autopilot_utils.c

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/*
 * Copyright (C) 2016 Gautier Hattenberger <gautier.hattenberger@enac.fr>
 *
 * This file is part of paparazzi.
 *
 * paparazzi is free software; you can redistribute it and/or modify
 * it under the terms of the GNU General Public License as published by
 * the Free Software Foundation; either version 2, or (at your option)
 * any later version.
 *
 * paparazzi is distributed in the hope that it will be useful,
 * but WITHOUT ANY WARRANTY; without even the implied warranty of
 * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
 * GNU General Public License for more details.
 *
 * You should have received a copy of the GNU General Public License
 * along with paparazzi; see the file COPYING.  If not, write to
 * the Free Software Foundation, 59 Temple Place - Suite 330,
 * Boston, MA 02111-1307, USA.
 */
 
#include "firmwares/rotorcraft/autopilot_utils.h"
#include "autopilot.h"
#include "firmwares/rotorcraft/autopilot_rc_helpers.h"
#include "state.h"
#include "modules/radio_control/radio_control.h"
 
PRINT_CONFIG_VAR(FAILSAFE_DESCENT_SPEED)
 
#if (defined MODE_MANUAL) && (defined MODE_AUTO1)
 
#if defined RADIO_MODE_2x3
 
#define THRESHOLD_1d3_PPRZ (MAX_PPRZ / 3)
#define THRESHOLD_2d3_PPRZ ((MAX_PPRZ / 3) * 2)
uint8_t ap_mode_of_3x2way_switch(void)
{
  int val = radio_control.values[RADIO_MODE];
  if (radio_control.values[RADIO_MODE] < 0) {
    val = MAX_PPRZ + val;
  }
  if (val < THRESHOLD_1d3_PPRZ) {
    return MODE_MANUAL;
  } else if (val < THRESHOLD_2d3_PPRZ) {
    return MODE_AUTO1;
  } else {
    return autopilot_mode_auto2;
  }
}
 
#else
 
#define THRESHOLD_1_PPRZ (MIN_PPRZ / 2)
#define THRESHOLD_2_PPRZ (MAX_PPRZ / 2)
 
uint8_t ap_mode_of_3way_switch(void)
{
  if (radio_control.values[RADIO_MODE] > THRESHOLD_2_PPRZ) {
    return autopilot_mode_auto2;
  } else if (radio_control.values[RADIO_MODE] > THRESHOLD_1_PPRZ) {
    return MODE_AUTO1;
  } else {
    return MODE_MANUAL;
  }
}
 
#endif
 
#if defined RADIO_AUTO_MODE || defined(__DOXYGEN__)
uint8_t ap_mode_of_two_switches(void)
{
  if (radio_control.values[RADIO_MODE] < THRESHOLD_1_PPRZ) {
    /* RADIO_MODE in MANUAL position */
    return MODE_MANUAL;
  } else {
    /* RADIO_MODE not in MANUAL position.
     * Select AUTO mode bassed on RADIO_AUTO_MODE channel
     */
    if (radio_control.values[RADIO_AUTO_MODE] > THRESHOLD_2_PPRZ) {
      return autopilot_mode_auto2;
    } else {
      return MODE_AUTO1;
    }
  }
}
#endif
 
#endif // MODE_MANUAL && MODE_AUTO1
 
void WEAK set_rotorcraft_commands(pprz_t *cmd_out, int32_t *cmd_in, bool in_flight __attribute__((unused)), bool motors_on __attribute__((unused)))
{
#if !ROTORCRAFT_IS_HELI
#if !ROTORCRAFT_COMMANDS_YAW_ALWAYS_ENABLED && defined(COMMAND_YAW)
  if (!in_flight) {
    cmd_in[COMMAND_YAW] = 0;
  }
#endif
  if (!motors_on) {
    cmd_in[COMMAND_THRUST] = 0;
  }
#endif
#ifdef COMMAND_ROLL
  cmd_out[COMMAND_ROLL] = cmd_in[COMMAND_ROLL];
#endif
#ifdef COMMAND_PITCH
  cmd_out[COMMAND_PITCH] = cmd_in[COMMAND_PITCH];
#endif
#ifdef COMMAND_YAW
  cmd_out[COMMAND_YAW] = cmd_in[COMMAND_YAW];
#endif
  cmd_out[COMMAND_THRUST] = cmd_in[COMMAND_THRUST];
}