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| // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // + 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 und 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 Medien veröffentlicht werden, muss unsere Webseite "http://www.mikrokopter.de" |
| // + eindeutig als Ursprung verlinkt und genannt 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" |
| |
| |
| unsigned char PlatinenVersion = 10; |
| unsigned char SendVersionToNavi = 1; |
| unsigned char BattLowVoltageWarning = 94; |
| unsigned int FlugMinuten = 0,FlugMinutenGesamt = 0; |
| unsigned int FlugSekunden = 0; |
| pVoidFnct_pVoidFnctChar_const_fmt _printf_P; |
| unsigned char FoundMotors = 0; |
| |
| void CalMk3Mag(void) |
| { |
| static unsigned char stick = 1; |
| if(PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] > -20) stick = 0; |
| if((PPM_in[EE_Parameter.Kanalbelegung[K_NICK]] < -70) && !stick) |
| { |
| stick = 1; |
| WinkelOut.CalcState++; |
| if(WinkelOut.CalcState > 4) |
| { |
| // WinkelOut.CalcState = 0; // in Uart.c |
| beeptime = 1000; |
| } |
| else Piep(WinkelOut.CalcState,150); |
| } |
| DebugOut.Analog[19] = WinkelOut.CalcState; |
| } |
| |
| |
| void LipoDetection(unsigned char print) |
| { |
| #define MAX_CELL_VOLTAGE 43 // max cell volatage for LiPO |
| unsigned int timer, cells; |
| if(print) printf("\n\rBatt:"); |
| if(EE_Parameter.UnterspannungsWarnung < 50) // automatische Zellenerkennung |
| { |
| timer = SetDelay(500); |
| if(print) while (!CheckDelay(timer)); |
| // up to 6s LiPo, less than 2s is technical impossible |
| for(cells = 2; cells < 7; cells++) |
| { |
| if(UBat < cells * MAX_CELL_VOLTAGE) break; |
| } |
| |
| BattLowVoltageWarning = cells * EE_Parameter.UnterspannungsWarnung; |
| if(print) |
| { |
| Piep(cells, 200); |
| printf(" %d Cells ", cells); |
| } |
| } |
| else BattLowVoltageWarning = EE_Parameter.UnterspannungsWarnung; |
| if(print) printf(" Low warning level: %d.%d",BattLowVoltageWarning/10,BattLowVoltageWarning%10); |
| } |
| |
| //############################################################################ |
| //Hauptprogramm |
| int main (void) |
| //############################################################################ |
| { |
| unsigned int timer,i,timer2 = 0, timerPolling; |
| |
| DDRB = 0x00; |
| PORTB = 0x00; |
| for(timer = 0; timer < 1000; timer++); // verzögern |
| #if (defined(__AVR_ATmega1284__) || defined(__AVR_ATmega1284P__)) |
| PlatinenVersion = 21; |
| #else |
| if(PINB & 0x01) |
| { |
| if(PINB & 0x02) PlatinenVersion = 13; |
| else PlatinenVersion = 11; |
| } |
| else |
| { |
| if(PINB & 0x02) PlatinenVersion = 20; |
| else PlatinenVersion = 10; |
| } |
| #endif |
| DDRC = 0x81; // SCL |
| DDRC |=0x40; // HEF4017 Reset |
| PORTC = 0xff; // Pullup SDA |
| DDRB = 0x1B; // LEDs und Druckoffset |
| PORTB = 0x01; // LED_Rot |
| DDRD = 0x3E; // Speaker & TXD & J3 J4 J5 |
| PORTD = 0x47; // LED |
| HEF4017R_ON; |
| MCUSR &=~(1<<WDRF); |
| WDTCSR |= (1<<WDCE)|(1<<WDE); |
| WDTCSR = 0; |
| |
| beeptime = 2500; |
| StickGier = 0; PPM_in[K_GAS] = 0; StickRoll = 0; StickNick = 0; |
| if(PlatinenVersion >= 20) GIER_GRAD_FAKTOR = 1220; else GIER_GRAD_FAKTOR = 1291; // unterschiedlich für ME und ENC |
| ROT_OFF; |
| |
| Timer_Init(); |
| TIMER2_Init(); |
| UART_Init(); |
| rc_sum_init(); |
| ADC_Init(); |
| I2C_Init(); |
| SPI_MasterInit(); |
| Capacity_Init(); |
| LIBFC_Init(); |
| GRN_ON; |
| sei(); |
| ParamSet_Init(); |
| |
| |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // + Check connected BL-Ctrls |
| // +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| // Check connected BL-Ctrls |
| BLFlags |= BLFLAG_READ_VERSION; |
| motor_read = 0; // read the first I2C-Data |
| SendMotorData(); |
| timer = SetDelay(500); |
| while(!(BLFlags & BLFLAG_TX_COMPLETE) && !CheckDelay(timer)); //wait for complete transfer |
| |
| printf("\n\rFound BL-Ctrl: "); |
| timer = SetDelay(4000); |
| for(i=0; i < MAX_MOTORS; i++) |
| { |
| SendMotorData(); |
| while(!(BLFlags & BLFLAG_TX_COMPLETE) && !CheckDelay(timer)); //wait for complete transfer |
| if(Mixer.Motor[i][0] > 0) // wait max 4 sec for the BL-Ctrls to wake up |
| { |
| while(!CheckDelay(timer) && !(Motor[i].State & MOTOR_STATE_PRESENT_MASK) ) |
| { |
| SendMotorData(); |
| while(!(BLFlags & BLFLAG_TX_COMPLETE) && !CheckDelay(timer)); //wait for complete transfer |
| } |
| } |
| if(Motor[i].State & MOTOR_STATE_PRESENT_MASK) |
| { |
| printf("%d",i+1); |
| FoundMotors++; |
| // if(Motor[i].Version & MOTOR_STATE_NEW_PROTOCOL_MASK) printf("(new) "); |
| } |
| } |
| for(i=0; i < MAX_MOTORS; i++) |
| { |
| if(!(Motor[i].State & MOTOR_STATE_PRESENT_MASK) && Mixer.Motor[i][0] > 0) |
| { |
| printf("\n\r\n\r!! MISSING BL-CTRL: %d !!",i+1); |
| ServoActive = 2; // just in case the FC would be used as camera-stabilizer |
| } |
| Motor[i].State &= ~MOTOR_STATE_ERROR_MASK; // clear error counter |
| } |
| printf("\n\r==================================="); |
| |
| if(RequiredMotors < FoundMotors) VersionInfo.HardwareError[1] |= DEFEKT_MIXER_ERR; |
| |
| //if(EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG) |
| { |
| printf("\n\rCalibrating pressure sensor.."); |
| timer = SetDelay(1000); |
| SucheLuftruckOffset(); |
| while (!CheckDelay(timer)); |
| printf("OK\n\r"); |
| } |
| |
| SetNeutral(0); |
| |
| ROT_OFF; |
| |
| beeptime = 2000; |
| ExternControl.Digital[0] = 0x55; |
| |
| |
| FlugMinuten = (unsigned int)GetParamByte(PID_FLIGHT_MINUTES) * 256 + (unsigned int)GetParamByte(PID_FLIGHT_MINUTES + 1); |
| FlugMinutenGesamt = (unsigned int)GetParamByte(PID_FLIGHT_MINUTES_TOTAL) * 256 + (unsigned int)GetParamByte(PID_FLIGHT_MINUTES_TOTAL + 1); |
| |
| if((FlugMinutenGesamt == 0xFFFF) || (FlugMinuten == 0xFFFF)) |
| { |
| FlugMinuten = 0; |
| FlugMinutenGesamt = 0; |
| } |
| printf("\n\rFlight-time %u min Total:%u min", FlugMinuten, FlugMinutenGesamt); |
| |
| printf("\n\rControl: "); |
| if (EE_Parameter.GlobalConfig & CFG_HEADING_HOLD) printf("HeadingHold"); |
| else printf("Normal (ACC-Mode)"); |
| |
| LcdClear(); |
| I2CTimeout = 5000; |
| WinkelOut.Orientation = 1; |
| LipoDetection(1); |
| |
| LIBFC_ReceiverInit(EE_Parameter.Receiver); |
| |
| printf("\n\r===================================\n\r"); |
| //SpektrumBinding(); |
| timer = SetDelay(2000); |
| timerPolling = SetDelay(250); |
| |
| Debug(ANSI_CLEAR "FC-Start!\n\rFlugzeit: %d min", FlugMinutenGesamt); // Note: this won't waste flash memory, if #DEBUG is not active |
| DebugOut.Status[0] = 0x01 | 0x02; |
| |
| while (1) |
| { |
| if(CheckDelay(timerPolling)) |
| { |
| timerPolling = SetDelay(100); |
| LIBFC_Polling(); |
| } |
| if(UpdateMotor && AdReady) // ReglerIntervall |
| { |
| UpdateMotor=0; |
| if(WinkelOut.CalcState) CalMk3Mag(); |
| else MotorRegler(); |
| SendMotorData(); |
| ROT_OFF; |
| if(SenderOkay) { SenderOkay--; VersionInfo.HardwareError[1] &= ~DEFEKT_PPM_ERR; } |
| else |
| { |
| TIMSK1 |= _BV(ICIE1); // enable PPM-Input |
| PPM_in[0] = 0; // set RSSI to zero on data timeout |
| VersionInfo.HardwareError[1] |= DEFEKT_PPM_ERR; |
| } |
| //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| //if(HoehenReglerAktiv && NaviDataOkay && SenderOkay < 160 && SenderOkay > 10 && FromNaviCtrl_Value.SerialDataOkay > 220) SenderOkay = 160; |
| //if(HoehenReglerAktiv && NaviDataOkay && SenderOkay < 101 && SenderOkay > 10 && FromNaviCtrl_Value.SerialDataOkay > 1) SenderOkay = 101; |
| //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
| if(!--I2CTimeout || MissingMotor) |
| { |
| if(!I2CTimeout) |
| { |
| I2C_Reset(); |
| I2CTimeout = 5; |
| DebugOut.Analog[28]++; // I2C-Error |
| FCFlags |= FCFLAG_I2CERR; |
| VersionInfo.HardwareError[1] |= DEFEKT_I2C; |
| DebugOut.Status[1] |= 0x02; // BL-Error-Status |
| } |
| if((BeepMuster == 0xffff) && MotorenEin) |
| { |
| beeptime = 10000; |
| BeepMuster = 0x0080; |
| } |
| } |
| else |
| { |
| ROT_OFF; |
| if(!beeptime) |
| { |
| FCFlags &= ~FCFLAG_I2CERR; |
| } |
| } |
| if(!UpdateMotor) |
| { |
| DatenUebertragung(); |
| BearbeiteRxDaten(); |
| if(CheckDelay(timer)) |
| { |
| static unsigned char second; |
| timer += 20; // 20 ms interval |
| if(MissingMotor) |
| { |
| VersionInfo.HardwareError[1] |= DEFEKT_BL_MISSING; |
| DebugOut.Status[1] |= 0x02; // BL-Error-Status |
| } |
| else |
| { |
| VersionInfo.HardwareError[1] &= ~DEFEKT_BL_MISSING; |
| if(I2CTimeout > 6) DebugOut.Status[1] &= ~0x02; // BL-Error-Status |
| } |
| |
| if(I2CTimeout > 6) VersionInfo.HardwareError[1] &= ~DEFEKT_I2C; |
| |
| if(PcZugriff) PcZugriff--; |
| else |
| { |
| ExternControl.Config = 0; |
| ExternStickNick = 0; |
| ExternStickRoll = 0; |
| ExternStickGier = 0; |
| if(BeepMuster == 0xffff && SenderOkay == 0) |
| { |
| beeptime = 15000; |
| BeepMuster = 0x0c00; |
| } |
| } |
| if(NaviDataOkay > 200) |
| { |
| NaviDataOkay--; |
| FCFlags &= ~FCFLAG_SPI_RX_ERR; |
| VersionInfo.HardwareError[1] &= ~DEFEKT_SPI_RX_ERR; |
| } |
| else |
| { |
| if(NC_Version.Compatible) |
| { |
| FCFlags |= FCFLAG_SPI_RX_ERR; |
| VersionInfo.HardwareError[1] |= DEFEKT_SPI_RX_ERR; |
| if(BeepMuster == 0xffff && MotorenEin) |
| { |
| beeptime = 15000; |
| BeepMuster = 0xA800; |
| } |
| } |
| GPS_Nick = 0; |
| GPS_Roll = 0; |
| //if(!beeptime) |
| FromNaviCtrl.CompassValue = -1; |
| NaviDataOkay = 0; |
| } |
| if(UBat < BattLowVoltageWarning) |
| { |
| FCFlags |= FCFLAG_LOWBAT; |
| if(BeepMuster == 0xffff) |
| { |
| beeptime = 6000; |
| BeepMuster = 0x0300; |
| } |
| } |
| else if(!beeptime) FCFlags &= ~FCFLAG_LOWBAT; |
| |
| SPI_StartTransmitPacket(); |
| SendSPI = 4; |
| if(!MotorenEin) timer2 = 1450; // 0,5 Minuten aufrunden |
| else |
| if(++second == 49) |
| { |
| second = 0; |
| FlugSekunden++; |
| } |
| if(++timer2 == 2930) // eine Minute |
| { |
| timer2 = 0; |
| FlugMinuten++; |
| FlugMinutenGesamt++; |
| SetParamByte(PID_FLIGHT_MINUTES,FlugMinuten / 256); |
| SetParamByte(PID_FLIGHT_MINUTES+1,FlugMinuten % 256); |
| SetParamByte(PID_FLIGHT_MINUTES_TOTAL,FlugMinutenGesamt / 256); |
| SetParamByte(PID_FLIGHT_MINUTES_TOTAL+1,FlugMinutenGesamt % 256); |
| timer = SetDelay(20); // falls "timer += 20;" mal nicht geht |
| } |
| } |
| LED_Update(); |
| Capacity_Update(); |
| } |
| } |
| if(!SendSPI) { SPI_TransmitByte(); } |
| } |
| return (1); |
| } |
| |
| |