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 (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,

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

// + Werden Teile des Quellcodes (mit oder ohne Modifikation) weiterverwendet oder veröffentlicht,

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

// + 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 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.

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// +     clearly linked as origin

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// +  THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS"

// +  AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE

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

#include <stdlib.h>

#include "controlMixer.h"

#include "rc.h"

#include "heightControl.h"

#include "attitudeControl.h"

#include "externalControl.h"

#include "configuration.h"

#include "attitude.h"

#include "commands.h"

#include "output.h"

uint16_t maxControl[2] = {0,0};

int16_t control[2] = {0,0};

int16_t controlYaw = 0, controlThrottle = 0;

uint8_t looping = 0;

// Internal variables for reading commands made with an R/C stick.

uint8_t lastCommand  = COMMAND_NONE;

uint8_t lastArgument;

uint8_t isCommandRepeated = 0;

// MK flags. TODO: Replace by enum. State machine.

uint16_t isFlying = 0;

volatile uint8_t MKFlags = 0;

/*

 * This could be expanded to take arguments from ohter sources than the RC

 * (read: Custom MK RC project)

 */

uint8_t controlMixer_getArgument(void) {

  return lastArgument;

}

/*

 * This could be expanded to take calibrate / start / stop commands from ohter sources

 * than the R/C (read: Custom MK R/C project)

 */

uint8_t controlMixer_getCommand(void) {

  return lastCommand;

}

uint8_t controlMixer_isCommandRepeated(void) {

  return isCommandRepeated;

}

void controlMixer_setNeutral() {

  EC_setNeutral();

  HC_setGround();

}

/*

 * Set the potientiometer values to the momentary values of the respective R/C channels.

 * No slew rate limitation.

 */

void controlMixer_initVariables(void) {

  uint8_t i;

  for (i=0; i<8; i++) {

    variables[i] = RC_getVariable(i);

  }

}

/*

 * Update potentiometer values with limited slew rate. Could be made faster if desired.

 * TODO: It assumes R/C as source. Not necessarily true.

 */

void controlMixer_updateVariables(void) {

  uint8_t i;

  int16_t targetvalue;

  for (i=0; i<8; i++) {

    targetvalue = RC_getVariable(i);

    if (targetvalue < 0) targetvalue = 0;

    if (variables[i] < targetvalue && variables[i] < 255) variables[i]++; else if(variables[i] > 0 && variables[i] > targetvalue) variables[i]--;

  }

}

uint8_t controlMixer_getSignalQuality(void) {

  uint8_t rcQ = RC_getSignalQuality();

  uint8_t ecQ = EC_getSignalQuality();

  // This needs not be the only correct solution...

  return rcQ > ecQ ? rcQ : ecQ;

}

/*

 * Update the variables indicating stick position from the sum of R/C, GPS and external control.

 */

void controlMixer_update(void) {

  // calculate Stick inputs by rc channels (P) and changing of rc channels (D)

  // TODO: If no signal --> zero.

  uint8_t axis;

  // takes almost no time...

  RC_update();

  // takes almost no time...

  EC_update();

  // takes about 80 usec.

  HC_update();

  int16_t* RC_PRTY = RC_getPRTY();

  int16_t* EC_PRTY = EC_getPRTY();

  control[PITCH]   = RC_PRTY[CONTROL_PITCH] + EC_PRTY[CONTROL_PITCH];

  control[ROLL]    = RC_PRTY[CONTROL_ROLL] + EC_PRTY[CONTROL_ROLL];

  // This can be a CPU time killer if the function implementations are inefficient.

  controlThrottle  = HC_getThrottle(AC_getThrottle(RC_PRTY[CONTROL_THROTTLE] + EC_PRTY[CONTROL_THROTTLE]));

  controlYaw       = RC_PRTY[CONTROL_YAW] + EC_PRTY[CONTROL_YAW];

  DebugOut.Analog[12] = control[PITCH];

  DebugOut.Analog[13] = control[ROLL];

  //DebugOut.Analog[26] = controlYaw;

  if (controlMixer_getSignalQuality() >= SIGNAL_GOOD) {

    controlMixer_updateVariables();

    configuration_applyVariablesToParams();

    looping = RC_getLooping(looping);

  } else { // Signal is not OK

    // Could handle switch to emergency flight here.

    // throttle is handled elsewhere.

    looping = 0;

  }

  // part1a end.

  /* This is not really necessary with the dead-gap feature on all sticks (see rc.c)

  if(staticParams.GlobalConfig & (CFG_COMPASS_ACTIVE | CFG_GPS_ACTIVE)) {

    if (controlYaw > 2) controlYaw-= 2;

    else if (controlYaw< -2) controlYaw += 2;

    else controlYaw = 0;

  }

  */

  /*

   * Record maxima

   */

  for (axis=PITCH; axis<=ROLL; axis++) {

    if(abs(control[axis] / CONTROL_SCALING) > maxControl[axis]) {

      maxControl[axis] = abs(control[axis]) / CONTROL_SCALING;

      if(maxControl[axis] > 100) maxControl[axis] = 100;

    } else if (maxControl[axis]) maxControl[axis]--;

  }

  uint8_t rcCommand = (RC_getSignalQuality() >= SIGNAL_OK) ? RC_getCommand() : COMMAND_NONE;

  uint8_t ecCommand = (EC_getSignalQuality() >= SIGNAL_OK) ? EC_getCommand() : COMMAND_NONE;

  if (rcCommand != COMMAND_NONE) {

    isCommandRepeated = (lastCommand == rcCommand);

    lastCommand = rcCommand;

    lastArgument = RC_getArgument();

  } else if (ecCommand != COMMAND_NONE) {

    isCommandRepeated = (lastCommand == ecCommand);

    lastCommand = ecCommand;

    lastArgument = EC_getArgument();

  } else {

    // Both sources have no command, or one or both are out.

    // Just set to false. There is no reason to check if the none-command was repeated anyway.

    isCommandRepeated = 0;

    lastCommand = COMMAND_NONE;

  }

  if (isCommandRepeated) DebugOut.Digital[0] |= DEBUG_COMMANDREPEATED; else DebugOut.Digital[0] &= ~DEBUG_COMMANDREPEATED;

  if (rcCommand) DebugOut.Digital[1] |= DEBUG_COMMANDREPEATED; else DebugOut.Digital[1] &= ~DEBUG_COMMANDREPEATED;

  // part1 end.

}

// TODO: Integrate into command system.

uint8_t controlMixer_testCompassCalState(void) {

  return RC_testCompassCalState();

}