Ardupilot2/ArduCopter/control_modes.pde

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

#define CONTROL_SWITCH_COUNTER  20  // 20 iterations at 100hz (i.e. 2/10th of a second) at a new switch position will cause flight mode change
static void read_control_switch()
{
    static uint8_t switch_counter = 0;

    uint8_t switchPosition = readSwitch();

    // has switch moved?
    // ignore flight mode changes if in failsafe
    if (oldSwitchPosition != switchPosition && !ap.failsafe_radio) {
        switch_counter++;
        if(switch_counter >= CONTROL_SWITCH_COUNTER) {
            oldSwitchPosition       = switchPosition;
            switch_counter          = 0;

            // set flight mode and simple mode setting
            if (set_mode(flight_modes[switchPosition])) {
                if(g.ch7_option != AUX_SWITCH_SIMPLE_MODE && g.ch8_option != AUX_SWITCH_SIMPLE_MODE) {
                    // set Simple mode using stored paramters from Mission planner
                    // rather than by the control switch
                    set_simple_mode(BIT_IS_SET(g.simple_modes, switchPosition));
                }
            }

        }
    }else{
        // reset switch_counter if there's been no change
        // we don't want 10 intermittant blips causing a flight mode change
        switch_counter = 0;
    }
}

static uint8_t readSwitch(void){
    int16_t pulsewidth = g.rc_5.radio_in;   // default for Arducopter

    if (pulsewidth < 1231) return 0;
    if (pulsewidth < 1361) return 1;
    if (pulsewidth < 1491) return 2;
    if (pulsewidth < 1621) return 3;
    if (pulsewidth < 1750) return 4;        // Software Manual
    return 5;                               // Hardware Manual
}

static void reset_control_switch()
{
    oldSwitchPosition = -1;
    read_control_switch();
}

// read_aux_switches - checks aux switch positions and invokes configured actions
static void read_aux_switches()
{
    // check if ch7 switch has changed position
    if (ap_system.CH7_flag != (g.rc_7.radio_in >= AUX_SWITCH_PWM_TRIGGER)) {
        // set the ch7 flag
        ap_system.CH7_flag = (g.rc_7.radio_in >= AUX_SWITCH_PWM_TRIGGER);

        // invoke the appropriate function
        do_aux_switch_function(g.ch7_option, ap_system.CH7_flag);
    }

    // safety check to ensure we ch7 and ch8 have different functions
    if (g.ch7_option == g.ch8_option) {
        return;
    }

    // check if ch8 switch has changed position
    if (ap_system.CH8_flag != (g.rc_8.radio_in >= AUX_SWITCH_PWM_TRIGGER)) {
        // set the ch8 flag
        ap_system.CH8_flag = (g.rc_8.radio_in >= AUX_SWITCH_PWM_TRIGGER);
        // invoke the appropriate function
        do_aux_switch_function(g.ch8_option, ap_system.CH8_flag);
    }
}

// init_aux_switches - invoke configured actions at start-up for aux function where it is safe to do so
static void init_aux_switches()
{
    // set channel 7 and 8 flags according to switch position
    ap_system.CH7_flag = (g.rc_7.radio_in >= AUX_SWITCH_PWM_TRIGGER);
    ap_system.CH8_flag = (g.rc_8.radio_in >= AUX_SWITCH_PWM_TRIGGER);

    // init channel 7 options
    switch(g.ch7_option) {
        case AUX_SWITCH_SIMPLE_MODE:
        case AUX_SWITCH_SONAR:
        case AUX_SWITCH_RESETTOARMEDYAW:
            do_aux_switch_function(g.ch7_option, ap_system.CH7_flag);
            break;
    }

    // safety check to ensure we ch7 and ch8 have different functions
    if (g.ch7_option == g.ch8_option) {
        return;
    }

    // init channel 8 option
    switch(g.ch8_option) {
        case AUX_SWITCH_SIMPLE_MODE:
        case AUX_SWITCH_SONAR:
        case AUX_SWITCH_RESETTOARMEDYAW:
            do_aux_switch_function(g.ch8_option, ap_system.CH8_flag);
            break;
    }
}

// do_aux_switch_function - implement the function invoked by the ch7 or ch8 switch
static void do_aux_switch_function(int8_t ch_function, bool ch_flag)
{
    int8_t tmp_function = ch_function;

    // multi mode check
    if(ch_function == AUX_SWITCH_MULTI_MODE) {
        if (g.rc_6.radio_in < CH6_PWM_TRIGGER_LOW) {
            tmp_function = AUX_SWITCH_FLIP;
        }else if (g.rc_6.radio_in > CH6_PWM_TRIGGER_HIGH) {
            tmp_function = AUX_SWITCH_SAVE_WP;
        }else{
            tmp_function = AUX_SWITCH_RTL;
        }
    }

    switch(tmp_function) {
        case AUX_SWITCH_FLIP:
            // flip if switch is on, positive throttle and we're actually flying
            if(ch_flag && g.rc_3.control_in >= 0 && ap.takeoff_complete) {
                init_flip();
            }
            break;

        case AUX_SWITCH_SIMPLE_MODE:
            set_simple_mode(ch_flag);
            break;

        case AUX_SWITCH_RTL:
            if (ch_flag) {
                // engage RTL (if not possible we remain in current flight mode)
                set_mode(RTL);
            }else{
                // disengage RTL to previous flight mode if we are currently in RTL or loiter
                if (control_mode == RTL || control_mode == LOITER) {
                    reset_control_switch();
                }
            }
            break;

        case AUX_SWITCH_SAVE_TRIM:
            if(ch_flag && control_mode <= ACRO && g.rc_3.control_in == 0) {
                save_trim();
            }
            break;

        case AUX_SWITCH_SAVE_WP:
            // save waypoint when switch is switched off
            if (ch_flag == false) {

                // if in auto mode, reset the mission
                if(control_mode == AUTO) {
                    aux_switch_wp_index = 0;
                    g.command_total.set_and_save(1);
                    set_mode(RTL);  // if by chance we are unable to switch to RTL we just stay in AUTO and hope the GPS failsafe will take-over
                    return;
                }

                if(aux_switch_wp_index == 0) {
                    // this is our first WP, let's save WP 1 as a takeoff
                    // increment index to WP index of 1 (home is stored at 0)
                    aux_switch_wp_index = 1;

                    Location temp   = home;
                    // set our location ID to 16, MAV_CMD_NAV_WAYPOINT
                    temp.id = MAV_CMD_NAV_TAKEOFF;
                    temp.alt = current_loc.alt;

                    // save command:
                    // we use the current altitude to be the target for takeoff.
                    // only altitude will matter to the AP mission script for takeoff.
                    // If we are above the altitude, we will skip the command.
                    set_cmd_with_index(temp, aux_switch_wp_index);
                }

                // increment index
                aux_switch_wp_index++;

                // set the next_WP (home is stored at 0)
                // max out at 100 since I think we need to stay under the EEPROM limit
                aux_switch_wp_index = constrain_int16(aux_switch_wp_index, 1, 100);

                if(g.rc_3.control_in > 0) {
                    // set our location ID to 16, MAV_CMD_NAV_WAYPOINT
                    current_loc.id = MAV_CMD_NAV_WAYPOINT;
                }else{
                    // set our location ID to 21, MAV_CMD_NAV_LAND
                    current_loc.id = MAV_CMD_NAV_LAND;
                }

                // save command
                set_cmd_with_index(current_loc, aux_switch_wp_index);

                // Cause the CopterLEDs to blink twice to indicate saved waypoint
                copter_leds_nav_blink = 10;
            }
            break;

#if CAMERA == ENABLED
        case AUX_SWITCH_CAMERA_TRIGGER:
            if(ch_flag) {
                do_take_picture();
            }
            break;
#endif

        case AUX_SWITCH_SONAR:
            // enable or disable the sonar
            g.sonar_enabled = ch_flag;
            break;

        case AUX_SWITCH_RESETTOARMEDYAW:
            if (ch_flag) {
                set_yaw_mode(YAW_RESETTOARMEDYAW);
            }else{
                set_yaw_mode(YAW_HOLD);
            }
            break; 
    }
}

// save_trim - adds roll and pitch trims from the radio to ahrs
static void save_trim()
{
    // save roll and pitch trim
    float roll_trim = ToRad((float)g.rc_1.control_in/100.0f);
    float pitch_trim = ToRad((float)g.rc_2.control_in/100.0f);
    ahrs.add_trim(roll_trim, pitch_trim);
}

// auto_trim - slightly adjusts the ahrs.roll_trim and ahrs.pitch_trim towards the current stick positions
// meant to be called continuously while the pilot attempts to keep the copter level
static void auto_trim()
{
    if(auto_trim_counter > 0) {
        auto_trim_counter--;

        // flash the leds
        led_mode = SAVE_TRIM_LEDS;

        // calculate roll trim adjustment
        float roll_trim_adjustment = ToRad((float)g.rc_1.control_in / 4000.0f);

        // calculate pitch trim adjustment
        float pitch_trim_adjustment = ToRad((float)g.rc_2.control_in / 4000.0f);

        // make sure accelerometer values impact attitude quickly
        ahrs.set_fast_gains(true);

        // add trim to ahrs object
        // save to eeprom on last iteration
        ahrs.add_trim(roll_trim_adjustment, pitch_trim_adjustment, (auto_trim_counter == 0));

        // on last iteration restore leds and accel gains to normal
        if(auto_trim_counter == 0) {
            ahrs.set_fast_gains(false);
            led_mode = NORMAL_LEDS;
            clear_leds();
        }
    }
}