| 0,0 → 1,1672 |
|---|
| /*####################################################################################### |
| Flight Control |
| #######################################################################################*/ |
| // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // + Copyright (c) Holger Buss, Ingo Busker |
| // + Nur für den privaten Gebrauch / NON-COMMERCIAL USE ONLY |
| // + www.MikroKopter.com |
| // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // + Es gilt für das gesamte Projekt (Hardware, Software, Binärfiles, Sourcecode und Dokumentation), |
| // + dass eine Nutzung (auch auszugsweise) nur für den privaten (nicht-kommerziellen) Gebrauch zulässig ist. |
| // + Sollten direkte oder indirekte kommerzielle Absichten verfolgt werden, ist mit uns (info@mikrokopter.de) Kontakt |
| // + bzgl. der Nutzungsbedingungen aufzunehmen. |
| // + Eine kommerzielle Nutzung ist z.B.Verkauf von MikroKoptern, Bestückung und Verkauf von Platinen oder Bausätzen, |
| // + Verkauf von Luftbildaufnahmen, usw. |
| // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // + Werden Teile des Quellcodes (mit oder ohne Modifikation) weiterverwendet oder veröffentlicht, |
| // + unterliegen sie auch diesen Nutzungsbedingungen und diese Nutzungsbedingungen incl. Copyright müssen dann beiliegen |
| // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // + Sollte die Software (auch auszugesweise) oder sonstige Informationen des MikroKopter-Projekts |
| // + auf anderen Webseiten oder sonstigen Medien veröffentlicht werden, muss unsere Webseite "http://www.mikrokopter.de" |
| // + eindeutig als Ursprung verlinkt werden |
| // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // + Keine Gewähr auf Fehlerfreiheit, Vollständigkeit oder Funktion |
| // + Benutzung auf eigene Gefahr |
| // + Wir übernehmen keinerlei Haftung für direkte oder indirekte Personen- oder Sachschäden |
| // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // + Die Portierung oder Nutzung der Software (oder Teile davon) auf andere Systeme (ausser der Hardware von www.mikrokopter.de) ist nur |
| // + mit unserer Zustimmung zulässig |
| // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // + Die Funktion printf_P() unterliegt ihrer eigenen Lizenz und ist hiervon nicht betroffen |
| // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // + Redistributions of source code (with or without modifications) must retain the above copyright notice, |
| // + this list of conditions and the following disclaimer. |
| // + * Neither the name of the copyright holders nor the names of contributors may be used to endorse or promote products derived |
| // + from this software without specific prior written permission. |
| // + * The use of this project (hardware, software, binary files, sources and documentation) is only permittet |
| // + for non-commercial use (directly or indirectly) |
| // + Commercial use (for excample: selling of MikroKopters, selling of PCBs, assembly, ...) is only permitted |
| // + with our written permission |
| // + * If sources or documentations are redistributet on other webpages, out webpage (http://www.MikroKopter.de) must be |
| // + clearly linked as origin |
| // + * porting the sources to other systems or using the software on other systems (except hardware from www.mikrokopter.de) is not allowed |
| // + THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" |
| // + AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE |
| // + IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE |
| // + ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER OR CONTRIBUTORS BE |
| // + LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR |
| // + CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF |
| // + SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS |
| // + INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN |
| // + CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) |
| // + ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
| // + POSSIBILITY OF SUCH DAMAGE. |
| // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| |
| #include "main.h" |
| #include "eeprom.c" |
| #include "mymath.h" |
| #include "isqrt.h" |
| |
| unsigned char h,m,s; |
| unsigned int BaroExpandActive = 0; |
| volatile unsigned int I2CTimeout = 100; |
| int MesswertNick,MesswertRoll,MesswertGier,MesswertGierBias, RohMesswertNick,RohMesswertRoll; |
| int TrimNick, TrimRoll; |
| int AdNeutralGierBias; |
| int AdNeutralNick = 0,AdNeutralRoll = 0,AdNeutralGier = 0,StartNeutralRoll = 0,StartNeutralNick = 0; |
| int Mittelwert_AccNick, Mittelwert_AccRoll,Mittelwert_AccHoch, NeutralAccX=0, NeutralAccY=0; |
| int NaviAccNick, NaviAccRoll,NaviCntAcc = 0; |
| volatile float NeutralAccZ = 0; |
| unsigned char CosinusNickWinkel = 0, CosinusRollWinkel = 0; |
| long IntegralNick = 0,IntegralNick2 = 0; |
| long IntegralRoll = 0,IntegralRoll2 = 0; |
| long IntegralAccNick = 0,IntegralAccRoll = 0,IntegralAccZ = 0; |
| long Integral_Gier = 0; |
| long Mess_IntegralNick = 0,Mess_IntegralNick2 = 0; |
| long Mess_IntegralRoll = 0,Mess_IntegralRoll2 = 0; |
| long Mess_Integral_Gier = 0,Mess_Integral_Gier2 = 0; |
| long MittelIntegralNick,MittelIntegralRoll,MittelIntegralNick2,MittelIntegralRoll2; |
| volatile long Mess_Integral_Hoch = 0; |
| int KompassValue = 0; |
| int KompassStartwert = 0; |
| int KompassEinschaltStartwert = 0; |
| int KompassRichtung = 0; |
| unsigned int KompassSignalSchlecht = 500; |
| unsigned char MAX_GAS,MIN_GAS; |
| unsigned char HoehenReglerAktiv = 0; |
| unsigned char TrichterFlug = 0; |
| long Umschlag180Nick = 250000L, Umschlag180Roll = 250000L; |
| long ErsatzKompass; |
| int ErsatzKompassInGrad; // Kompasswert in Grad |
| int GierGyroFehler = 0; |
| char GyroFaktor,GyroFaktorGier; |
| char IntegralFaktor,IntegralFaktorGier; |
| int DiffNick,DiffRoll; |
| int Poti1 = 0, Poti2 = 0, Poti3 = 0, Poti4 = 0; |
| volatile unsigned char SenderOkay = 0; |
| volatile unsigned char SenderRSSI = 0; |
| int StickNick = 0,StickRoll = 0,StickGier = 0,StickGas = 0; |
| char MotorenEin = 0; |
| long HoehenWert = 0; |
| long SollHoehe = 0; |
| int LageKorrekturRoll = 0,LageKorrekturNick = 0; |
| //float Ki = FAKTOR_I; |
| int Ki = 10300 / 33; |
| unsigned char Looping_Nick = 0,Looping_Roll = 0; |
| unsigned char Looping_Links = 0, Looping_Rechts = 0, Looping_Unten = 0, Looping_Oben = 0; |
| |
| unsigned char Parameter_Luftdruck_D = 48; // Wert : 0-250 |
| unsigned char Parameter_MaxHoehe = 251; // Wert : 0-250 |
| unsigned char Parameter_Hoehe_P = 16; // Wert : 0-32 |
| unsigned char Parameter_Hoehe_ACC_Wirkung = 58; // Wert : 0-250 |
| unsigned char Parameter_KompassWirkung = 64; // Wert : 0-250 |
| unsigned char Parameter_Hoehe_GPS_Z = 64; // Wert : 0-250 |
| unsigned char Parameter_Gyro_D = 8; // Wert : 0-250 |
| unsigned char Parameter_Gyro_P = 150; // Wert : 10-250 |
| unsigned char Parameter_Gyro_I = 150; // Wert : 0-250 |
| unsigned char Parameter_Gyro_Gier_P = 150; // Wert : 10-250 |
| unsigned char Parameter_Gyro_Gier_I = 150; // Wert : 10-250 |
| unsigned char Parameter_Gier_P = 2; // Wert : 1-20 |
| unsigned char Parameter_I_Faktor = 10; // Wert : 1-20 |
| unsigned char Parameter_UserParam1 = 0; |
| unsigned char Parameter_UserParam2 = 0; |
| unsigned char Parameter_UserParam3 = 0; |
| unsigned char Parameter_UserParam4 = 0; |
| unsigned char Parameter_UserParam5 = 0; |
| unsigned char Parameter_UserParam6 = 0; |
| unsigned char Parameter_UserParam7 = 0; |
| unsigned char Parameter_UserParam8 = 0; |
| unsigned char Parameter_ServoNickControl = 100; |
| unsigned char Parameter_ServoRollControl = 100; |
| unsigned char Parameter_LoopGasLimit = 70; |
| unsigned char Parameter_AchsKopplung1 = 90; |
| unsigned char Parameter_AchsKopplung2 = 65; |
| unsigned char Parameter_CouplingYawCorrection = 64; |
| //unsigned char Parameter_AchsGegenKopplung1 = 0; |
| unsigned char Parameter_DynamicStability = 100; |
| unsigned char Parameter_J16Bitmask; // for the J16 Output |
| unsigned char Parameter_J16Timing; // for the J16 Output |
| unsigned char Parameter_J17Bitmask; // for the J17 Output |
| unsigned char Parameter_J17Timing; // for the J17 Output |
| unsigned char Parameter_NaviGpsModeControl; // Parameters for the Naviboard |
| unsigned char Parameter_NaviGpsGain; |
| unsigned char Parameter_NaviGpsP; |
| unsigned char Parameter_NaviGpsI; |
| unsigned char Parameter_NaviGpsD; |
| unsigned char Parameter_NaviGpsACC; |
| unsigned char Parameter_NaviOperatingRadius; |
| unsigned char Parameter_NaviWindCorrection; |
| unsigned char Parameter_NaviSpeedCompensation; |
| unsigned char Parameter_ExternalControl; |
| struct mk_param_struct EE_Parameter; |
| signed int ExternStickNick = 0,ExternStickRoll = 0,ExternStickGier = 0, ExternHoehenValue = -20; |
| int MaxStickNick = 0,MaxStickRoll = 0; |
| unsigned int modell_fliegt = 0; |
| volatile unsigned char MikroKopterFlags = 0; |
| long GIER_GRAD_FAKTOR = 1291; |
| signed int KopplungsteilNickRoll,KopplungsteilRollNick; |
| unsigned char RequiredMotors = 4; |
| unsigned char Motor[MAX_MOTORS]; |
| signed int tmp_motorwert[MAX_MOTORS]; |
| unsigned char LoadHandler = 0; |
| #define LIMIT_MIN(value, min) {if(value < min) value = min;} |
| #define LIMIT_MAX(value, max) {if(value > max) value = max;} |
| #define LIMIT_MIN_MAX(value, min, max) {if(value < min) value = min; else if(value > max) value = max;} |
| |
| int MotorSmoothing(int neu, int alt) |
| { |
| int motor; |
| if(neu > alt) motor = (1*(int)alt + neu) / 2; |
| else motor = neu - (alt - neu)*1; |
| //if(Poti2 < 20) return(neu); |
| return(motor); |
| } |
| |
| void Piep(unsigned char Anzahl, unsigned int dauer) |
| { |
| if(MotorenEin) return; //auf keinen Fall im Flug! |
| while(Anzahl--) |
| { |
| beeptime = dauer; |
| while(beeptime); |
| Delay_ms(dauer * 2); |
| } |
| } |
| |
| //############################################################################ |
| // Nullwerte ermitteln |
| void SetNeutral(void) |
| //############################################################################ |
| { |
| unsigned char i; |
| unsigned int gier_neutral=0, nick_neutral=0, roll_neutral=0; |
| HEF4017R_ON; |
| NeutralAccX = 0; |
| NeutralAccY = 0; |
| NeutralAccZ = 0; |
| AdNeutralNick = 0; |
| AdNeutralRoll = 0; |
| AdNeutralGier = 0; |
| AdNeutralGierBias = 0; |
| Parameter_AchsKopplung1 = 0; |
| Parameter_AchsKopplung2 = 0; |
| ExpandBaro = 0; |
| CalibrierMittelwert(); |
| Delay_ms_Mess(100); |
| CalibrierMittelwert(); |
| if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
| { |
| if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
| } |
| #define NEUTRAL_FILTER 32 |
| for(i=0; i<NEUTRAL_FILTER; i++) |
| { |
| Delay_ms_Mess(10); |
| gier_neutral += AdWertGier; |
| nick_neutral += AdWertNick; |
| roll_neutral += AdWertRoll; |
| } |
| AdNeutralNick= (nick_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
| AdNeutralRoll= (roll_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER / 8); |
| AdNeutralGier= (gier_neutral+NEUTRAL_FILTER/2) / (NEUTRAL_FILTER); |
| AdNeutralGierBias = AdNeutralGier; |
| StartNeutralRoll = AdNeutralRoll; |
| StartNeutralNick = AdNeutralNick; |
| if(eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_NICK]) > 4) |
| { |
| NeutralAccY = abs(Mittelwert_AccRoll) / (2*ACC_AMPLIFY); |
| NeutralAccX = abs(Mittelwert_AccNick) / (2*ACC_AMPLIFY); |
| NeutralAccZ = Aktuell_az; |
| } |
| else |
| { |
| NeutralAccX = (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_NICK]) * 256 + (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_NICK+1]); |
| NeutralAccY = (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL]) * 256 + (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL+1]); |
| NeutralAccZ = (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_Z]) * 256 + (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_Z+1]); |
| } |
| |
| MesswertNick = 0; |
| MesswertRoll = 0; |
| MesswertGier = 0; |
| Delay_ms_Mess(100); |
| Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
| Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
| IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
| IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
| Mess_IntegralNick2 = IntegralNick; |
| Mess_IntegralRoll2 = IntegralRoll; |
| Mess_Integral_Gier = 0; |
| StartLuftdruck = Luftdruck; |
| VarioMeter = 0; |
| Mess_Integral_Hoch = 0; |
| KompassStartwert = KompassValue; |
| KompassEinschaltStartwert = KompassValue; |
| GPS_Neutral(); |
| beeptime = 50; |
| Umschlag180Nick = ((long) EE_Parameter.WinkelUmschlagNick * 2500L) + 15000L; |
| Umschlag180Roll = ((long) EE_Parameter.WinkelUmschlagRoll * 2500L) + 15000L; |
| ExternHoehenValue = 0; |
| ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
| GierGyroFehler = 0; |
| SendVersionToNavi = 1; |
| LED_Init(); |
| MikroKopterFlags |= FLAG_CALIBRATE; |
| FromNaviCtrl_Value.Kalman_K = -1; |
| FromNaviCtrl_Value.Kalman_MaxDrift = 0; |
| FromNaviCtrl_Value.Kalman_MaxFusion = 32; |
| Poti1 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110; |
| Poti2 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110; |
| Poti3 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110; |
| Poti4 = PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110; |
| SenderOkay = 100; |
| if(ServoActive) |
| { |
| HEF4017R_ON; |
| DDRD |=0x80; // enable J7 -> Servo signal |
| } |
| } |
| |
| //############################################################################ |
| // Bearbeitet die Messwerte |
| void Mittelwert(void) |
| //############################################################################ |
| { |
| static signed long tmpl,tmpl2,tmpl3,tmpl4; |
| static signed int oldNick, oldRoll, d2Roll, d2Nick; |
| signed long winkel_nick, winkel_roll; |
| |
| MesswertGier = (signed int) AdNeutralGier - AdWertGier; |
| // MesswertGierBias = (signed int) AdNeutralGierBias - AdWertGier; |
| MesswertNick = (signed int) AdWertNickFilter / 8; |
| MesswertRoll = (signed int) AdWertRollFilter / 8; |
| RohMesswertNick = MesswertNick; |
| RohMesswertRoll = MesswertRoll; |
| |
| // Beschleunigungssensor ++++++++++++++++++++++++++++++++++++++++++++++++ |
| Mittelwert_AccNick = ((long)Mittelwert_AccNick * 3 + ((ACC_AMPLIFY * (long)AdWertAccNick))) / 4L; |
| Mittelwert_AccRoll = ((long)Mittelwert_AccRoll * 3 + ((ACC_AMPLIFY * (long)AdWertAccRoll))) / 4L; |
| Mittelwert_AccHoch = ((long)Mittelwert_AccHoch * 3 + ((long)AdWertAccHoch)) / 4L; |
| IntegralAccNick += ACC_AMPLIFY * AdWertAccNick; |
| IntegralAccRoll += ACC_AMPLIFY * AdWertAccRoll; |
| NaviAccNick += AdWertAccNick; |
| NaviAccRoll += AdWertAccRoll; |
| NaviCntAcc++; |
| IntegralAccZ += Aktuell_az - NeutralAccZ; |
| |
| //++++++++++++++++++++++++++++++++++++++++++++++++ |
| // ADC einschalten |
| ANALOG_ON; |
| AdReady = 0; |
| //++++++++++++++++++++++++++++++++++++++++++++++++ |
| |
| if(Mess_IntegralRoll > 93000L) winkel_roll = 93000L; |
| else if(Mess_IntegralRoll <-93000L) winkel_roll = -93000L; |
| else winkel_roll = Mess_IntegralRoll; |
| |
| if(Mess_IntegralNick > 93000L) winkel_nick = 93000L; |
| else if(Mess_IntegralNick <-93000L) winkel_nick = -93000L; |
| else winkel_nick = Mess_IntegralNick; |
| |
| // Gier ++++++++++++++++++++++++++++++++++++++++++++++++ |
| Mess_Integral_Gier += MesswertGier; |
| ErsatzKompass += MesswertGier; |
| // Kopplungsanteil +++++++++++++++++++++++++++++++++++++ |
| if(!Looping_Nick && !Looping_Roll && (EE_Parameter.GlobalConfig & CFG_ACHSENKOPPLUNG_AKTIV)) |
| { |
| tmpl3 = (MesswertRoll * winkel_nick) / 2048L; |
| tmpl3 *= Parameter_AchsKopplung2; //65 |
| tmpl3 /= 4096L; |
| tmpl4 = (MesswertNick * winkel_roll) / 2048L; |
| tmpl4 *= Parameter_AchsKopplung2; //65 |
| tmpl4 /= 4096L; |
| KopplungsteilNickRoll = tmpl3; |
| KopplungsteilRollNick = tmpl4; |
| tmpl4 -= tmpl3; |
| ErsatzKompass += tmpl4; |
| if(!Parameter_CouplingYawCorrection) Mess_Integral_Gier -= tmpl4/2; // Gier nachhelfen |
| |
| tmpl = ((MesswertGier + tmpl4) * winkel_nick) / 2048L; |
| tmpl *= Parameter_AchsKopplung1; // 90 |
| tmpl /= 4096L; |
| tmpl2 = ((MesswertGier + tmpl4) * winkel_roll) / 2048L; |
| tmpl2 *= Parameter_AchsKopplung1; |
| tmpl2 /= 4096L; |
| if(abs(MesswertGier) > 64) if(labs(tmpl) > 128 || labs(tmpl2) > 128) TrichterFlug = 1; |
| //MesswertGier += (Parameter_CouplingYawCorrection * tmpl4) / 256; |
| } |
| else tmpl = tmpl2 = KopplungsteilNickRoll = KopplungsteilRollNick = 0; |
| |
| TrimRoll = tmpl - tmpl2 / 100L; |
| TrimNick = -tmpl2 + tmpl / 100L; |
| |
| // Kompasswert begrenzen ++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(ErsatzKompass >= (360L * GIER_GRAD_FAKTOR)) ErsatzKompass -= 360L * GIER_GRAD_FAKTOR; // 360° Umschlag |
| if(ErsatzKompass < 0) ErsatzKompass += 360L * GIER_GRAD_FAKTOR; |
| // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
| Mess_IntegralRoll2 += MesswertRoll + TrimRoll; |
| Mess_IntegralRoll += MesswertRoll + TrimRoll - LageKorrekturRoll; |
| if(Mess_IntegralRoll > Umschlag180Roll) |
| { |
| Mess_IntegralRoll = -(Umschlag180Roll - 25000L); |
| Mess_IntegralRoll2 = Mess_IntegralRoll; |
| } |
| if(Mess_IntegralRoll <-Umschlag180Roll) |
| { |
| Mess_IntegralRoll = (Umschlag180Roll - 25000L); |
| Mess_IntegralRoll2 = Mess_IntegralRoll; |
| } |
| // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
| Mess_IntegralNick2 += MesswertNick + TrimNick; |
| Mess_IntegralNick += MesswertNick + TrimNick - LageKorrekturNick; |
| if(Mess_IntegralNick > Umschlag180Nick) |
| { |
| Mess_IntegralNick = -(Umschlag180Nick - 25000L); |
| Mess_IntegralNick2 = Mess_IntegralNick; |
| } |
| if(Mess_IntegralNick <-Umschlag180Nick) |
| { |
| Mess_IntegralNick = (Umschlag180Nick - 25000L); |
| Mess_IntegralNick2 = Mess_IntegralNick; |
| } |
| |
| Integral_Gier = Mess_Integral_Gier; |
| IntegralNick = Mess_IntegralNick; |
| IntegralRoll = Mess_IntegralRoll; |
| IntegralNick2 = Mess_IntegralNick2; |
| IntegralRoll2 = Mess_IntegralRoll2; |
| |
| #define D_LIMIT 128 |
| |
| MesswertNick = HiResNick / 8; |
| MesswertRoll = HiResRoll / 8; |
| |
| if(AdWertNick < 15) MesswertNick = -1000; if(AdWertNick < 7) MesswertNick = -2000; |
| if(PlatinenVersion == 10) { if(AdWertNick > 1010) MesswertNick = +1000; if(AdWertNick > 1017) MesswertNick = +2000; } |
| else { if(AdWertNick > 2000) MesswertNick = +1000; if(AdWertNick > 2015) MesswertNick = +2000; } |
| if(AdWertRoll < 15) MesswertRoll = -1000; if(AdWertRoll < 7) MesswertRoll = -2000; |
| if(PlatinenVersion == 10) { if(AdWertRoll > 1010) MesswertRoll = +1000; if(AdWertRoll > 1017) MesswertRoll = +2000; } |
| else { if(AdWertRoll > 2000) MesswertRoll = +1000; if(AdWertRoll > 2015) MesswertRoll = +2000; } |
| |
| if(Parameter_Gyro_D) |
| { |
| d2Nick = HiResNick - oldNick; |
| oldNick = (oldNick + HiResNick)/2; |
| if(d2Nick > D_LIMIT) d2Nick = D_LIMIT; |
| else if(d2Nick < -D_LIMIT) d2Nick = -D_LIMIT; |
| MesswertNick += (d2Nick * (signed int) Parameter_Gyro_D) / 16; |
| d2Roll = HiResRoll - oldRoll; |
| oldRoll = (oldRoll + HiResRoll)/2; |
| if(d2Roll > D_LIMIT) d2Roll = D_LIMIT; |
| else if(d2Roll < -D_LIMIT) d2Roll = -D_LIMIT; |
| MesswertRoll += (d2Roll * (signed int) Parameter_Gyro_D) / 16; |
| HiResNick += (d2Nick * (signed int) Parameter_Gyro_D); |
| HiResRoll += (d2Roll * (signed int) Parameter_Gyro_D); |
| } |
| |
| if(RohMesswertRoll > 0) TrimRoll += ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
| else TrimRoll -= ((long) abs(KopplungsteilNickRoll) * Parameter_CouplingYawCorrection) / 64L; |
| if(RohMesswertNick > 0) TrimNick += ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
| else TrimNick -= ((long) abs(KopplungsteilRollNick) * Parameter_CouplingYawCorrection) / 64L; |
| |
| if(EE_Parameter.GlobalConfig & CFG_DREHRATEN_BEGRENZER && !Looping_Nick && !Looping_Roll) |
| { |
| if(RohMesswertNick > 256) MesswertNick += 1 * (RohMesswertNick - 256); |
| else if(RohMesswertNick < -256) MesswertNick += 1 * (RohMesswertNick + 256); |
| if(RohMesswertRoll > 256) MesswertRoll += 1 * (RohMesswertRoll - 256); |
| else if(RohMesswertRoll < -256) MesswertRoll += 1 * (RohMesswertRoll + 256); |
| } |
| |
| if(Poti1 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110) Poti1++; else if(Poti1 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110 && Poti1) Poti1--; |
| if(Poti2 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110) Poti2++; else if(Poti2 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110 && Poti2) Poti2--; |
| if(Poti3 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110) Poti3++; else if(Poti3 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110 && Poti3) Poti3--; |
| if(Poti4 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110) Poti4++; else if(Poti4 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110 && Poti4) Poti4--; |
| if(Poti1 < 0) Poti1 = 0; else if(Poti1 > 255) Poti1 = 255; |
| if(Poti2 < 0) Poti2 = 0; else if(Poti2 > 255) Poti2 = 255; |
| if(Poti3 < 0) Poti3 = 0; else if(Poti3 > 255) Poti3 = 255; |
| if(Poti4 < 0) Poti4 = 0; else if(Poti4 > 255) Poti4 = 255; |
| } |
| |
| //############################################################################ |
| // Messwerte beim Ermitteln der Nullage |
| void CalibrierMittelwert(void) |
| //############################################################################ |
| { |
| if(PlatinenVersion == 13) SucheGyroOffset(); |
| // ADC auschalten, damit die Werte sich nicht während der Berechnung ändern |
| ANALOG_OFF; |
| MesswertNick = AdWertNick; |
| MesswertRoll = AdWertRoll; |
| MesswertGier = AdWertGier; |
| Mittelwert_AccNick = ACC_AMPLIFY * (long)AdWertAccNick; |
| Mittelwert_AccRoll = ACC_AMPLIFY * (long)AdWertAccRoll; |
| Mittelwert_AccHoch = (long)AdWertAccHoch; |
| // ADC einschalten |
| ANALOG_ON; |
| if(Poti1 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110) Poti1++; else if(Poti1 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI1]] + 110 && Poti1) Poti1--; |
| if(Poti2 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110) Poti2++; else if(Poti2 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI2]] + 110 && Poti2) Poti2--; |
| if(Poti3 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110) Poti3++; else if(Poti3 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI3]] + 110 && Poti3) Poti3--; |
| if(Poti4 < PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110) Poti4++; else if(Poti4 > PPM_in[EE_Parameter.Kanalbelegung[K_POTI4]] + 110 && Poti4) Poti4--; |
| if(Poti1 < 0) Poti1 = 0; else if(Poti1 > 255) Poti1 = 255; |
| if(Poti2 < 0) Poti2 = 0; else if(Poti2 > 255) Poti2 = 255; |
| if(Poti3 < 0) Poti3 = 0; else if(Poti3 > 255) Poti3 = 255; |
| if(Poti4 < 0) Poti4 = 0; else if(Poti4 > 255) Poti4 = 255; |
| |
| Umschlag180Nick = (long) EE_Parameter.WinkelUmschlagNick * 2500L; |
| Umschlag180Roll = (long) EE_Parameter.WinkelUmschlagRoll * 2500L; |
| } |
| |
| //############################################################################ |
| // Senden der Motorwerte per I2C-Bus |
| void SendMotorData(void) |
| //############################################################################ |
| { |
| unsigned char i; |
| if(!MotorenEin) |
| { |
| MikroKopterFlags &= ~(FLAG_MOTOR_RUN | FLAG_FLY); |
| for(i=0;i<MAX_MOTORS;i++) |
| { |
| if(!PC_MotortestActive) MotorTest[i] = 0; |
| Motor[i] = MotorTest[i]; |
| } |
| if(PC_MotortestActive) PC_MotortestActive--; |
| } |
| else MikroKopterFlags |= FLAG_MOTOR_RUN; |
| |
| DebugOut.Analog[12] = Motor[0]; |
| DebugOut.Analog[13] = Motor[1]; |
| DebugOut.Analog[14] = Motor[3]; |
| DebugOut.Analog[15] = Motor[2]; |
| |
| //Start I2C Interrupt Mode |
| twi_state = 0; |
| motor = 0; |
| i2c_start(); |
| } |
| |
| |
| |
| //############################################################################ |
| // Trägt ggf. das Poti als Parameter ein |
| void ParameterZuordnung(void) |
| //############################################################################ |
| { |
| #define CHK_POTI_MM(b,a,min,max) { if(a > 250) { if(a == 251) b = Poti1; else if(a == 252) b = Poti2; else if(a == 253) b = Poti3; else if(a == 254) b = Poti4;} else b = a; if(b <= min) b = min; else if(b >= max) b = max;} |
| #define CHK_POTI(b,a,min,max) { if(a > 250) { if(a == 251) b = Poti1; else if(a == 252) b = Poti2; else if(a == 253) b = Poti3; else if(a == 254) b = Poti4;} else b = a; } |
| CHK_POTI(Parameter_MaxHoehe,EE_Parameter.MaxHoehe,0,255); |
| CHK_POTI_MM(Parameter_Luftdruck_D,EE_Parameter.Luftdruck_D,0,100); |
| CHK_POTI_MM(Parameter_Hoehe_P,EE_Parameter.Hoehe_P,0,100); |
| CHK_POTI(Parameter_Hoehe_ACC_Wirkung,EE_Parameter.Hoehe_ACC_Wirkung,0,255); |
| CHK_POTI(Parameter_Hoehe_GPS_Z,EE_Parameter.Hoehe_GPS_Z,0,255); |
| CHK_POTI(Parameter_KompassWirkung,EE_Parameter.KompassWirkung,0,255); |
| CHK_POTI_MM(Parameter_Gyro_P,EE_Parameter.Gyro_P,10,255); |
| CHK_POTI(Parameter_Gyro_I,EE_Parameter.Gyro_I,0,255); |
| CHK_POTI(Parameter_Gyro_D,EE_Parameter.Gyro_D,0,255); |
| CHK_POTI(Parameter_Gyro_Gier_P,EE_Parameter.Gyro_Gier_P,10,255); |
| CHK_POTI(Parameter_Gyro_Gier_I,EE_Parameter.Gyro_Gier_I,0,255); |
| CHK_POTI(Parameter_I_Faktor,EE_Parameter.I_Faktor,0,255); |
| CHK_POTI(Parameter_UserParam1,EE_Parameter.UserParam1,0,255); |
| CHK_POTI(Parameter_UserParam2,EE_Parameter.UserParam2,0,255); |
| CHK_POTI(Parameter_UserParam3,EE_Parameter.UserParam3,0,255); |
| CHK_POTI(Parameter_UserParam4,EE_Parameter.UserParam4,0,255); |
| CHK_POTI(Parameter_UserParam5,EE_Parameter.UserParam5,0,255); |
| CHK_POTI(Parameter_UserParam6,EE_Parameter.UserParam6,0,255); |
| CHK_POTI(Parameter_UserParam7,EE_Parameter.UserParam7,0,255); |
| CHK_POTI(Parameter_UserParam8,EE_Parameter.UserParam8,0,255); |
| CHK_POTI(Parameter_ServoNickControl,EE_Parameter.ServoNickControl,0,255); |
| CHK_POTI(Parameter_ServoRollControl,EE_Parameter.ServoRollControl,0,255); |
| CHK_POTI(Parameter_LoopGasLimit,EE_Parameter.LoopGasLimit,0,255); |
| CHK_POTI(Parameter_AchsKopplung1, EE_Parameter.AchsKopplung1,0,255); |
| CHK_POTI(Parameter_AchsKopplung2, EE_Parameter.AchsKopplung2,0,255); |
| CHK_POTI(Parameter_CouplingYawCorrection,EE_Parameter.CouplingYawCorrection,0,255); |
| // CHK_POTI(Parameter_AchsGegenKopplung1,EE_Parameter.AchsGegenKopplung1,0,255); |
| CHK_POTI(Parameter_DynamicStability,EE_Parameter.DynamicStability,0,255); |
| CHK_POTI_MM(Parameter_J16Timing,EE_Parameter.J16Timing,1,255); |
| CHK_POTI_MM(Parameter_J17Timing,EE_Parameter.J17Timing,1,255); |
| CHK_POTI(Parameter_ExternalControl,EE_Parameter.ExternalControl,0,255); |
| Ki = 10300 / (Parameter_I_Faktor + 1); |
| MAX_GAS = EE_Parameter.Gas_Max; |
| MIN_GAS = EE_Parameter.Gas_Min; |
| } |
| |
| |
| //############################################################################ |
| // |
| void MotorRegler(void) |
| //############################################################################ |
| { |
| int pd_ergebnis_nick,pd_ergebnis_roll,tmp_int, tmp_int2; |
| int GierMischanteil,GasMischanteil; |
| static long SummeNick=0,SummeRoll=0; |
| static long sollGier = 0,tmp_long,tmp_long2; |
| static long IntegralFehlerNick = 0; |
| static long IntegralFehlerRoll = 0; |
| static unsigned int RcLostTimer; |
| static unsigned char delay_neutral = 0; |
| static unsigned char delay_einschalten = 0,delay_ausschalten = 0; |
| static char TimerWerteausgabe = 0; |
| static char NeueKompassRichtungMerken = 0; |
| static long ausgleichNick, ausgleichRoll; |
| int IntegralNickMalFaktor,IntegralRollMalFaktor; |
| unsigned char i; |
| if(--LoadHandler == 0) LoadHandler = 5; // verteilt die Prozessorlast |
| Mittelwert(); |
| GRN_ON; |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Gaswert ermitteln |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| GasMischanteil = StickGas; |
| if(GasMischanteil < MIN_GAS + 10) GasMischanteil = MIN_GAS + 10; |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Empfang schlecht |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(SenderOkay < 100) |
| { |
| if(RcLostTimer) RcLostTimer--; |
| else |
| { |
| MotorenEin = 0; |
| MikroKopterFlags &= ~FLAG_NOTLANDUNG; |
| } |
| ROT_ON; |
| if(modell_fliegt > 1000) // wahrscheinlich in der Luft --> langsam absenken |
| { |
| GasMischanteil = EE_Parameter.NotGas; |
| MikroKopterFlags |= FLAG_NOTLANDUNG; |
| PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
| PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
| PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] = 0; |
| PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] = 0; |
| PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] = 0; |
| } |
| else MotorenEin = 0; |
| } |
| else |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Emfang gut |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(SenderOkay > 140) |
| { |
| MikroKopterFlags &= ~FLAG_NOTLANDUNG; |
| RcLostTimer = EE_Parameter.NotGasZeit * 50; |
| if(GasMischanteil > 40 && MotorenEin) |
| { |
| if(modell_fliegt < 0xffff) modell_fliegt++; |
| } |
| if((modell_fliegt < 256)) |
| { |
| SummeNick = 0; |
| SummeRoll = 0; |
| if(modell_fliegt == 250) |
| { |
| NeueKompassRichtungMerken = 1; |
| sollGier = 0; |
| Mess_Integral_Gier = 0; |
| // Mess_Integral_Gier2 = 0; |
| } |
| } else MikroKopterFlags |= FLAG_FLY; |
| |
| if((PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] > 80) && MotorenEin == 0) |
| { |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // auf Nullwerte kalibrieren |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) // Neutralwerte |
| { |
| if(++delay_neutral > 200) // nicht sofort |
| { |
| GRN_OFF; |
| MotorenEin = 0; |
| delay_neutral = 0; |
| modell_fliegt = 0; |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70 || abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) > 70) |
| { |
| unsigned char setting=1; |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 1; |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 2; |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < 70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 3; |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > 70) setting = 4; |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] <-70 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < 70) setting = 5; |
| SetActiveParamSetNumber(setting); // aktiven Datensatz merken |
| } |
| // else |
| if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]) < 30 && PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -70) |
| { |
| WinkelOut.CalcState = 1; |
| beeptime = 1000; |
| } |
| else |
| { |
| ReadParameterSet(GetActiveParamSetNumber(), (unsigned char *) &EE_Parameter.Kanalbelegung[0], STRUCT_PARAM_LAENGE); |
| if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)) // Höhenregelung aktiviert? |
| { |
| if((MessLuftdruck > 950) || (MessLuftdruck < 750)) SucheLuftruckOffset(); |
| } |
| ServoActive = 0; |
| SetNeutral(); |
| ServoActive = 1; |
| DDRD |=0x80; // enable J7 -> Servo signal |
| Piep(GetActiveParamSetNumber(),120); |
| } |
| } |
| } |
| else |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) // ACC Neutralwerte speichern |
| { |
| if(++delay_neutral > 200) // nicht sofort |
| { |
| GRN_OFF; |
| eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_NICK],0xff); // Werte löschen |
| MotorenEin = 0; |
| delay_neutral = 0; |
| modell_fliegt = 0; |
| SetNeutral(); |
| eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_NICK],NeutralAccX / 256); // ACC-NeutralWerte speichern |
| eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_NICK+1],NeutralAccX % 256); // ACC-NeutralWerte speichern |
| eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL],NeutralAccY / 256); |
| eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_ROLL+1],NeutralAccY % 256); |
| eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_Z],(int)NeutralAccZ / 256); |
| eeprom_write_byte(&EEPromArray[EEPROM_ADR_ACC_Z+1],(int)NeutralAccZ % 256); |
| Piep(GetActiveParamSetNumber(),120); |
| } |
| } |
| else delay_neutral = 0; |
| } |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Gas ist unten |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] < 35-120) |
| { |
| // Starten |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] < -75) |
| { |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Einschalten |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(++delay_einschalten > 200) |
| { |
| delay_einschalten = 200; |
| modell_fliegt = 1; |
| MotorenEin = 1; |
| sollGier = 0; |
| Mess_Integral_Gier = 0; |
| Mess_Integral_Gier2 = 0; |
| Mess_IntegralNick = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccNick; |
| Mess_IntegralRoll = EE_Parameter.GyroAccFaktor * (long)Mittelwert_AccRoll; |
| Mess_IntegralNick2 = IntegralNick; |
| Mess_IntegralRoll2 = IntegralRoll; |
| SummeNick = 0; |
| SummeRoll = 0; |
| MikroKopterFlags |= FLAG_START; |
| KompassEinschaltStartwert = KompassValue; |
| } |
| } |
| else delay_einschalten = 0; |
| //Auf Neutralwerte setzen |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Auschalten |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]] > 75) |
| { |
| if(++delay_ausschalten > 200) // nicht sofort |
| { |
| MotorenEin = 0; |
| delay_ausschalten = 200; |
| modell_fliegt = 0; |
| } |
| } |
| else delay_ausschalten = 0; |
| } |
| } |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // neue Werte von der Funke |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| |
| if(!NewPpmData-- || (MikroKopterFlags & FLAG_NOTLANDUNG)) |
| { |
| static int stick_nick,stick_roll; |
| int e_stick_nick, e_stick_nick_diff, e_stick_roll, e_stick_roll_diff; |
| int stick_p, stick_d; |
| |
| ParameterZuordnung(); |
| |
| stick_p = EE_Parameter.Stick_P; |
| stick_d = EE_Parameter.Stick_D; |
| |
| if (Parameter_UserParam8) { |
| |
| int angle, stick_nick_tmp, stick_roll_tmp; |
| |
| if (Parameter_UserParam8 == 254) { |
| angle = -45; |
| } else if (Parameter_UserParam8 > 128) { |
| angle = KompassValue; |
| } else { |
| angle = (ErsatzKompass / GIER_GRAD_FAKTOR); |
| } |
| |
| angle = ((KompassEinschaltStartwert - angle + 360) % 360); |
| |
| stick_nick_tmp = (long)c_cos_8192(angle) * (long)PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] / 8192L; |
| stick_roll_tmp = (long)c_sin_8192(angle) * (long)PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] / 8192L; |
| |
| e_stick_nick = stick_roll_tmp + stick_nick_tmp; |
| e_stick_roll = stick_roll_tmp - stick_nick_tmp; |
| |
| stick_nick_tmp = (long)c_cos_8192(angle) * (long)PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]] / 8192L; |
| stick_roll_tmp = (long)c_sin_8192(angle) * (long)PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]] / 8192L; |
| |
| e_stick_nick_diff = stick_roll_tmp + stick_nick_tmp; |
| e_stick_roll_diff = stick_roll_tmp - stick_nick_tmp; |
| |
| if (Parameter_UserParam8 == 255) { |
| |
| int gier = abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]); |
| if (gier > 100) { |
| stick_d /= 3; |
| } else if (gier > 50) { |
| stick_d /= 2; |
| } |
| |
| if (stick_d < 1) { |
| stick_d = 1; |
| } |
| |
| } |
| |
| /* |
| DebugOut.Analog[12] = PPM_in[EE_Parameter.Kanalbelegung[K_NICK]]; |
| DebugOut.Analog[13] = e_stick_nick; |
| DebugOut.Analog[14] = PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]; |
| DebugOut.Analog[15] = e_stick_roll; |
| */ |
| |
| } else { |
| |
| e_stick_nick = PPM_in[EE_Parameter.Kanalbelegung[K_NICK]]; |
| e_stick_roll = PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]]; |
| e_stick_nick_diff = PPM_diff[EE_Parameter.Kanalbelegung[K_NICK]]; |
| e_stick_roll_diff = PPM_diff[EE_Parameter.Kanalbelegung[K_ROLL]]; |
| |
| } |
| |
| stick_nick = (stick_nick * 3 + e_stick_nick * stick_p) / 4; |
| stick_nick += e_stick_nick_diff * stick_d; |
| StickNick = stick_nick - (GPS_Nick + GPS_Nick2); |
| |
| stick_roll = (stick_roll * 3 + e_stick_roll * stick_p) / 4; |
| stick_roll += e_stick_roll_diff * stick_d; |
| StickRoll = stick_roll - (GPS_Roll + GPS_Roll2); |
| |
| StickGier = -PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]; |
| if(StickGier > 2) StickGier -= 2; else |
| if(StickGier < -2) StickGier += 2; else StickGier = 0; |
| |
| StickGas = PPM_in[EE_Parameter.Kanalbelegung[K_GAS]] + 120; |
| |
| GyroFaktor = (Parameter_Gyro_P + 10.0); |
| IntegralFaktor = Parameter_Gyro_I; |
| GyroFaktorGier = (Parameter_Gyro_Gier_P + 10.0); |
| IntegralFaktorGier = Parameter_Gyro_Gier_I; |
| |
| //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| //+ Analoge Steuerung per Seriell |
| //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(ExternControl.Config & 0x01 && Parameter_ExternalControl > 128) |
| { |
| StickNick += (int) ExternControl.Nick * (int) EE_Parameter.Stick_P; |
| StickRoll += (int) ExternControl.Roll * (int) EE_Parameter.Stick_P; |
| StickGier += ExternControl.Gier; |
| ExternHoehenValue = (int) ExternControl.Hight * (int)EE_Parameter.Hoehe_Verstaerkung; |
| if(ExternControl.Gas < StickGas) StickGas = ExternControl.Gas; |
| } |
| if(StickGas < 0) StickGas = 0; |
| |
| if(EE_Parameter.GlobalConfig & CFG_HEADING_HOLD) IntegralFaktor = 0; |
| //if(GyroFaktor < 0) GyroFaktor = 0; |
| //if(IntegralFaktor < 0) IntegralFaktor = 0; |
| |
| if(abs(StickNick/STICK_GAIN) > MaxStickNick) |
| { |
| MaxStickNick = abs(StickNick)/STICK_GAIN; |
| if(MaxStickNick > 100) MaxStickNick = 100; |
| } |
| else MaxStickNick--; |
| if(abs(StickRoll/STICK_GAIN) > MaxStickRoll) |
| { |
| MaxStickRoll = abs(StickRoll)/STICK_GAIN; |
| if(MaxStickRoll > 100) MaxStickRoll = 100; |
| } |
| else MaxStickRoll--; |
| if(MikroKopterFlags & FLAG_NOTLANDUNG) {MaxStickNick = 0; MaxStickRoll = 0;} |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Looping? |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_LINKS) Looping_Links = 1; |
| else |
| { |
| { |
| if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Links = 0; |
| } |
| } |
| if((PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_RECHTS) Looping_Rechts = 1; |
| else |
| { |
| if(Looping_Rechts) // Hysterese |
| { |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_ROLL]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Rechts = 0; |
| } |
| } |
| |
| if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_OBEN) Looping_Oben = 1; |
| else |
| { |
| if(Looping_Oben) // Hysterese |
| { |
| if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < (EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese))) Looping_Oben = 0; |
| } |
| } |
| if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -EE_Parameter.LoopThreshold) && EE_Parameter.BitConfig & CFG_LOOP_UNTEN) Looping_Unten = 1; |
| else |
| { |
| if(Looping_Unten) // Hysterese |
| { |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -(EE_Parameter.LoopThreshold - EE_Parameter.LoopHysterese)) Looping_Unten = 0; |
| } |
| } |
| |
| if(Looping_Links || Looping_Rechts) Looping_Roll = 1; else Looping_Roll = 0; |
| if(Looping_Oben || Looping_Unten) { Looping_Nick = 1; Looping_Roll = 0; Looping_Links = 0; Looping_Rechts = 0;} else Looping_Nick = 0; |
| } // Ende neue Funken-Werte |
| |
| if(Looping_Roll || Looping_Nick) |
| { |
| if(GasMischanteil > EE_Parameter.LoopGasLimit) GasMischanteil = EE_Parameter.LoopGasLimit; |
| TrichterFlug = 1; |
| } |
| |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Bei Empfangsausfall im Flug |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(MikroKopterFlags & FLAG_NOTLANDUNG) |
| { |
| StickGier = 0; |
| StickNick = 0; |
| StickRoll = 0; |
| GyroFaktor = 90; |
| IntegralFaktor = 120; |
| GyroFaktorGier = 90; |
| IntegralFaktorGier = 120; |
| Looping_Roll = 0; |
| Looping_Nick = 0; |
| } |
| |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Integrale auf ACC-Signal abgleichen |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| #define ABGLEICH_ANZAHL 256L |
| |
| MittelIntegralNick += IntegralNick; // Für die Mittelwertbildung aufsummieren |
| MittelIntegralRoll += IntegralRoll; |
| MittelIntegralNick2 += IntegralNick2; |
| MittelIntegralRoll2 += IntegralRoll2; |
| |
| if(Looping_Nick || Looping_Roll) |
| { |
| IntegralAccNick = 0; |
| IntegralAccRoll = 0; |
| MittelIntegralNick = 0; |
| MittelIntegralRoll = 0; |
| MittelIntegralNick2 = 0; |
| MittelIntegralRoll2 = 0; |
| Mess_IntegralNick2 = Mess_IntegralNick; |
| Mess_IntegralRoll2 = Mess_IntegralRoll; |
| ZaehlMessungen = 0; |
| LageKorrekturNick = 0; |
| LageKorrekturRoll = 0; |
| } |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(!Looping_Nick && !Looping_Roll && (Aktuell_az > 512 || MotorenEin)) |
| { |
| long tmp_long, tmp_long2; |
| if(FromNaviCtrl_Value.Kalman_K != -1 /*&& !TrichterFlug*/) |
| { |
| tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
| tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
| tmp_long = (tmp_long * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
| tmp_long2 = (tmp_long2 * FromNaviCtrl_Value.Kalman_K) / (32 * 16); |
| if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
| { |
| tmp_long /= 2; |
| tmp_long2 /= 2; |
| } |
| if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
| { |
| tmp_long /= 3; |
| tmp_long2 /= 3; |
| } |
| if(tmp_long > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
| if(tmp_long < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
| if(tmp_long2 > (long) FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long) FromNaviCtrl_Value.Kalman_MaxFusion; |
| if(tmp_long2 < (long)-FromNaviCtrl_Value.Kalman_MaxFusion) tmp_long2 = (long)-FromNaviCtrl_Value.Kalman_MaxFusion; |
| } |
| else |
| { |
| tmp_long = (long)(IntegralNick / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccNick); |
| tmp_long2 = (long)(IntegralRoll / EE_Parameter.GyroAccFaktor - (long)Mittelwert_AccRoll); |
| tmp_long /= 16; |
| tmp_long2 /= 16; |
| if((MaxStickNick > 64) || (MaxStickRoll > 64)) |
| { |
| tmp_long /= 3; |
| tmp_long2 /= 3; |
| } |
| if(abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25) |
| { |
| tmp_long /= 3; |
| tmp_long2 /= 3; |
| } |
| |
| #define AUSGLEICH 32 |
| if(tmp_long > AUSGLEICH) tmp_long = AUSGLEICH; |
| if(tmp_long < -AUSGLEICH) tmp_long =-AUSGLEICH; |
| if(tmp_long2 > AUSGLEICH) tmp_long2 = AUSGLEICH; |
| if(tmp_long2 <-AUSGLEICH) tmp_long2 =-AUSGLEICH; |
| } |
| |
| //if(Poti2 > 20) { tmp_long = 0; tmp_long2 = 0;} |
| Mess_IntegralNick -= tmp_long; |
| Mess_IntegralRoll -= tmp_long2; |
| } |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(ZaehlMessungen >= ABGLEICH_ANZAHL) |
| { |
| static int cnt = 0; |
| static char last_n_p,last_n_n,last_r_p,last_r_n; |
| static long MittelIntegralNick_Alt,MittelIntegralRoll_Alt; |
| if(!Looping_Nick && !Looping_Roll && !TrichterFlug && EE_Parameter.Driftkomp) |
| { |
| MittelIntegralNick /= ABGLEICH_ANZAHL; |
| MittelIntegralRoll /= ABGLEICH_ANZAHL; |
| IntegralAccNick = (EE_Parameter.GyroAccFaktor * IntegralAccNick) / ABGLEICH_ANZAHL; |
| IntegralAccRoll = (EE_Parameter.GyroAccFaktor * IntegralAccRoll) / ABGLEICH_ANZAHL; |
| IntegralAccZ = IntegralAccZ / ABGLEICH_ANZAHL; |
| #define MAX_I 0//(Poti2/10) |
| // Nick ++++++++++++++++++++++++++++++++++++++++++++++++ |
| IntegralFehlerNick = (long)(MittelIntegralNick - (long)IntegralAccNick); |
| ausgleichNick = IntegralFehlerNick / EE_Parameter.GyroAccAbgleich; |
| // Roll ++++++++++++++++++++++++++++++++++++++++++++++++ |
| IntegralFehlerRoll = (long)(MittelIntegralRoll - (long)IntegralAccRoll); |
| ausgleichRoll = IntegralFehlerRoll / EE_Parameter.GyroAccAbgleich; |
| |
| LageKorrekturNick = ausgleichNick / ABGLEICH_ANZAHL; |
| LageKorrekturRoll = ausgleichRoll / ABGLEICH_ANZAHL; |
| |
| if(((MaxStickNick > 64) || (MaxStickRoll > 64) || (abs(PPM_in[EE_Parameter.Kanalbelegung[K_GIER]]) > 25)) && (FromNaviCtrl_Value.Kalman_K == -1)) |
| { |
| LageKorrekturNick /= 2; |
| LageKorrekturRoll /= 2; |
| } |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Gyro-Drift ermitteln |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| MittelIntegralNick2 /= ABGLEICH_ANZAHL; |
| MittelIntegralRoll2 /= ABGLEICH_ANZAHL; |
| tmp_long = IntegralNick2 - IntegralNick; |
| tmp_long2 = IntegralRoll2 - IntegralRoll; |
| //DebugOut.Analog[25] = MittelIntegralRoll2 / 26; |
| |
| IntegralFehlerNick = tmp_long; |
| IntegralFehlerRoll = tmp_long2; |
| Mess_IntegralNick2 -= IntegralFehlerNick; |
| Mess_IntegralRoll2 -= IntegralFehlerRoll; |
| |
| if(EE_Parameter.Driftkomp) |
| { |
| if(GierGyroFehler > ABGLEICH_ANZAHL/2) { AdNeutralGier++; AdNeutralGierBias++; } |
| if(GierGyroFehler <-ABGLEICH_ANZAHL/2) { AdNeutralGier--; AdNeutralGierBias--; } |
| } |
| GierGyroFehler = 0; |
| |
| |
| #define FEHLER_LIMIT (ABGLEICH_ANZAHL / 2) |
| #define FEHLER_LIMIT1 (ABGLEICH_ANZAHL * 2) //4 |
| #define FEHLER_LIMIT2 (ABGLEICH_ANZAHL * 16) //16 |
| #define BEWEGUNGS_LIMIT 20000 |
| // Nick +++++++++++++++++++++++++++++++++++++++++++++++++ |
| cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
| if(labs(IntegralFehlerNick) > FEHLER_LIMIT1) cnt = 4; |
| if(labs(MittelIntegralNick_Alt - MittelIntegralNick) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
| { |
| if(IntegralFehlerNick > FEHLER_LIMIT2) |
| { |
| if(last_n_p) |
| { |
| cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
| ausgleichNick = IntegralFehlerNick / 8; |
| if(ausgleichNick > 5000) ausgleichNick = 5000; |
| LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
| } |
| else last_n_p = 1; |
| } else last_n_p = 0; |
| if(IntegralFehlerNick < -FEHLER_LIMIT2) |
| { |
| if(last_n_n) |
| { |
| cnt += labs(IntegralFehlerNick) / (FEHLER_LIMIT2 / 8); |
| ausgleichNick = IntegralFehlerNick / 8; |
| if(ausgleichNick < -5000) ausgleichNick = -5000; |
| LageKorrekturNick += ausgleichNick / ABGLEICH_ANZAHL; |
| } |
| else last_n_n = 1; |
| } else last_n_n = 0; |
| } |
| else |
| { |
| cnt = 0; |
| KompassSignalSchlecht = 1000; |
| } |
| if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
| if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
| if(IntegralFehlerNick > FEHLER_LIMIT) AdNeutralNick += cnt; |
| if(IntegralFehlerNick < -FEHLER_LIMIT) AdNeutralNick -= cnt; |
| |
| // Roll +++++++++++++++++++++++++++++++++++++++++++++++++ |
| cnt = 1;// + labs(IntegralFehlerNick) / 4096; |
| if(labs(IntegralFehlerRoll) > FEHLER_LIMIT1) cnt = 4; |
| ausgleichRoll = 0; |
| if(labs(MittelIntegralRoll_Alt - MittelIntegralRoll) < BEWEGUNGS_LIMIT || (FromNaviCtrl_Value.Kalman_MaxDrift > 3*8)) |
| { |
| if(IntegralFehlerRoll > FEHLER_LIMIT2) |
| { |
| if(last_r_p) |
| { |
| cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
| ausgleichRoll = IntegralFehlerRoll / 8; |
| if(ausgleichRoll > 5000) ausgleichRoll = 5000; |
| LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
| } |
| else last_r_p = 1; |
| } else last_r_p = 0; |
| if(IntegralFehlerRoll < -FEHLER_LIMIT2) |
| { |
| if(last_r_n) |
| { |
| cnt += labs(IntegralFehlerRoll) / (FEHLER_LIMIT2 / 8); |
| ausgleichRoll = IntegralFehlerRoll / 8; |
| if(ausgleichRoll < -5000) ausgleichRoll = -5000; |
| LageKorrekturRoll += ausgleichRoll / ABGLEICH_ANZAHL; |
| } |
| else last_r_n = 1; |
| } else last_r_n = 0; |
| } else |
| { |
| cnt = 0; |
| KompassSignalSchlecht = 1000; |
| } |
| if(cnt > EE_Parameter.Driftkomp) cnt = EE_Parameter.Driftkomp; |
| if(FromNaviCtrl_Value.Kalman_MaxDrift) if(cnt > FromNaviCtrl_Value.Kalman_MaxDrift) cnt = FromNaviCtrl_Value.Kalman_MaxDrift; |
| if(IntegralFehlerRoll > FEHLER_LIMIT) AdNeutralRoll += cnt; |
| if(IntegralFehlerRoll < -FEHLER_LIMIT) AdNeutralRoll -= cnt; |
| } |
| else |
| { |
| LageKorrekturRoll = 0; |
| LageKorrekturNick = 0; |
| TrichterFlug = 0; |
| } |
| |
| if(!IntegralFaktor) { LageKorrekturRoll = 0; LageKorrekturNick = 0;} // z.B. bei HH |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| MittelIntegralNick_Alt = MittelIntegralNick; |
| MittelIntegralRoll_Alt = MittelIntegralRoll; |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| IntegralAccNick = 0; |
| IntegralAccRoll = 0; |
| IntegralAccZ = 0; |
| MittelIntegralNick = 0; |
| MittelIntegralRoll = 0; |
| MittelIntegralNick2 = 0; |
| MittelIntegralRoll2 = 0; |
| ZaehlMessungen = 0; |
| } // ZaehlMessungen >= ABGLEICH_ANZAHL |
| |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Gieren |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // if(GasMischanteil < 35) { if(StickGier > 10) StickGier = 10; else if(StickGier < -10) StickGier = -10;}; |
| if(abs(StickGier) > 15) // war 35 |
| { |
| KompassSignalSchlecht = 1000; |
| if(!(EE_Parameter.GlobalConfig & CFG_KOMPASS_FIX)) |
| { |
| NeueKompassRichtungMerken = 1; |
| }; |
| } |
| tmp_int = (long) EE_Parameter.Gier_P * ((long)StickGier * abs(StickGier)) / 512L; // expo y = ax + bx² |
| tmp_int += (EE_Parameter.Gier_P * StickGier) / 4; |
| sollGier = tmp_int; |
| Mess_Integral_Gier -= tmp_int; |
| if(Mess_Integral_Gier > 50000) Mess_Integral_Gier = 50000; // begrenzen |
| if(Mess_Integral_Gier <-50000) Mess_Integral_Gier =-50000; |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Kompass |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| //DebugOut.Analog[16] = KompassSignalSchlecht; |
| |
| if(KompassValue && (EE_Parameter.GlobalConfig & CFG_KOMPASS_AKTIV)) |
| { |
| int w,v,r,fehler,korrektur; |
| w = abs(IntegralNick /512); // mit zunehmender Neigung den Einfluss drosseln |
| v = abs(IntegralRoll /512); |
| if(v > w) w = v; // grösste Neigung ermitteln |
| korrektur = w / 8 + 1; |
| fehler = ((540 + KompassValue - (ErsatzKompass/GIER_GRAD_FAKTOR)) % 360) - 180; |
| if(abs(MesswertGier) > 128) |
| { |
| fehler = 0; |
| } |
| if(!KompassSignalSchlecht && w < 25) |
| { |
| GierGyroFehler += fehler; |
| if(NeueKompassRichtungMerken) |
| { |
| // beeptime = 200; |
| // KompassStartwert = KompassValue; |
| ErsatzKompass = KompassValue * GIER_GRAD_FAKTOR; |
| KompassStartwert = (ErsatzKompass/GIER_GRAD_FAKTOR); |
| NeueKompassRichtungMerken = 0; |
| } |
| } |
| ErsatzKompass += (fehler * 8) / korrektur; |
| w = (w * Parameter_KompassWirkung) / 32; // auf die Wirkung normieren |
| w = Parameter_KompassWirkung - w; // Wirkung ggf drosseln |
| if(w >= 0) |
| { |
| if(!KompassSignalSchlecht) |
| { |
| v = 64 + ((MaxStickNick + MaxStickRoll)) / 8; |
| r = ((540 + (ErsatzKompass/GIER_GRAD_FAKTOR) - KompassStartwert) % 360) - 180; |
| // r = KompassRichtung; |
| v = (r * w) / v; // nach Kompass ausrichten |
| w = 3 * Parameter_KompassWirkung; |
| if(v > w) v = w; // Begrenzen |
| else |
| if(v < -w) v = -w; |
| Mess_Integral_Gier += v; |
| } |
| if(KompassSignalSchlecht) KompassSignalSchlecht--; |
| } |
| else KompassSignalSchlecht = 500; // so lange das Signal taub stellen --> ca. 1 sek |
| } |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Debugwerte zuordnen |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(!TimerWerteausgabe--) |
| { |
| TimerWerteausgabe = 24; |
| |
| DebugOut.Analog[0] = IntegralNick / (EE_Parameter.GyroAccFaktor * 4); |
| DebugOut.Analog[1] = IntegralRoll / (EE_Parameter.GyroAccFaktor * 4); |
| DebugOut.Analog[2] = Mittelwert_AccNick / 4; |
| DebugOut.Analog[3] = Mittelwert_AccRoll / 4; |
| DebugOut.Analog[4] = MesswertGier; |
| DebugOut.Analog[5] = HoehenWert/5; |
| DebugOut.Analog[6] = Aktuell_az;//(Mess_Integral_Hoch / 512);//Aktuell_az; |
| DebugOut.Analog[8] = KompassValue; |
| DebugOut.Analog[9] = UBat; |
| DebugOut.Analog[10] = SenderOkay; |
| DebugOut.Analog[11] = ErsatzKompass / GIER_GRAD_FAKTOR; |
| //DebugOut.Analog[16] = Mittelwert_AccHoch; |
| //DebugOut.Analog[17] = FromNaviCtrl_Value.Distance; |
| DebugOut.Analog[18] = VarioMeter; |
| DebugOut.Analog[19] = WinkelOut.CalcState; |
| DebugOut.Analog[20] = ServoNickValue; |
| // DebugOut.Analog[22] = FromNaviCtrl_Value.GpsZ; |
| // DebugOut.Analog[24] = MesswertNick/2; |
| // DebugOut.Analog[25] = MesswertRoll/2; |
| // DebugOut.Analog[27] = (int)FromNaviCtrl_Value.Kalman_MaxDrift; |
| // DebugOut.Analog[28] = (int)FromNaviCtrl_Value.Kalman_MaxFusion; |
| // DebugOut.Analog[29] = (int)FromNaviCtrl_Value.Kalman_K; |
| //DebugOut.Analog[28] = I2CError; |
| // DebugOut.Analog[29] = FromNaviCtrl_Value.SerialDataOkay; |
| DebugOut.Analog[30] = GPS_Nick; |
| DebugOut.Analog[31] = GPS_Roll; |
| } |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Drehgeschwindigkeit und -winkel zu einem Istwert zusammenfassen |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(TrichterFlug) { SummeRoll = 0; SummeNick = 0;}; |
| |
| if(!Looping_Nick) IntegralNickMalFaktor = (IntegralNick * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralNickMalFaktor = 0; |
| if(!Looping_Roll) IntegralRollMalFaktor = (IntegralRoll * IntegralFaktor) / (44000 / STICK_GAIN); else IntegralRollMalFaktor = 0; |
| |
| #define TRIM_MAX 200 |
| if(TrimNick > TRIM_MAX) TrimNick = TRIM_MAX; else if(TrimNick <-TRIM_MAX) TrimNick =-TRIM_MAX; |
| if(TrimRoll > TRIM_MAX) TrimRoll = TRIM_MAX; else if(TrimRoll <-TRIM_MAX) TrimRoll =-TRIM_MAX; |
| |
| MesswertNick = IntegralNickMalFaktor + (long)((long)MesswertNick * GyroFaktor + (long)TrimNick * 128L) / (256L / STICK_GAIN); |
| MesswertRoll = IntegralRollMalFaktor + (long)((long)MesswertRoll * GyroFaktor + (long)TrimRoll * 128L) / (256L / STICK_GAIN); |
| MesswertGier = (long)(MesswertGier * 2 * (long)GyroFaktorGier) / (256L / STICK_GAIN) + (long)(Integral_Gier * IntegralFaktorGier) / (2 * (44000 / STICK_GAIN)); |
| |
| // Maximalwerte abfangen |
| // #define MAX_SENSOR (4096*STICK_GAIN) |
| #define MAX_SENSOR (4096*4) |
| if(MesswertNick > MAX_SENSOR) MesswertNick = MAX_SENSOR; |
| if(MesswertNick < -MAX_SENSOR) MesswertNick = -MAX_SENSOR; |
| if(MesswertRoll > MAX_SENSOR) MesswertRoll = MAX_SENSOR; |
| if(MesswertRoll < -MAX_SENSOR) MesswertRoll = -MAX_SENSOR; |
| if(MesswertGier > MAX_SENSOR) MesswertGier = MAX_SENSOR; |
| if(MesswertGier < -MAX_SENSOR) MesswertGier = -MAX_SENSOR; |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Höhenregelung |
| // Die Höhenregelung schwächt lediglich das Gas ab, erhöht es allerdings nicht |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(UBat > BattLowVoltageWarning) GasMischanteil = ((unsigned int)GasMischanteil * BattLowVoltageWarning) / UBat; // Gas auf das aktuelle Spannungvieveau beziehen |
| GasMischanteil *= STICK_GAIN; |
| |
| // if height control is activated |
| if((EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG) && !(Looping_Roll || Looping_Nick)) // Höhenregelung |
| { |
| #define HOOVER_GAS_AVERAGE 4096L // 4096 * 2ms = 8.2s averaging |
| #define HC_GAS_AVERAGE 4 // 4 * 2ms= 8ms averaging |
| #define OPA_OFFSET_STEP 10 |
| int HCGas, HeightDeviation; |
| static int HeightTrimming = 0; // rate for change of height setpoint |
| static int FilterHCGas = 0; |
| static int StickGasHoover = 120, HooverGas = 0, HooverGasMin = 0, HooverGasMax = 1023; |
| static unsigned long HooverGasFilter = 0; |
| static unsigned char delay = 100, BaroAtUpperLimit = 0, BaroAtLowerLimit = 0; |
| int CosAttitude; // for projection of hoover gas |
| |
| // get the current hooverpoint |
| // if(LoadHandler == 1) |
| { |
| DebugOut.Analog[21] = HooverGas; |
| DebugOut.Analog[18] = VarioMeter; |
| |
| // Expand the measurement |
| // measurement of air pressure close to upper limit and no overflow in correction of the new OCR0A value occurs |
| if(!BaroExpandActive) |
| { |
| if(MessLuftdruck > 920) |
| { // increase offset |
| if(OCR0A < (255 - OPA_OFFSET_STEP)) |
| { |
| ExpandBaro -= 1; |
| OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // increase offset to shift ADC down |
| beeptime = 300; |
| BaroExpandActive = 350; |
| } |
| else |
| { |
| BaroAtLowerLimit = 1; |
| } |
| } |
| // measurement of air pressure close to lower limit and |
| else |
| if(MessLuftdruck < 100) |
| { // decrease offset |
| if(OCR0A > OPA_OFFSET_STEP) |
| { |
| ExpandBaro += 1; |
| OCR0A = DruckOffsetSetting - OPA_OFFSET_STEP * ExpandBaro; // decrease offset to shift ADC up |
| beeptime = 300; |
| BaroExpandActive = 350; |
| } |
| else |
| { |
| BaroAtUpperLimit = 1; |
| } |
| } |
| else |
| { |
| BaroAtUpperLimit = 0; |
| BaroAtLowerLimit = 0; |
| } |
| } |
| else // delay, because of expanding the Baro-Range |
| { |
| // now clear the D-values |
| SummenHoehe = HoehenWert * SM_FILTER; |
| VarioMeter = 0; |
| BaroExpandActive--; |
| } |
| |
| // if height control is activated by an rc channel |
| if(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER) // Regler wird über Schalter gesteuert |
| { // check if parameter is less than activation threshold |
| if(Parameter_MaxHoehe < 50) // for 3 or 2-state switch height control is disabled in lowest position |
| { //height control not active |
| if(!delay--) |
| { |
| HoehenReglerAktiv = 0; // disable height control |
| SollHoehe = HoehenWert; // update SetPoint with current reading |
| delay = 1; |
| } |
| } |
| else |
| { //height control is activated |
| HoehenReglerAktiv = 1; // enable height control |
| delay = 200; |
| } |
| } |
| else // no switchable height control |
| { |
| SollHoehe = ((int16_t) ExternHoehenValue + (int16_t) Parameter_MaxHoehe) * (int)EE_Parameter.Hoehe_Verstaerkung; |
| HoehenReglerAktiv = 1; |
| } |
| |
| // calculate cos of nick and roll angle used for projection of the vertical hoover gas |
| tmp_int = (int)(IntegralNick/GIER_GRAD_FAKTOR); // nick angle in deg |
| tmp_int2 = (int)(IntegralRoll/GIER_GRAD_FAKTOR); // roll angle in deg |
| CosAttitude = (int16_t)ihypot(tmp_int, tmp_int2); // phytagoras gives effective attitude angle in deg |
| LIMIT_MAX(CosAttitude, 60); // limit effective attitude angle |
| CosAttitude = c_cos_8192(CosAttitude); // cos of actual attitude |
| if(HoehenReglerAktiv && !(MikroKopterFlags & FLAG_NOTLANDUNG)) |
| { |
| #define HEIGHT_TRIM_UP 0x01 |
| #define HEIGHT_TRIM_DOWN 0x02 |
| static unsigned char HeightTrimmingFlag = 0x00; |
| |
| #define HEIGHT_CONTROL_STICKTHRESHOLD 15 |
| // Holger original version |
| // start of height control algorithm |
| // the height control is only an attenuation of the actual gas stick. |
| // I.e. it will work only if the gas stick is higher than the hover gas |
| // and the hover height will be allways larger than height setpoint. |
| if((EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) || !(EE_Parameter.GlobalConfig & CFG_HOEHEN_SCHALTER)) // Regler wird über Schalter gesteuert) |
| { // old version |
| HCGas = GasMischanteil; // take current stick gas as neutral point for the height control |
| HeightTrimming = 0; |
| } |
| else |
| { |
| // alternative height control |
| // PD-Control with respect to hoover point |
| // the thrust loss out of horizontal attitude is compensated |
| // the setpoint will be fine adjusted with the gas stick position |
| if(MikroKopterFlags & FLAG_FLY) // trim setpoint only when flying |
| { // gas stick is above hoover point |
| if(StickGas > (StickGasHoover + HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtUpperLimit) |
| { |
| if(HeightTrimmingFlag & HEIGHT_TRIM_DOWN) |
| { |
| HeightTrimmingFlag &= ~HEIGHT_TRIM_DOWN; |
| SollHoehe = HoehenWert; // update setpoint to current heigth |
| } |
| HeightTrimmingFlag |= HEIGHT_TRIM_UP; |
| HeightTrimming += abs(StickGas - (StickGasHoover + HEIGHT_CONTROL_STICKTHRESHOLD)); |
| } // gas stick is below hoover point |
| else if(StickGas < (StickGasHoover - HEIGHT_CONTROL_STICKTHRESHOLD) && !BaroAtLowerLimit ) |
| { |
| if(HeightTrimmingFlag & HEIGHT_TRIM_UP) |
| { |
| HeightTrimmingFlag &= ~HEIGHT_TRIM_UP; |
| SollHoehe = HoehenWert; // update setpoint to current heigth |
| } |
| HeightTrimmingFlag |= HEIGHT_TRIM_DOWN; |
| HeightTrimming -= abs(StickGas - (StickGasHoover - HEIGHT_CONTROL_STICKTHRESHOLD)); |
| } |
| else // Gas Stick in Hoover Range |
| { |
| if(HeightTrimmingFlag & (HEIGHT_TRIM_UP | HEIGHT_TRIM_DOWN)) |
| { |
| HeightTrimmingFlag &= ~(HEIGHT_TRIM_UP | HEIGHT_TRIM_DOWN); |
| HeightTrimming = 0; |
| SollHoehe = HoehenWert; // update setpoint to current height |
| if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 500; |
| } |
| } |
| // Trim height set point |
| if(abs(HeightTrimming) > 512) |
| { |
| SollHoehe += (HeightTrimming * EE_Parameter.Hoehe_Verstaerkung)/(5 * 512 / 2); // move setpoint |
| HeightTrimming = 0; |
| if(EE_Parameter.ExtraConfig & CFG2_VARIO_BEEP) beeptime = 75; |
| //update hoover gas stick value when setpoint is shifted |
| if(!EE_Parameter.Hoehe_StickNeutralPoint) |
| { |
| StickGasHoover = HooverGas/STICK_GAIN; //rescale back to stick value |
| StickGasHoover = (StickGasHoover * UBat) / BattLowVoltageWarning; |
| if(StickGasHoover < 70) StickGasHoover = 70; |
| else if(StickGasHoover > 150) StickGasHoover = 150; |
| } |
| } |
| if(BaroExpandActive) SollHoehe = HoehenWert; // update setpoint to current altitude if Expanding is active |
| } //if MikroKopterFlags & MKFLAG_FLY |
| else |
| { |
| SollHoehe = HoehenWert - 400; |
| if(EE_Parameter.Hoehe_StickNeutralPoint) StickGasHoover = EE_Parameter.Hoehe_StickNeutralPoint; |
| else StickGasHoover = 120; |
| } |
| HCGas = HooverGas; // take hoover gas (neutral point) |
| } |
| |
| if(HoehenWert > SollHoehe || !(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT)) |
| { |
| // ------------------------- P-Part ---------------------------- |
| HeightDeviation = (int)(HoehenWert - SollHoehe); // positive when too high |
| tmp_int = (HeightDeviation * (int)Parameter_Hoehe_P) / 16; // p-part |
| HCGas -= tmp_int; |
| // ------------------------- D-Part 1: Vario Meter ---------------------------- |
| tmp_int = VarioMeter / 8; |
| if(tmp_int > 8) tmp_int = 8; // limit quadratic part on upward movement to avoid to much gas reduction |
| if(tmp_int > 0) tmp_int = VarioMeter + (tmp_int * tmp_int) / 4; |
| else tmp_int = VarioMeter - (tmp_int * tmp_int) / 4; |
| tmp_int = (Parameter_Luftdruck_D * (long)(tmp_int)) / 128L; // scale to d-gain parameter |
| LIMIT_MIN_MAX(tmp_int, -127, 255); |
| HCGas -= tmp_int; |
| // ------------------------ D-Part 2: ACC-Z Integral ------------------------ |
| tmp_int = ((Mess_Integral_Hoch / 128) * (long) Parameter_Hoehe_ACC_Wirkung) / (128 / STICK_GAIN); |
| LIMIT_MIN_MAX(tmp_int, -127, 255); |
| HCGas -= tmp_int; |
| |
| // limit deviation from hoover point within the target region |
| if( (abs(HeightDeviation) < 150) && (!HeightTrimming) && (HooverGas > 0)) // height setpoint is not changed and hoover gas not zero |
| { |
| LIMIT_MIN_MAX(HCGas, HooverGasMin, HooverGasMax); // limit gas around the hoover point |
| } |
| |
| if(BaroExpandActive) HCGas = HooverGas; |
| // ------------------------ D-Part 3: GpsZ ---------------------------------- |
| tmp_int = (Parameter_Hoehe_GPS_Z * (long)FromNaviCtrl_Value.GpsZ)/128L; |
| LIMIT_MIN_MAX(tmp_int, -127, 255); |
| HCGas -= tmp_int; |
| |
| // strech control output by inverse attitude projection 1/cos |
| // + 1/cos(angle) ++++++++++++++++++++++++++ |
| tmp_long2 = (int32_t)HCGas; |
| tmp_long2 *= 8192L; |
| tmp_long2 /= CosAttitude; |
| HCGas = (int16_t)tmp_long2; |
| // update height control gas averaging |
| FilterHCGas = (FilterHCGas * (HC_GAS_AVERAGE - 1) + HCGas) / HC_GAS_AVERAGE; |
| // limit height control gas pd-control output |
| LIMIT_MIN_MAX(FilterHCGas, EE_Parameter.Hoehe_MinGas * STICK_GAIN, (MAX_GAS - 20) * STICK_GAIN); |
| // set GasMischanteil to HeightControlGasFilter |
| if(EE_Parameter.ExtraConfig & CFG2_HEIGHT_LIMIT) |
| { // old version |
| if(FilterHCGas > GasMischanteil) FilterHCGas = GasMischanteil; // nicht mehr als Gas |
| } |
| GasMischanteil = FilterHCGas; |
| } |
| }// EOF height control active |
| else // HC not active |
| { |
| //update hoover gas stick value when HC is not active |
| if(!EE_Parameter.Hoehe_StickNeutralPoint) |
| { |
| StickGasHoover = HooverGas/STICK_GAIN; // rescale back to stick value |
| StickGasHoover = (StickGasHoover * UBat) / BattLowVoltageWarning; |
| } |
| else StickGasHoover = EE_Parameter.Hoehe_StickNeutralPoint; |
| if(StickGasHoover < 70) StickGasHoover = 70; |
| else if(StickGasHoover > 150) StickGasHoover = 150; |
| FilterHCGas = GasMischanteil; |
| } |
| |
| // Hoover gas estimation by averaging gas control output on small z-velocities |
| // this is done only if height contol option is selected in global config and aircraft is flying |
| if((MikroKopterFlags & FLAG_FLY) && !(MikroKopterFlags & FLAG_NOTLANDUNG)) |
| { |
| if(HooverGasFilter == 0) HooverGasFilter = HOOVER_GAS_AVERAGE * (unsigned long)(GasMischanteil); // init estimation |
| if(abs(VarioMeter) < 100) // only on small vertical speed |
| { |
| tmp_long2 = (int32_t)GasMischanteil; // take current thrust |
| tmp_long2 *= CosAttitude; // apply attitude projection |
| tmp_long2 /= 8192; |
| |
| // average vertical projected thrust |
| if(modell_fliegt < 2000) // the first 4 seconds |
| { // reduce the time constant of averaging by factor of 8 to get much faster a stable value |
| HooverGasFilter -= HooverGasFilter/(HOOVER_GAS_AVERAGE/8L); |
| HooverGasFilter += 8L * tmp_long2; |
| } |
| else if(modell_fliegt < 4000) // the first 8 seconds |
| { // reduce the time constant of averaging by factor of 4 to get much faster a stable value |
| HooverGasFilter -= HooverGasFilter/(HOOVER_GAS_AVERAGE/4L); |
| HooverGasFilter += 4L * tmp_long2; |
| } |
| else if(modell_fliegt < 8000) // the first 16 seconds |
| { // reduce the time constant of averaging by factor of 2 to get much faster a stable value |
| HooverGasFilter -= HooverGasFilter/(HOOVER_GAS_AVERAGE/2L); |
| HooverGasFilter += 2L * tmp_long2; |
| } |
| else //later |
| { |
| HooverGasFilter -= HooverGasFilter/HOOVER_GAS_AVERAGE; |
| HooverGasFilter += tmp_long2; |
| } |
| HooverGas = (int16_t)(HooverGasFilter/HOOVER_GAS_AVERAGE); |
| if(EE_Parameter.Hoehe_HoverBand) |
| { |
| int16_t band; |
| band = HooverGas / EE_Parameter.Hoehe_HoverBand; // the higher the parameter the smaller the range |
| HooverGasMin = HooverGas - band; |
| HooverGasMax = HooverGas + band; |
| } |
| else |
| { // no limit |
| HooverGasMin = 0; |
| HooverGasMax = 1023; |
| } |
| } |
| } |
| } |
| //DebugOut.Analog[26] = HooverGasMax; |
| }// EOF ParamSet.GlobalConfig & CFG_HEIGHT_CONTROL |
| |
| // limit gas to parameter setting |
| LIMIT_MIN(GasMischanteil, (MIN_GAS + 10) * STICK_GAIN); |
| if(GasMischanteil > (MAX_GAS - 20) * STICK_GAIN) GasMischanteil = (MAX_GAS - 20) * STICK_GAIN; |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // all BL-Ctrl connected? |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(MissingMotor) |
| if(modell_fliegt > 1 && modell_fliegt < 50 && GasMischanteil > 0) |
| { |
| modell_fliegt = 1; |
| GasMischanteil = MIN_GAS; |
| } |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // + Mischer und PI-Regler |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| DebugOut.Analog[7] = GasMischanteil; |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Gier-Anteil |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| GierMischanteil = MesswertGier - sollGier * STICK_GAIN; // Regler für Gier |
| #define MIN_GIERGAS (40*STICK_GAIN) // unter diesem Gaswert trotzdem Gieren |
| if(GasMischanteil > MIN_GIERGAS) |
| { |
| if(GierMischanteil > (GasMischanteil / 2)) GierMischanteil = GasMischanteil / 2; |
| if(GierMischanteil < -(GasMischanteil / 2)) GierMischanteil = -(GasMischanteil / 2); |
| } |
| else |
| { |
| if(GierMischanteil > (MIN_GIERGAS / 2)) GierMischanteil = MIN_GIERGAS / 2; |
| if(GierMischanteil < -(MIN_GIERGAS / 2)) GierMischanteil = -(MIN_GIERGAS / 2); |
| } |
| tmp_int = MAX_GAS*STICK_GAIN; |
| if(GierMischanteil > ((tmp_int - GasMischanteil))) GierMischanteil = ((tmp_int - GasMischanteil)); |
| if(GierMischanteil < -((tmp_int - GasMischanteil))) GierMischanteil = -((tmp_int - GasMischanteil)); |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Nick-Achse |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| DiffNick = MesswertNick - StickNick; // Differenz bestimmen |
| if(IntegralFaktor) SummeNick += IntegralNickMalFaktor - StickNick; // I-Anteil bei Winkelregelung |
| else SummeNick += DiffNick; // I-Anteil bei HH |
| if(SummeNick > (STICK_GAIN * 16000L)) SummeNick = (STICK_GAIN * 16000L); |
| if(SummeNick < -(16000L * STICK_GAIN)) SummeNick = -(16000L * STICK_GAIN); |
| pd_ergebnis_nick = DiffNick + SummeNick / Ki; // PI-Regler für Nick |
| // Motor Vorn |
| tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
| if(pd_ergebnis_nick > tmp_int) pd_ergebnis_nick = tmp_int; |
| if(pd_ergebnis_nick < -tmp_int) pd_ergebnis_nick = -tmp_int; |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Roll-Achse |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| DiffRoll = MesswertRoll - StickRoll; // Differenz bestimmen |
| if(IntegralFaktor) SummeRoll += IntegralRollMalFaktor - StickRoll;// I-Anteil bei Winkelregelung |
| else SummeRoll += DiffRoll; // I-Anteil bei HH |
| if(SummeRoll > (STICK_GAIN * 16000L)) SummeRoll = (STICK_GAIN * 16000L); |
| if(SummeRoll < -(16000L * STICK_GAIN)) SummeRoll = -(16000L * STICK_GAIN); |
| pd_ergebnis_roll = DiffRoll + SummeRoll / Ki; // PI-Regler für Roll |
| tmp_int = (long)((long)Parameter_DynamicStability * (long)(GasMischanteil + abs(GierMischanteil)/2)) / 64; |
| if(pd_ergebnis_roll > tmp_int) pd_ergebnis_roll = tmp_int; |
| if(pd_ergebnis_roll < -tmp_int) pd_ergebnis_roll = -tmp_int; |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Universal Mixer |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| for(i=0; i<MAX_MOTORS; i++) |
| { |
| signed int tmp_int; |
| if(Mixer.Motor[i][0] > 0) |
| { |
| tmp_int = ((long)GasMischanteil * Mixer.Motor[i][0]) / 64L; |
| tmp_int += ((long)pd_ergebnis_nick * Mixer.Motor[i][1]) / 64L; |
| tmp_int += ((long)pd_ergebnis_roll * Mixer.Motor[i][2]) / 64L; |
| tmp_int += ((long)GierMischanteil * Mixer.Motor[i][3]) / 64L; |
| tmp_motorwert[i] = MotorSmoothing(tmp_int,tmp_motorwert[i]); // Filter |
| tmp_int = tmp_motorwert[i] / STICK_GAIN; |
| CHECK_MIN_MAX(tmp_int,MIN_GAS,MAX_GAS); |
| Motor[i] = tmp_int; |
| } |
| else Motor[i] = 0; |
| } |
| /* |
| if(Poti1 > 20) Motor1 = 0; |
| if(Poti1 > 90) Motor6 = 0; |
| if(Poti1 > 140) Motor2 = 0; |
| //if(Poti1 > 200) Motor7 = 0; |
| */ |
| } |