Subversion Repositories FlightCtrl

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/branches/V0.76g_dk9nw_balancekopter/main.c
0,0 → 1,491
/**************************************************************************************************************************************
* File: main.c
*
* Purpose: main function fot Flight Ctrl
*
* Functions: void CalMk3Mag(void)
* void LipoDetection(unsigned char print)
* int main(void)
*
* hardware: Flight Ctrl V1.3
*
* Created: Feb 2013
*
* Revisions: 1.00 experimental subversion for a balancekopter
* Achtung: nicht flugfähige Experimentalversion für eine Balenwaage mit Flight-CTRL
* siehe: http://forum.mikrokopter.de/topic-39231.html
*
* Copyright: (c)2013 www.mikrokopter.de
* All rights reserved. This software is available only for non-commercial or educational applications.
* Other uses are prohibited. This software may be modified only if
* the resulting code be made available publicly and the original author(s) given credit.
*
************************************************************************************************************************************/
// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// + 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 = 13;
unsigned char SendVersionToNavi = 1;
unsigned char BattLowVoltageWarning = 94;
unsigned int FlugMinuten = 0,FlugMinutenGesamt = 0;
 
 
 
//-----------------------------------------------------------------------------------------------------
// calibrate magnetic compass
//-----------------------------------------------------------------------------------------------------
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)
{
beeptime = 1000;
}
else Piep(WinkelOut.CalcState,150);
}
DebugOut.Analog[19] = WinkelOut.CalcState;
}
//-----------------------------------------------------------------------------------------------------
 
 
 
//-----------------------------------------------------------------------------------------------------
// recognize the LiPo accumulators
// char print can be 0 or 1
//-----------------------------------------------------------------------------------------------------
void LipoDetection(unsigned char print)
{
unsigned int timer;
if(print) printf("\n\rBatt:");
if(EE_Parameter.UnterspannungsWarnung < 50) // automatic recognition of lipo cells -> default = 33
{
timer = SetDelay(500); //
if(print) while (!CheckDelay(timer));
if(UBat < 130)
{
BattLowVoltageWarning = 3 * EE_Parameter.UnterspannungsWarnung;
if(print)
{
Piep(3,200);
printf(" 3 Cells ");
}
}
else
{
BattLowVoltageWarning = 4 * EE_Parameter.UnterspannungsWarnung;
if(print)
{
Piep(4,200);
printf(" 4 Cells ");
}
}
}
else BattLowVoltageWarning = EE_Parameter.UnterspannungsWarnung;
 
if(print) printf(" Low warning level: %d.%d",BattLowVoltageWarning/10,BattLowVoltageWarning%10);
}
//-----------------------------------------------------------------------------------------------------
 
 
 
// --------------------------------------------------------------------------------------------------------------------------
// main program starting here
//
// INPUT: None
// OUTPUT: None
// RETURN: 1
// --------------------------------------------------------------------------------------------------------------------------
int main(void)
{
unsigned int timer,i,timer2 = 0;
DDRB = 0x00;
PORTB = 0x00;
for(timer = 0; timer < 1000; timer++); // verzögern
PlatinenVersion = 13;
DDRC = 0x81; // SCL
PORTC = 0xFF; // Pullup SDA
DDRB = 0x1B; // LEDs und Druckoffset
PORTB = 0x01; // LED_Rot
DDRD = 0x3E; // Speaker & TXD & J3 J4 J5
PORTD = 0x47; // LED
HEF4017R_OFF; // #define HEF4017R_OFF PORTC &= ~(1<<PORTC6)
MCUSR &=~(1<<WDRF); // MCUSR – MCU Status Register provides information on which reset source caused an MCU reset
WDTCSR |= (1<<WDCE)|(1<<WDE); // WDTCSR – Watchdog Timer Control Register
WDTCSR = 0;
beeptime = 2000;
StickGier = 0; PPM_in[K_GAS] = 0; StickRoll = 0; StickNick = 0;
GIER_GRAD_FAKTOR = 1291;
ROT_OFF; // rote LED aus // PORTB |= 0x01;
Timer_Init(); // goto timer0.c Zeile 40
TIMER2_Init(); // goto timer0.c Zeile 170
UART_Init(); // goto uart.c Zeile 488
rc_sum_init(); // goto rc.c line 17
ADC_Init(); // goto analog.c Zeile 26
i2c_init(); // goto twimaster.c Zeile 16
//---------------------------------------------------------------------------------------------------------------------------------
// passes one time through the following code before arriving at the forever loop
//---------------------------------------------------------------------------------------------------------------------------------
sei();
printf("\n\r===================================");
printf("\n\rFlightControl\n\rHardware:%d.%d\n\rSoftware:V%d.%d%c ",PlatinenVersion/10,PlatinenVersion%10, VERSION_MAJOR, VERSION_MINOR,VERSION_PATCH + 'a');
printf("\n\rexperimental version");
printf("\n\r===================================");
 
GRN_ON; // switch green LED on // PORTB &=~0x02;
ReadParameterSet(3, (unsigned char *) &EE_Parameter.Kanalbelegung[0], 9); // read first 9 Bytes = chanal setup of radio control
 
// ---------------------------------------------------------------------------------------------------------------------------
// setup of mixer
// ---------------------------------------------------------------------------------------------------------------------------
 
// check MIXER-Revision at first EEPROM Byte = 1000 // #define EEPROM_ADR_MIXER_TABLE 1000
 
// if((eeprom_read_byte(&EEPromArray[EEPROM_ADR_MIXER_TABLE]) == MIXER_REVISION) && (eeprom_read_byte(&EEPromArray[EEPROM_ADR_VALID]) != 0xff))
if((eeprom_read_byte(&EEPromArray[1000]) == 1) && (eeprom_read_byte(&EEPromArray[1]) != 0xFF)) // aufgelöst
{
unsigned char i; // Settings via Koptertool zurücksetzen
RequiredMotors = 0;
eeprom_read_block(&Mixer, &EEPromArray[EEPROM_ADR_MIXER_TABLE], sizeof(Mixer));
for(i=0; i<16;i++) { if(Mixer.Motor[i][0] > 0) RequiredMotors++;}
}
else // default
{
unsigned char i;
printf("\n\rerzeugt default Mixer Table");
for(i=0; i<16;i++) { Mixer.Motor[i][0] = 0;Mixer.Motor[i][1] = 0;Mixer.Motor[i][2] = 0;Mixer.Motor[i][3] = 0;};
// default = Quadro
// number 64 is equivalent to 100%
// GasMischanteil pd_ergebnis_nick pd_ergebnis_roll GierMischanteil
Mixer.Motor[0][0] = 64; Mixer.Motor[0][1] = +64; Mixer.Motor[0][2] = 0; Mixer.Motor[0][3] = +64; // vorne
Mixer.Motor[1][0] = 64; Mixer.Motor[1][1] = -64; Mixer.Motor[1][2] = 0; Mixer.Motor[1][3] = +64; // hinten
Mixer.Motor[2][0] = 64; Mixer.Motor[2][1] = 0; Mixer.Motor[2][2] = -64; Mixer.Motor[2][3] = -64; // rechts
Mixer.Motor[3][0] = 64; Mixer.Motor[3][1] = 0; Mixer.Motor[3][2] = +64; Mixer.Motor[3][3] = -64; // links
Mixer.Revision = MIXER_REVISION; // #define MIXER_REVISION 1
memcpy(Mixer.Name, "Quadro\0", 11);
eeprom_write_block(&Mixer, &EEPromArray[EEPROM_ADR_MIXER_TABLE], sizeof(Mixer)); // sizeof(Mixer) = 77
}
printf("\n\rMixer-Config: '%s' (%u Motors)",Mixer.Name,RequiredMotors);
// ---------------------------------------------------------------------------------------------------------------------------
// how many BL-Ctrls are connected ?
// ---------------------------------------------------------------------------------------------------------------------------
printf("\n\r...BL-Ctrl....");
motorread = 0;
UpdateMotor = 0;
SendMotorData();
while(!UpdateMotor);
motorread = 0; // read the first I2C-Datasets
timer = SetDelay(2000); // sets
for(i=0; i < MAX_MOTORS; i++) // #define MAX_MOTORS 4
{
UpdateMotor = 0;
SendMotorData(); // goto fc.c line 460
while(!UpdateMotor);
if(Mixer.Motor[i][0] > 0) // wait maximum 2 sec to wake up the BL-Ctrls
{
while(!CheckDelay(timer) && !MotorPresent[i])
{
UpdateMotor = 0;
SendMotorData();
while(!UpdateMotor);
}
}
if(MotorPresent[i]) printf("%d ",i+1);
}
for(i=0; i < MAX_MOTORS; i++)
{
if(!MotorPresent[i] && Mixer.Motor[i][0] > 0) // #define MAX_MOTORS 4
{
printf("\n\r\n\r!! missing BL-CTRL: %d !!",i+1);
ServoActive = 1; // just in case the FlightCtrl would be used as camera-stabilizer
}
MotorError[i] = 0;
}
printf("\n\r===================================");
SendMotorData();
 
// ---------------------------------------------------------------------------------------------------------------------------
// check, that the revision in EEPROM fits to actual software
// ---------------------------------------------------------------------------------------------------------------------------
if(eeprom_read_byte(&EEPromArray[EEPROM_ADR_VALID]) != EE_DATENREVISION) // #define EEPROM_ADR_VALID 1
{ // #define EE_DATENREVISION 80
DefaultKonstanten1(); // Funktion aus eeprom.c
printf("\n\rInit. EEPROM");
for (unsigned char i=1;i<6;i++) // es gibt 5 verschiedene Settings
{
if(i==2) DefaultKonstanten2(); // Kamera
if(i==3) DefaultKonstanten3(); // Anfänger
if(i>3) DefaultKonstanten2(); // Kamera
// ---------------------------------------------------------------------------------------------------------------------------
// valid Setting ?
// ---------------------------------------------------------------------------------------------------------------------------
if(eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS]) < 12 && eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS+1]) < 12 && eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS+2]) < 12 && eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS+3]) < 12)
{
EE_Parameter.Kanalbelegung[0] = eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS+0]); // Nick // #define EEPROM_ADR_CHANNELS 80
EE_Parameter.Kanalbelegung[1] = eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS+1]); // Roll
EE_Parameter.Kanalbelegung[2] = eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS+2]); // Gas
EE_Parameter.Kanalbelegung[3] = eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS+3]); // Gier
EE_Parameter.Kanalbelegung[4] = eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS+4]); // Poti 1
EE_Parameter.Kanalbelegung[5] = eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS+5]); // Poti 2
EE_Parameter.Kanalbelegung[6] = eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS+6]); // Poti 3
EE_Parameter.Kanalbelegung[7] = eeprom_read_byte(&EEPromArray[EEPROM_ADR_CHANNELS+7]); // Poti 4
if(i==1) printf(": Generating Default-Parameter using old Stick Settings");
} else DefaultStickMapping();
WriteParameterSet(i, (unsigned char *) &EE_Parameter.Kanalbelegung[0], STRUCT_PARAM_LAENGE); // #define STRUCT_PARAM_LAENGE sizeof(EE_Parameter)
// WriteParameterSet(i, (unsigned char *) &EE_Parameter.Kanalbelegung[0], 101));
}
SetActiveParamSetNumber(3); // default Setting ist Beginner
eeprom_write_byte(&EEPromArray[EEPROM_ADR_VALID], EE_DATENREVISION); // #define EE_DATENREVISION 80
// eeprom_write_byte(&EEPromArray[1], 80); // aufgelöst
} // EOF : check existing revision at EEPROM
FlugMinuten = (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_MINUTES2]) * 256 + (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_MINUTES2+1]);
FlugMinutenGesamt = (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_MINUTES]) * 256 + (int)eeprom_read_byte(&EEPromArray[EEPROM_ADR_MINUTES+1]);
if(FlugMinutenGesamt == 0xFFFF || FlugMinuten == 0xFFFF) // Flugminuten sind am überlaufen - zurücksetzen
{
FlugMinuten = 0;
FlugMinutenGesamt = 0;
}
printf("\n\rFlight-time %u min Total:%u min" ,FlugMinuten,FlugMinutenGesamt);
if(eeprom_read_byte(&EEPromArray[EEPROM_ADR_ACC_NICK]) > 4)
{
printf("\n\rACC noch nicht calibriert !");
}
ReadParameterSet(GetActiveParamSetNumber(), (unsigned char *) &EE_Parameter.Kanalbelegung[0], STRUCT_PARAM_LAENGE); // #define STRUCT_PARAM_LAENGE sizeof(EE_Parameter)
printf("\n\rUsing parameterset %d", GetActiveParamSetNumber());
if(EE_Parameter.GlobalConfig & CFG_HOEHENREGELUNG)
{
printf("\n\rKalibrieren des Drucksensors.");
timer = SetDelay(1000); //
SucheLuftruckOffset();
while (!CheckDelay(timer)); // pause 1 sec
printf("OK\n\r");
}
SetNeutral(); // Nullwerte ermitteln und Startwerte festlegen - goto fc.c line 162
ROT_OFF; // redLED off // PORTB |= 0x01;
beeptime = 2000;
ExternControl.Digital[0] = 0x55; // externe Steuerung per serieller Schnittstelle - siehe uart.h
printf("\n\rControl: ");
if (EE_Parameter.GlobalConfig & CFG_HEADING_HOLD) printf("HeadingHold");
else printf("normaler (ACC-Mode)");
LcdClear();
I2CTimeout = 5000; // watchdog set up to 10 sec
WinkelOut.Orientation = 1;
LipoDetection(1); // Lipos should be detected now
printf("\n\r===================================\n\r");
timer = SetDelay(2000);
// -------------------------------- end of main() prelude ---------------------------------------------------------------------
 
 
 
//----------------------------------------------------------------------------------------------------------------------
// forever loop of main program
//----------------------------------------------------------------------------------------------------------------------
while(1)
{
if(UpdateMotor && AdReady) // motor is updated every 2 ms and ADC is already passed
{
UpdateMotor=0; // reset and wait fpr the next 2ms timed trigger from timer0 IR
if(WinkelOut.CalcState) CalMk3Mag(); // In diesem Spezial-Fall soll der Kompass kalibriert werden
else MotorRegler(); // Im Normalfall Sollwerte für die Motoren berechnen = goto fc.c line 541
SendMotorData(); // Sollwerte an die Motorren senden -> fc.c Zeile 465
ROT_OFF; // switch red LED off // PORTB |= 0x01;
if(SenderOkay) SenderOkay--; // ICIE1: Timer/Counter1, Input Capture Interrupt Enable
else TIMSK1 |= _BV(ICIE1); // enable PPM-Input // TIMSK1 – Timer/Counter1 Interrupt Mask Register -> – – ICIE1 – – OCIE1B OCIE1A TOIE1
if(!--I2CTimeout || MissingMotor) // counting down I2CTimeout or motor is missing
{
if(!I2CTimeout)
{
i2c_reset();
I2CTimeout = 5;
DebugOut.Analog[28]++; // I2C-Error
}
if((BeepMuster == 0xffff) && MotorenEin)
{
beeptime = 10000;
BeepMuster = 0x0080;
}
}
else
{
ROT_OFF; // switch red LED off // PORTB |= 0x01;
}
if( 1 && (!UpdateMotor || !MotorenEin))
{
DatenUebertragung();
BearbeiteRxDaten();
}
else BearbeiteRxDaten();
// DatenUebertragung(); // where ist that contained?
// BearbeiteRxDaten(); // where ist that contained?
if(CheckDelay(timer)) // goto timer0.c line 65
{
timer += 20;
if(PcZugriff) PcZugriff--; // flight-CTRL controlled by external PC
else
{
ExternControl.Config = 0;
ExternStickNick = 0;
ExternStickRoll = 0;
ExternStickGier = 0;
if(BeepMuster == 0xffff && SenderOkay == 0)
{
beeptime = 15000;
BeepMuster = 0x0c00;
}
}
if(UBat < BattLowVoltageWarning) // low battery
{
MikroKopterFlags |= FLAG_LOWBAT;
if(BeepMuster == 0xffff)
{
beeptime = 6000;
BeepMuster = 0x0300;
}
}
else MikroKopterFlags &= ~FLAG_LOWBAT;
//SPI_StartTransmitPacket(); // where ist that contained?
SendSPI = 4;
if(!MotorenEin) timer2 = 1450; // round it up to 30 sec
if(++timer2 == 2930) // one minute
{
timer2 = 0;
FlugMinuten++;
FlugMinutenGesamt++;
eeprom_write_byte(&EEPromArray[EEPROM_ADR_MINUTES2],FlugMinuten / 256);
eeprom_write_byte(&EEPromArray[EEPROM_ADR_MINUTES2+1],FlugMinuten % 256);
eeprom_write_byte(&EEPromArray[EEPROM_ADR_MINUTES],FlugMinutenGesamt / 256);
eeprom_write_byte(&EEPromArray[EEPROM_ADR_MINUTES+1],FlugMinutenGesamt % 256);
timer = SetDelay(20); // delay 20 ms
}
}
LED_Update(); // junmps erery 2ms to led.c line 32
} // *** EOF : if(UpdateMotor && AdReady)
// *** EOF: if(!SendSPI) { SPI_TransmitByte(); }
} // End of endlessloop
return (1);
}
// *** EOF: main(void) ************************************************************************************************************