ardupilot/ArduPlane/control_modes.cpp

/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-

#include "Plane.h"

void Plane::read_control_switch()
{
    static bool switch_debouncer;
    uint8_t switchPosition = readSwitch();

    // If switchPosition = 255 this indicates that the mode control channel input was out of range
    // If we get this value we do not want to change modes.
    if(switchPosition == 255) return;

    if (failsafe.ch3_failsafe || failsafe.ch3_counter > 0) {
        // when we are in ch3_failsafe mode then RC input is not
        // working, and we need to ignore the mode switch channel
        return;
    }

    if (millis() - failsafe.last_valid_rc_ms > 100) {
        // only use signals that are less than 0.1s old.
        return;
    }

    // we look for changes in the switch position. If the
    // RST_SWITCH_CH parameter is set, then it is a switch that can be
    // used to force re-reading of the control switch. This is useful
    // when returning to the previous mode after a failsafe or fence
    // breach. This channel is best used on a momentary switch (such
    // as a spring loaded trainer switch).
    if (oldSwitchPosition != switchPosition ||
        (g.reset_switch_chan != 0 &&
         hal.rcin->read(g.reset_switch_chan-1) > RESET_SWITCH_CHAN_PWM)) {

        if (switch_debouncer == false) {
            // this ensures that mode switches only happen if the
            // switch changes for 2 reads. This prevents momentary
            // spikes in the mode control channel from causing a mode
            // switch
            switch_debouncer = true;
            return;
        }

        set_mode((enum FlightMode)(flight_modes[switchPosition].get()), MODE_REASON_TX_COMMAND);

        oldSwitchPosition = switchPosition;
    }

    if (g.reset_mission_chan != 0 &&
        hal.rcin->read(g.reset_mission_chan-1) > RESET_SWITCH_CHAN_PWM) {
        mission.start();
        prev_WP_loc = current_loc;
    }

    switch_debouncer = false;

    if (g.inverted_flight_ch != 0) {
        // if the user has configured an inverted flight channel, then
        // fly upside down when that channel goes above INVERTED_FLIGHT_PWM
        inverted_flight = (control_mode != MANUAL && hal.rcin->read(g.inverted_flight_ch-1) > INVERTED_FLIGHT_PWM);
    }

#if PARACHUTE == ENABLED
    if (g.parachute_channel > 0) {
        if (hal.rcin->read(g.parachute_channel-1) >= 1700) {
            parachute_manual_release();
        }
    }
#endif
    
#if HAVE_PX4_MIXER
    if (g.override_channel > 0) {
        // if the user has configured an override channel then check it
        bool override_requested = (hal.rcin->read(g.override_channel-1) >= PX4IO_OVERRIDE_PWM);
        if (override_requested && !px4io_override_enabled) {
            if (hal.util->get_soft_armed() || (last_mixer_crc != -1)) {
                px4io_override_enabled = true;
                // disable output channels to force PX4IO override
                gcs_send_text(MAV_SEVERITY_WARNING, "PX4IO override enabled");
            } else {
                // we'll let the one second loop reconfigure the mixer. The
                // PX4IO code sometimes rejects a mixer, probably due to it
                // being busy in some way?
                gcs_send_text(MAV_SEVERITY_WARNING, "PX4IO override enable failed");
            }
        } else if (!override_requested && px4io_override_enabled) {
            px4io_override_enabled = false;
            RC_Channel_aux::enable_aux_servos();
            gcs_send_text(MAV_SEVERITY_WARNING, "PX4IO override disabled");
        }
        if (px4io_override_enabled && 
            hal.util->safety_switch_state() != AP_HAL::Util::SAFETY_ARMED &&
            g.override_safety == 1) {
            // we force safety off, so that if this override is used
            // with a in-flight reboot it gives a way for the pilot to
            // re-arm and take manual control
            hal.rcout->force_safety_off();
        }
    }
#endif // HAVE_PX4_MIXER
}

uint8_t Plane::readSwitch(void)
{
    uint16_t pulsewidth = hal.rcin->read(g.flight_mode_channel - 1);
    if (pulsewidth <= 900 || pulsewidth >= 2200) return 255;            // This is an error condition
    if (pulsewidth <= 1230) return 0;
    if (pulsewidth <= 1360) return 1;
    if (pulsewidth <= 1490) return 2;
    if (pulsewidth <= 1620) return 3;
    if (pulsewidth <= 1749) return 4;              // Software Manual
    return 5;                                                           // Hardware Manual
}

void Plane::reset_control_switch()
{
    oldSwitchPosition = 254;
    read_control_switch();
}

/*
  called when entering autotune
 */
void Plane::autotune_start(void)
{
    rollController.autotune_start();
    pitchController.autotune_start();
}

/*
  called when exiting autotune
 */
void Plane::autotune_restore(void)
{
    rollController.autotune_restore();
    pitchController.autotune_restore();
}

/*
  enable/disable autotune for AUTO modes
 */
void Plane::autotune_enable(bool enable)
{
    if (enable) {
        autotune_start();
    } else {
        autotune_restore();
    }
}

/*
  are we flying inverted?
 */
bool Plane::fly_inverted(void)
{
    if (g.inverted_flight_ch != 0 && inverted_flight) {
        // controlled with INVERTED_FLIGHT_CH
        return true;
    }
    if (control_mode == AUTO && auto_state.inverted_flight) {
        return true;
    }
    return false;
}