Subversion Repositories FlightCtrl

// ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++

// + Copyright (c) 04.2007 Holger Buss

// + Nur für den privaten Gebrauch

// + 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 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 to systems other than 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 <avr/boot.h>

#include <avr/io.h>

#include <avr/interrupt.h>

#include <util/delay.h>

#include "timer0.h"

#include "timer2.h"

#include "uart0.h"

#include "uart1.h"

#include "output.h"

#include "menu.h"

#include "attitude.h"

#include "flight.h"

#include "controlMixer.h"

#include "rc.h"

#include "analog.h"

#include "configuration.h"

#include "printf_P.h"

#include "twimaster.h"

#ifdef USE_NAVICTRL

#include "spi.h"

#endif

#ifdef USE_MK3MAG

#include "mk3mag.h"

#endif

#include "eeprom.h"

int16_t main (void) {

  uint16_t timer;

  // disable interrupts global

  cli();

  // analyze hardware environment

  CPUType = getCPUType();

  BoardRelease = getBoardRelease();

  // disable watchdog

  MCUSR &=~(1<<WDRF);

  WDTCSR |= (1<<WDCE)|(1<<WDE);

  WDTCSR = 0;

  // PPM_in[CH_THROTTLE] = 0;

  // Why??? They are already initialized to 0.

  // stickPitch = stickRoll = stickYaw = 0;

  RED_OFF;

  // initalize modules

  output_init();

  timer0_init();

  timer2_init();

  USART0_Init();

  if(CPUType == ATMEGA644P) USART1_Init();

  RC_Init();

  analog_init();

  I2C_init();

#ifdef USE_NAVICTRL

  SPI_MasterInit();

#endif

#ifdef USE_MK3MAG

  MK3MAG_Init();

#endif

  // enable interrupts global

  sei();

  printf("\n\r===================================");

  printf("\n\rFlightControl");

  printf("\n\rHardware: Custom");

  printf("\r\n     CPU: Atmega644");

  if(CPUType == ATMEGA644P)

    printf("p");

  printf("\n\rSoftware: V%d.%d%c",VERSION_MAJOR, VERSION_MINOR, VERSION_PATCH + 'a');

  printf("\n\r===================================");

  // Parameter Set handling

  ParamSet_Init();

  // Wait for a short time (otherwise the RC channel check won't work below)

  // timer = SetDelay(500);

  // while(!CheckDelay(timer));

  // Instead, while away the time by flashing the 2 outputs:

  // First J16, then J17. Makes it easier to see which is which.

  timer = SetDelay(200);

  J16_ON;

  GRN_OFF;

  RED_ON;

  while(!CheckDelay(timer));

  timer = SetDelay(200);

  J16_OFF;

  RED_OFF;

  GRN_ON;

  J17_ON;

  while(!CheckDelay(timer));

  timer = SetDelay(200);

  while(!CheckDelay(timer));

  J17_OFF;

  twi_diagnostics();

  printf("\n\r===================================");

  /*

  if(staticParams.GlobalConfig & CFG_HEIGHT_CONTROL)

    {

      printf("\n\rCalibrating air pressure sensor..");

      timer = SetDelay(1000);

      SearchAirPressureOffset();

      while (!CheckDelay(timer));

      printf("OK\n\r");

    }

  */

#ifdef USE_NAVICTRL

  printf("\n\rSupport for NaviCtrl");

#ifdef USE_RC_DSL

  printf("\r\nSupport for DSL RC at 2nd UART");

#endif

#ifdef USE_RC_SPECTRUM

  printf("\r\nSupport for SPECTRUM RC at 2nd UART");

#endif

#endif

#ifdef USE_MK3MAG

  printf("\n\rSupport for MK3MAG Compass");

#endif

#if (defined (USE_MK3MAG))

  if(CPUType == ATMEGA644P) printf("\n\rSupport for GPS at 2nd UART");

  else                      printf("\n\rSupport for GPS at 1st UART");

#endif

  controlMixer_setNeutral(0);

  // Cal. attitude sensors and reset integrals.

  attitude_setNeutral();

  Servo_On();

  // Init flight parameters

  flight_setNeutral();

  // RED_OFF;

  beep(2000);

  printf("\n\rControl: ");

  if (staticParams.GlobalConfig & CFG_HEADING_HOLD) printf("HeadingHold");

  else printf("Neutral (ACC-Mode)");

  printf("\n\n\r");

  LCD_Clear();

  I2CTimeout = 5000;

  while (1) {

    if(runFlightControl && analogDataReady) {      // control interval

      runFlightControl = 0; // reset Flag, is enabled every 2 ms by ISR of timer0

      J4HIGH;

      flight_control();

      J4LOW;

      sendMotorData(); // the flight control code

      RED_OFF;

      /*

        Does not belong here. Instead, external control should be ignored in

        controlMixer if there was no new data from there for some time.

      if(externalControlActive) externalControlActive--;

      else {

        externalControl.config = 0;

        externalStickPitch = 0;

        externalStickRoll = 0;

        externalStickYaw = 0;

      }

      */

      /*

        Does not belong here.

        if(RC_Quality)  RC_Quality--;

      */

      /* Does not belong here. Well since we are not supporting navi right now anyway, leave out.

#ifdef USE_NAVICTRL

      if(NCDataOkay) {

        if(--NCDataOkay == 0) // no data from NC

          {  // set gps control sticks neutral

            GPSStickPitch = 0;

            GPSStickRoll = 0;

            NCSerialDataOkay = 0;

          }

      }

#endif

      */

      if(!--I2CTimeout || missingMotor) { // try to reset the i2c if motor is missing ot timeout

        RED_ON;

        if(!I2CTimeout) {

          I2C_Reset();

          I2CTimeout = 5;

        }

      } else {

        RED_OFF;

      }

      // Allow Serial Data Transmit if motors must not updated or motors are not running

      if( !runFlightControl || !(MKFlags & MKFLAG_MOTOR_RUN)) {

        USART0_TransmitTxData();

      }

      USART0_ProcessRxData();

      if(CheckDelay(timer)) {

        if(UBat < staticParams.LowVoltageWarning) {

          beepBatteryAlarm();

        }

#ifdef USE_NAVICTRL

        SPI_StartTransmitPacket();

        SendSPI = 4;

#endif

        timer = SetDelay(20); // every 20 ms

      }

      output_update();

    }

#ifdef USE_NAVICTRL

    if(!SendSPI) {

      // SendSPI is decremented in timer0.c with a rate of 9.765 kHz.

      // within the SPI_TransmitByte() routine the value is set to 4.

      // I.e. the SPI_TransmitByte() is called at a rate of 9.765 kHz/4= 2441.25 Hz,

      // and therefore the time of transmission of a complete spi-packet (32 bytes) is 32*4/9.765 kHz = 13.1 ms.

      SPI_TransmitByte();

    }

#endif

  }

  return (1);

}