activated |
||
| 1413 | HoehenReglerAktiv = 1; // enable height control |
||
| 1334 | killagreg | 1414 | delay = 200; |
| 1328 | hbuss | 1415 | } |
| 1051 | killagreg | 1416 | } |
| 1309 | hbuss | 1417 | else // no switchable height control |
| 1418 | { |
||
| 1419 | SollHoehe = ((int16_t) ExternHoehenValue + (int16_t) Parameter_MaxHoehe) * (int)EE_Parameter.Hoehe_Verstaerkung; |
||
| 1420 | HoehenReglerAktiv = 1; |
||
| 1051 | killagreg | 1421 | } |
| 1322 | hbuss | 1422 | |
| 1320 | hbuss | 1423 | // calculate cos of nick and roll angle used for projection of the vertical hoover gas |
| 1330 | killagreg | 1424 | tmp_int = (int)(IntegralNick/GIER_GRAD_FAKTOR); // nick angle in deg |
| 1425 | tmp_int2 = (int)(IntegralRoll/GIER_GRAD_FAKTOR); // roll angle in deg |
||
| 1426 | CosAttitude = (int16_t)ihypot(tmp_int, tmp_int2); // phytagoras gives effective attitude angle in deg |
||
| 1320 | hbuss | 1427 | LIMIT_MAX(CosAttitude, 60); // limit effective attitude angle |
| 1428 | CosAttitude = c_cos_8192(CosAttitude); // cos of actual attitude |
||
| 1591 | holgerb | 1429 | VarioCharacter = ' '; |
| 1765 | killagreg | 1430 | if(HoehenReglerAktiv && !(FC_StatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
| 1309 | hbuss | 1431 | { |
| 1330 | killagreg | 1432 | #define HEIGHT_CONTROL_STICKTHRESHOLD 15 |
| 1309 | hbuss | 1433 | // Holger original version |
| 1434 | // start of height control algorithm |
||
| 1435 | // the height control is only an attenuation of the actual gas stick. |
||
| 1436 | // I.e. it will work only if the gas stick is higher than the hover gas |
||
| 1437 | // and the hover height will be allways larger than height setpoint. |
||
| 1314 | killagreg | 1438 | if((EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) || !(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER)) // Regler wird über Schalter gesteuert) |
| 1439 | { // old version |
||
| 1309 | hbuss | 1440 | HCGas = GasMischanteil; // take current stick gas as neutral point for the height control |
| 1441 | HeightTrimming = 0; |
||
| 1773 | killagreg | 1442 | // set both flags to indicate no vario mode |
| 1443 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
||
| 1309 | hbuss | 1444 | } |
| 1314 | killagreg | 1445 | else |
| 1309 | hbuss | 1446 | { |
| 1447 | // alternative height control |
||
| 1448 | // PD-Control with respect to hoover point |
||
| 1449 | // the thrust loss out of horizontal attitude is compensated |
||
| 1450 | // the setpoint will be fine adjusted with the gas stick position |
||
| 1765 | killagreg | 1451 | if(FC_StatusFlags & FC_STATUS_FLY) // trim setpoint only when flying |
| 1309 | hbuss | 1452 | { // gas stick is above hoover point |
| 1587 | killagreg | 1453 | if(StickGas > (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtUpperLimit) |
| 1309 | hbuss | 1454 | { |
| 1767 | killagreg | 1455 | if(FC_StatusFlags & FC_STATUS_VARIO_TRIM_DOWN) |
| 1309 | hbuss | 1456 | { |
| 1767 | killagreg | 1457 | FC_StatusFlags &= ~FC_STATUS_VARIO_TRIM_DOWN; |
| 1309 | hbuss | 1458 | SollHoehe = HoehenWert; // update setpoint to current heigth |
| 1459 | } |
||
| 1767 | killagreg | 1460 | FC_StatusFlags |= FC_STATUS_VARIO_TRIM_UP; |
| 1587 | killagreg | 1461 | HeightTrimming += abs(StickGas - (StickGasHover + HEIGHT_CONTROL_STICKTHRESHOLD)); |
| 1591 | holgerb | 1462 | VarioCharacter = '+'; |
| 1309 | hbuss | 1463 | } // gas stick is below hoover point |
| 1587 | killagreg | 1464 | else if(StickGas < (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtLowerLimit ) |
| 1309 | hbuss | 1465 | { |
| 1767 | killagreg | 1466 | if(FC_StatusFlags & FC_STATUS_VARIO_TRIM_UP) |
| 1309 | hbuss | 1467 | { |
| 1767 | killagreg | 1468 | FC_StatusFlags &= ~FC_STATUS_VARIO_TRIM_UP; |
| 1309 | hbuss | 1469 | SollHoehe = HoehenWert; // update setpoint to current heigth |
| 1470 | } |
||
| 1767 | killagreg | 1471 | FC_StatusFlags |= FC_STATUS_VARIO_TRIM_DOWN; |
| 1587 | killagreg | 1472 | HeightTrimming -= abs(StickGas - (StickGasHover - HEIGHT_CONTROL_STICKTHRESHOLD)); |
| 1591 | holgerb | 1473 | VarioCharacter = '-'; |
| 1309 | hbuss | 1474 | } |
| 1587 | killagreg | 1475 | else // Gas Stick in Hover Range |
| 1309 | hbuss | 1476 | { |
| 1767 | killagreg | 1477 | if(FC_StatusFlags & (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN)) |
| 1309 | hbuss | 1478 | { |
| 1767 | killagreg | 1479 | FC_StatusFlags &= ~(FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
| 1309 | hbuss | 1480 | HeightTrimming = 0; |
| 1481 | SollHoehe = HoehenWert; // update setpoint to current height |
||
| 1482 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 500; |
||
| 1698 | holgerb | 1483 | if(!StartTrigger && HoehenWert > 50) |
| 1484 | { |
||
| 1485 | StartTrigger = 1; |
||
| 1765 | killagreg | 1486 | } |
| 1309 | hbuss | 1487 | } |
| 1591 | holgerb | 1488 | VarioCharacter = '='; |
| 1309 | hbuss | 1489 | } |
| 1490 | // Trim height set point |
||
| 1334 | killagreg | 1491 | if(abs(HeightTrimming) > 512) |
| 1309 | hbuss | 1492 | { |
| 1332 | hbuss | 1493 | SollHoehe += (HeightTrimming * EE_Parameter.Hoehe_Verstaerkung)/(5 * 512 / 2); // move setpoint |
| 1309 | hbuss | 1494 | HeightTrimming = 0; |
| 1587 | killagreg | 1495 | LIMIT_MIN_MAX(SollHoehe, (HoehenWert-1024), (HoehenWert+1024)); // max. 10m Unterschied |
| 1720 | holgerb | 1496 | if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 100; |
| 1320 | hbuss | 1497 | //update hoover gas stick value when setpoint is shifted |
| 1332 | hbuss | 1498 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
| 1499 | { |
||
| 1587 | killagreg | 1500 | StickGasHover = HoverGas/STICK_GAIN; //rescale back to stick value |
| 1501 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
||
| 1502 | if(StickGasHover < 70) StickGasHover = 70; |
||
| 1503 | else if(StickGasHover > 150) StickGasHover = 150; |
||
| 1332 | hbuss | 1504 | } |
| 1309 | hbuss | 1505 | } |
| 1352 | hbuss | 1506 | if(BaroExpandActive) SollHoehe = HoehenWert; // update setpoint to current altitude if Expanding is active |
| 1420 | killagreg | 1507 | } //if FCFlags & MKFCFLAG_FLY |
| 1330 | killagreg | 1508 | else |
| 1509 | { |
||
| 1322 | hbuss | 1510 | SollHoehe = HoehenWert - 400; |
| 1587 | killagreg | 1511 | if(EE_Parameter.Hoehe_StickNeutralPoint) StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
| 1512 | else StickGasHover = 120; |
||
| 1698 | holgerb | 1513 | HoverGas = GasMischanteil; |
| 1320 | hbuss | 1514 | } |
| 1590 | killagreg | 1515 | HCGas = HoverGas; // take hover gas (neutral point) |
| 1516 | } |
||
| 1314 | killagreg | 1517 | if(HoehenWert > SollHoehe || !(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT)) |
| 1283 | hbuss | 1518 | { |
| 1590 | killagreg | 1519 | // from this point the Heigth Control Algorithm is identical for both versions |
| 1520 | if(BaroExpandActive) // baro range expanding active |
||
| 1521 | { |
||
| 1522 | HCGas = HoverGas; // hover while expanding baro adc range |
||
| 1523 | HeightDeviation = 0; |
||
| 1524 | } // EOF // baro range expanding active |
||
| 1525 | else // valid data from air pressure sensor |
||
| 1526 | { |
||
| 1527 | // ------------------------- P-Part ---------------------------- |
||
| 1528 | tmp_long = (HoehenWert - SollHoehe); // positive when too high |
||
| 1529 | LIMIT_MIN_MAX(tmp_long, -32767L, 32767L); // avoid overflov when casting to int16_t |
||
| 1530 | HeightDeviation = (int)(tmp_long); // positive when too high |
||
| 1695 | holgerb | 1531 | tmp_long = (tmp_long * (long)Parameter_Hoehe_P) / 32L; // p-part |
| 1698 | holgerb | 1532 | LIMIT_MIN_MAX(tmp_long, -127 * STICK_GAIN, 256 * STICK_GAIN); // more than the full range makes no sense |
| 1533 | GasReduction = tmp_long; |
||
| 1590 | killagreg | 1534 | // ------------------------- D-Part 1: Vario Meter ---------------------------- |
| 1535 | tmp_int = VarioMeter / 8; |
||
| 1765 | killagreg | 1536 | LIMIT_MIN_MAX(tmp_int, -127, 128); |
| 1705 | holgerb | 1537 | tmp_int = (tmp_int * (long)Parameter_Luftdruck_D) / 4L; // scale to d-gain parameter |
| 1538 | LIMIT_MIN_MAX(tmp_int,-64 * STICK_GAIN, 64 * STICK_GAIN); |
||
| 1767 | killagreg | 1539 | if(FC_StatusFlags & (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN)) tmp_int /= 4; // reduce d-part while trimming setpoint |
| 1765 | killagreg | 1540 | else |
| 1722 | holgerb | 1541 | if(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) tmp_int /= 8; // reduce d-part in "Deckel" mode |
| 1698 | holgerb | 1542 | GasReduction += tmp_int; |
| 1590 | killagreg | 1543 | } // EOF no baro range expanding |
| 1309 | hbuss | 1544 | // ------------------------ D-Part 2: ACC-Z Integral ------------------------ |
| 1698 | holgerb | 1545 | if(Parameter_Hoehe_ACC_Wirkung) |
| 1546 | { |
||
| 1547 | tmp_long = ((Mess_Integral_Hoch / 128L) * (int32_t) Parameter_Hoehe_ACC_Wirkung) / (128L / STICK_GAIN); |
||
| 1548 | LIMIT_MIN_MAX(tmp_long, -32 * STICK_GAIN, 64 * STICK_GAIN); |
||
| 1549 | GasReduction += tmp_long; |
||
| 1765 | killagreg | 1550 | } |
| 1587 | killagreg | 1551 | // ------------------------ D-Part 3: GpsZ ---------------------------------- |
| 1588 | killagreg | 1552 | tmp_int = (Parameter_Hoehe_GPS_Z * (int)FromNaviCtrl_Value.GpsZ)/128L; |
| 1553 | LIMIT_MIN_MAX(tmp_int, -32 * STICK_GAIN, 64 * STICK_GAIN); |
||
| 1698 | holgerb | 1554 | GasReduction += tmp_int; |
| 1701 | holgerb | 1555 | GasReduction = (long)((long)GasReduction * HoverGas) / 512; // scale to the gas value |
| 1556 | // ------------------------ ---------------------------------- |
||
| 1557 | HCGas -= GasReduction; |
||
| 1309 | hbuss | 1558 | // limit deviation from hoover point within the target region |
| 1692 | holgerb | 1559 | if(!HeightTrimming && HoverGas > 0) // height setpoint is not changed and hoover gas not zero |
| 1309 | hbuss | 1560 | { |
| 1765 | killagreg | 1561 | unsigned int tmp; |
| 1705 | holgerb | 1562 | tmp = abs(HeightDeviation); |
| 1563 | if(tmp <= 60) |
||
| 1564 | { |
||
| 1565 | LIMIT_MIN_MAX(HCGas, HoverGasMin, HoverGasMax); // limit gas around the hoover point |
||
| 1566 | } |
||
| 1567 | else |
||
| 1765 | killagreg | 1568 | { |
| 1705 | holgerb | 1569 | tmp = (tmp - 60) / 32; |
| 1692 | holgerb | 1570 | if(tmp > 15) tmp = 15; |
| 1705 | holgerb | 1571 | if(HeightDeviation > 0) |
| 1693 | holgerb | 1572 | { |
| 1705 | holgerb | 1573 | tmp = (HoverGasMin * (16 - tmp)) / 16; |
| 1574 | LIMIT_MIN_MAX(HCGas, tmp, HoverGasMax); // limit gas around the hoover point |
||
| 1693 | holgerb | 1575 | } |
| 1705 | holgerb | 1576 | else |
| 1577 | { |
||
| 1578 | tmp = (HoverGasMax * (tmp + 16)) / 16; |
||
| 1579 | LIMIT_MIN_MAX(HCGas, HoverGasMin, tmp); // limit gas around the hoover point |
||
| 1580 | } |
||
| 1581 | } |
||
| 1309 | hbuss | 1582 | } |
| 1322 | hbuss | 1583 | // strech control output by inverse attitude projection 1/cos |
| 1584 | // + 1/cos(angle) ++++++++++++++++++++++++++ |
||
| 1330 | killagreg | 1585 | tmp_long2 = (int32_t)HCGas; |
| 1586 | tmp_long2 *= 8192L; |
||
| 1587 | tmp_long2 /= CosAttitude; |
||
| 1588 | HCGas = (int16_t)tmp_long2; |
||
| 1309 | hbuss | 1589 | // update height control gas averaging |
| 1590 | FilterHCGas = (FilterHCGas * (HC_GAS_AVERAGE - 1) + HCGas) / HC_GAS_AVERAGE; |
||
| 1591 | // limit height control gas pd-control output |
||
| 1592 | LIMIT_MIN_MAX(FilterHCGas, EE_Parameter.Hoehe_MinGas * STICK_GAIN, (MAX_GAS - 20) * STICK_GAIN); |
||
| 1593 | // set GasMischanteil to HeightControlGasFilter |
||
| 1314 | killagreg | 1594 | if(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) |
| 1587 | killagreg | 1595 | { // old version |
| 1596 | LIMIT_MAX(FilterHCGas, GasMischanteil); // nicht mehr als Gas |
||
| 1719 | holgerb | 1597 | GasMischanteil = FilterHCGas; |
| 1765 | killagreg | 1598 | } |
| 1719 | holgerb | 1599 | else GasMischanteil = FilterHCGas + (GasMischanteil - HoverGas) / 4; // only in Vario-Mode |
| 1314 | killagreg | 1600 | } |
| 1309 | hbuss | 1601 | }// EOF height control active |
| 1320 | hbuss | 1602 | else // HC not active |
| 1603 | { |
||
| 1604 | //update hoover gas stick value when HC is not active |
||
| 1587 | killagreg | 1605 | if(!EE_Parameter.Hoehe_StickNeutralPoint) |
| 1606 | { |
||
| 1607 | StickGasHover = HoverGas/STICK_GAIN; // rescale back to stick value |
||
| 1608 | StickGasHover = (StickGasHover * UBat) / BattLowVoltageWarning; |
||
| 1322 | hbuss | 1609 | } |
| 1587 | killagreg | 1610 | else StickGasHover = EE_Parameter.Hoehe_StickNeutralPoint; |
| 1611 | LIMIT_MIN_MAX(StickGasHover, 70, 150); // reserve some range for trim up and down |
||
| 1328 | hbuss | 1612 | FilterHCGas = GasMischanteil; |
| 1773 | killagreg | 1613 | // set both flags to indicate no vario mode |
| 1614 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
||
| 1330 | killagreg | 1615 | } |
| 1283 | hbuss | 1616 | |
| 1587 | killagreg | 1617 | // Hover gas estimation by averaging gas control output on small z-velocities |
| 1309 | hbuss | 1618 | // this is done only if height contol option is selected in global config and aircraft is flying |
| 1765 | killagreg | 1619 | if((FC_StatusFlags & FC_STATUS_FLY))// && !(FC_SatusFlags & FC_STATUS_EMERGENCY_LANDING)) |
| 1309 | hbuss | 1620 | { |
| 1698 | holgerb | 1621 | if(HoverGasFilter == 0 || StartTrigger == 1) HoverGasFilter = HOVER_GAS_AVERAGE * (unsigned long)(GasMischanteil); // init estimation |
| 1622 | if(StartTrigger == 1) StartTrigger = 2; |
||
| 1330 | killagreg | 1623 | tmp_long2 = (int32_t)GasMischanteil; // take current thrust |
| 1624 | tmp_long2 *= CosAttitude; // apply attitude projection |
||
| 1625 | tmp_long2 /= 8192; |
||
| 1309 | hbuss | 1626 | // average vertical projected thrust |
| 1698 | holgerb | 1627 | if(modell_fliegt < 4000) // the first 8 seconds |
| 1628 | { // reduce the time constant of averaging by factor of 4 to get much faster a stable value |
||
| 1629 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/16L); |
||
| 1630 | HoverGasFilter += 16L * tmp_long2; |
||
| 1309 | hbuss | 1631 | } |
| 1698 | holgerb | 1632 | if(modell_fliegt < 8000) // the first 16 seconds |
| 1633 | { // reduce the time constant of averaging by factor of 2 to get much faster a stable value |
||
| 1590 | killagreg | 1634 | HoverGasFilter -= HoverGasFilter/(HOVER_GAS_AVERAGE/4L); |
| 1587 | killagreg | 1635 | HoverGasFilter += 4L * tmp_long2; |
| 1309 | hbuss | 1636 | } |
| 1698 | holgerb | 1637 | else //later |
| 1638 | if(abs(VarioMeter) < 100) // only on small vertical speed |
||
| 1309 | hbuss | 1639 | { |
| 1590 | killagreg | 1640 | HoverGasFilter -= HoverGasFilter/HOVER_GAS_AVERAGE; |
| 1587 | killagreg | 1641 | HoverGasFilter += tmp_long2; |
| 1309 | hbuss | 1642 | } |
| 1590 | killagreg | 1643 | HoverGas = (int16_t)(HoverGasFilter/HOVER_GAS_AVERAGE); |
| 1309 | hbuss | 1644 | if(EE_Parameter.Hoehe_HoverBand) |
| 1645 | { |
||
| 1646 | int16_t band; |
||
| 1587 | killagreg | 1647 | band = HoverGas / EE_Parameter.Hoehe_HoverBand; // the higher the parameter the smaller the range |
| 1648 | HoverGasMin = HoverGas - band; |
||
| 1649 | HoverGasMax = HoverGas + band; |
||
| 1309 | hbuss | 1650 | } |
| 1651 | else |
||
| 1652 | { // no limit |
||
| 1587 | killagreg | 1653 | HoverGasMin = 0; |
| 1654 | HoverGasMax = 1023; |
||
| 1309 | hbuss | 1655 | } |
| 1765 | killagreg | 1656 | } |
| 1657 | else |
||
| 1698 | holgerb | 1658 | { |
| 1659 | StartTrigger = 0; |
||
| 1660 | HoverGasFilter = 0; |
||
| 1661 | HoverGas = 0; |
||
| 1765 | killagreg | 1662 | } |
| 1309 | hbuss | 1663 | }// EOF ParamSet.GlobalConfig & CFG_HEIGHT_CONTROL |
| 1773 | killagreg | 1664 | else |
| 1665 | { |
||
| 1666 | // set undefined state to indicate vario off |
||
| 1667 | FC_StatusFlags |= (FC_STATUS_VARIO_TRIM_UP|FC_STATUS_VARIO_TRIM_DOWN); |
||
| 1668 | } // EOF no height control |
||
| 1669 | |||
| 1309 | hbuss | 1670 | // limit gas to parameter setting |
| 1320 | hbuss | 1671 | LIMIT_MIN(GasMischanteil, (MIN_GAS + 10) * STICK_GAIN); |
| 855 | hbuss | 1672 | if(GasMischanteil > (MAX_GAS - 20) * STICK_GAIN) GasMischanteil = (MAX_GAS - 20) * STICK_GAIN; |
| 1111 | hbuss | 1673 | |
| 1051 | killagreg | 1674 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1320 | hbuss | 1675 | // all BL-Ctrl connected? |
| 1676 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1675 | holgerb | 1677 | if(MissingMotor || Capacity.MinOfMaxPWM != 255) |
| 1320 | hbuss | 1678 | if(modell_fliegt > 1 && modell_fliegt < 50 && GasMischanteil > 0) |
| 1679 | { |
||
| 1680 | modell_fliegt = 1; |
||
| 1675 | holgerb | 1681 | GasMischanteil = (MIN_GAS + 10) * STICK_GAIN; |
| 1320 | hbuss | 1682 | } |
| 1683 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1 | ingob | 1684 | // + Mischer und PI-Regler |
| 1051 | killagreg | 1685 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 173 | holgerb | 1686 | DebugOut.Analog[7] = GasMischanteil; |
| 1051 | killagreg | 1687 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1688 | // Gier-Anteil |
| 1051 | killagreg | 1689 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 855 | hbuss | 1690 | GierMischanteil = MesswertGier - sollGier * STICK_GAIN; // Regler für Gier |
| 1691 | #define MIN_GIERGAS (40*STICK_GAIN) // unter diesem Gaswert trotzdem Gieren |
||
| 693 | hbuss | 1692 | if(GasMischanteil > MIN_GIERGAS) |
| 1693 | { |
||
| 1051 | killagreg | 1694 | if(GierMischanteil > (GasMischanteil / 2)) GierMischanteil = GasMischanteil / 2; |
| 1695 | if(GierMischanteil < -(GasMischanteil / 2)) GierMischanteil = -(GasMischanteil / 2); |
||
| 693 | hbuss | 1696 | } |
| 1051 | killagreg | 1697 | else |
| 693 | hbuss | 1698 | { |
| 1051 | killagreg | 1699 | if(GierMischanteil > (MIN_GIERGAS / 2)) GierMischanteil = MIN_GIERGAS / 2; |
| 1700 | if(GierMischanteil < -(MIN_GIERGAS / 2)) GierMischanteil = -(MIN_GIERGAS / 2); |
||
| 693 | hbuss | 1701 | } |
| 855 | hbuss | 1702 | tmp_int = MAX_GAS*STICK_GAIN; |
| 1051 | killagreg | 1703 | if(GierMischanteil > ((tmp_int - GasMischanteil))) GierMischanteil = ((tmp_int - GasMischanteil)); |
| 855 | hbuss | 1704 | if(GierMischanteil < -((tmp_int - GasMischanteil))) GierMischanteil = -((tmp_int - GasMischanteil)); |
| 513 | hbuss | 1705 | |
| 1051 | killagreg | 1706 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1 | ingob | 1707 | // Nick-Achse |
| 1051 | killagreg | 1708 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 723 | hbuss | 1709 | DiffNick = MesswertNick - StickNick; // Differenz bestimmen |
| 1153 | hbuss | 1710 | if(IntegralFaktor) SummeNick += IntegralNickMalFaktor - StickNick; // I-Anteil bei Winkelregelung |
| 1051 | killagreg | 1711 | else SummeNick += DiffNick; // I-Anteil bei HH |
| 855 | hbuss | 1712 | if(SummeNick > (STICK_GAIN * 16000L)) SummeNick = (STICK_GAIN * 16000L); |
| 1713 | if(SummeNick < -(16000L * STICK_GAIN)) SummeNick = -(16000L * STICK_GAIN); |
||
| 1791 | holgerb | 1714 | |
| 1715 | if(EE_Parameter.Gyro_Stability <= 8) pd_ergebnis_nick = (EE_Parameter.Gyro_Stability * DiffNick) / 8; // PI-Regler für Nick |
||
| 1716 | else pd_ergebnis_nick = ((EE_Parameter.Gyro_Stability / 2) * DiffNick) / 4; // Überlauf verhindern |
||
| 1717 | pd_ergebnis_nick += SummeNick / Ki; |
||
| 1718 | |||
| 1676 | holgerb | 1719 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
| 1153 | hbuss | 1720 | if(pd_ergebnis_nick > tmp_int) pd_ergebnis_nick = tmp_int; |
| 1721 | if(pd_ergebnis_nick < -tmp_int) pd_ergebnis_nick = -tmp_int; |
||
| 173 | holgerb | 1722 | |
| 1153 | hbuss | 1723 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1724 | // Roll-Achse |
||
| 1725 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1726 | DiffRoll = MesswertRoll - StickRoll; // Differenz bestimmen |
||
| 1727 | if(IntegralFaktor) SummeRoll += IntegralRollMalFaktor - StickRoll;// I-Anteil bei Winkelregelung |
||
| 1728 | else SummeRoll += DiffRoll; // I-Anteil bei HH |
||
| 1729 | if(SummeRoll > (STICK_GAIN * 16000L)) SummeRoll = (STICK_GAIN * 16000L); |
||
| 1730 | if(SummeRoll < -(16000L * STICK_GAIN)) SummeRoll = -(16000L * STICK_GAIN); |
||
| 1791 | holgerb | 1731 | |
| 1732 | if(EE_Parameter.Gyro_Stability <= 8) pd_ergebnis_roll = (EE_Parameter.Gyro_Stability * DiffRoll) / 8; // PI-Regler für Roll |
||
| 1733 | else pd_ergebnis_roll = ((EE_Parameter.Gyro_Stability / 2) * DiffRoll) / 4; // Überlauf verhindern |
||
| 1734 | pd_ergebnis_roll += SummeRoll / Ki; |
||
| 1735 | |||
| 1676 | holgerb | 1736 | tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
| 1153 | hbuss | 1737 | if(pd_ergebnis_roll > tmp_int) pd_ergebnis_roll = tmp_int; |
| 1738 | if(pd_ergebnis_roll < -tmp_int) pd_ergebnis_roll = -tmp_int; |
||
| 1739 | |||
| 1740 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
||
| 1209 | hbuss | 1741 | // Universal Mixer |
| 1155 | hbuss | 1742 | // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| 1642 | killagreg | 1743 | for(i=0; i<MAX_MOTORS; i++) |
| 1744 | { |
||
| 1745 | signed int tmp_int; |
||
| 1746 | if(Mixer.Motor[i][0] > 0) |
||
| 1747 | { |
||
| 1652 | holgerb | 1748 | // Gas |
| 1676 | holgerb | 1749 | if(Mixer.Motor[i][0] == 64) tmp_int = GasMischanteil; else tmp_int = ((long)GasMischanteil * Mixer.Motor[i][0]) / 64L; |
| 1652 | holgerb | 1750 | // Nick |
| 1751 | if(Mixer.Motor[i][1] == 64) tmp_int += pd_ergebnis_nick; |
||
| 1752 | else if(Mixer.Motor[i][1] == -64) tmp_int -= pd_ergebnis_nick; |
||
| 1753 | else tmp_int += ((long)pd_ergebnis_nick * Mixer.Motor[i][1]) / 64L; |
||
| 1754 | // Roll |
||
| 1755 | if(Mixer.Motor[i][2] == 64) tmp_int += pd_ergebnis_roll; |
||
| 1756 | else if(Mixer.Motor[i][2] == -64) tmp_int -= pd_ergebnis_roll; |
||
| 1757 | else tmp_int += ((long)pd_ergebnis_roll * Mixer.Motor[i][2]) / 64L; |
||
| 1758 | // Gier |
||
| 1676 | holgerb | 1759 | if(Mixer.Motor[i][3] == 64) tmp_int += GierMischanteil; |
| 1760 | else if(Mixer.Motor[i][3] == -64) tmp_int -= GierMischanteil; |
||
| 1761 | else tmp_int += ((long)GierMischanteil * Mixer.Motor[i][3]) / 64L; |
||
| 1675 | holgerb | 1762 | |
| 1680 | holgerb | 1763 | if(tmp_int > tmp_motorwert[i]) tmp_int = (tmp_motorwert[i] + tmp_int) / 2; // MotorSmoothing |
| 1764 | else tmp_int = 2 * tmp_int - tmp_motorwert[i]; // MotorSmoothing |
||
| 1693 | holgerb | 1765 | |
| 1760 | holgerb | 1766 | LIMIT_MIN_MAX(tmp_int,(int) MIN_GAS * 4,(int) MAX_GAS * 4); |
| 1676 | holgerb | 1767 | Motor[i].SetPoint = tmp_int / 4; |
| 1677 | killagreg | 1768 | Motor[i].SetPointLowerBits = (tmp_int % 4)<<1; // (3 bits total) |
| 1652 | holgerb | 1769 | tmp_motorwert[i] = tmp_int; |
| 1642 | killagreg | 1770 | } |
| 1771 | else |
||
| 1772 | { |
||
| 1773 | Motor[i].SetPoint = 0; |
||
| 1774 | Motor[i].SetPointLowerBits = 0; |
||
| 1775 | } |
||
| 1776 | } |
||
| 1111 | hbuss | 1777 | } |