ardupilot/ArduSub/motors.cpp

#include "Sub.h"

// enable_motor_output() - enable and output lowest possible value to motors
void Sub::enable_motor_output()
{
    motors.output_min();
}

// init_arm_motors - performs arming process including initialisation of barometer and gyros
//  returns false if arming failed because of pre-arm checks, arming checks or a gyro calibration failure
bool Sub::init_arm_motors(AP_Arming::Method method)
{
    static bool in_arm_motors = false;

    // exit immediately if already in this function
    if (in_arm_motors) {
        return false;
    }

    in_arm_motors = true;

    if (!arming.pre_arm_checks(true)) {
        AP_Notify::events.arming_failed = true;
        in_arm_motors = false;
        return false;
    }

    // let dataflash know that we're armed (it may open logs e.g.)
    AP::logger().set_vehicle_armed(true);

    // disable cpu failsafe because initialising everything takes a while
    mainloop_failsafe_disable();

    // notify that arming will occur (we do this early to give plenty of warning)
    AP_Notify::flags.armed = true;
    // call notify update a few times to ensure the message gets out
    for (uint8_t i=0; i<=10; i++) {
        notify.update();
    }

#if CONFIG_HAL_BOARD == HAL_BOARD_SITL
    gcs().send_text(MAV_SEVERITY_INFO, "Arming motors");
#endif

    initial_armed_bearing = ahrs.yaw_sensor;

    if (!ahrs.home_is_set()) {
        // Reset EKF altitude if home hasn't been set yet (we use EKF altitude as substitute for alt above home)

        // Always use absolute altitude for ROV
        // ahrs.resetHeightDatum();
        // Log_Write_Event(DATA_EKF_ALT_RESET);
    } else if (ahrs.home_is_set() && !ahrs.home_is_locked()) {
        // Reset home position if it has already been set before (but not locked)
        if (!set_home_to_current_location(false)) {
            // ignore this failure
        }
    }
	
    // enable gps velocity based centrefugal force compensation
    ahrs.set_correct_centrifugal(true);
    hal.util->set_soft_armed(true);

    // enable output to motors
    enable_motor_output();

    // finally actually arm the motors
    motors.armed(true);

    // log arming to dataflash
    Log_Write_Event(DATA_ARMED);

    // log flight mode in case it was changed while vehicle was disarmed
    logger.Write_Mode(control_mode, control_mode_reason);

    // reenable failsafe
    mainloop_failsafe_enable();

    // perf monitor ignores delay due to arming
    scheduler.perf_info.ignore_this_loop();

    // flag exiting this function
    in_arm_motors = false;

    // return success
    return true;
}

// init_disarm_motors - disarm motors
void Sub::init_disarm_motors()
{
    // return immediately if we are already disarmed
    if (!motors.armed()) {
        return;
    }

#if CONFIG_HAL_BOARD == HAL_BOARD_SITL
    gcs().send_text(MAV_SEVERITY_INFO, "Disarming motors");
#endif

    // save compass offsets learned by the EKF if enabled
    if (ahrs.use_compass() && compass.get_learn_type() == Compass::LEARN_EKF) {
        for (uint8_t i=0; i<COMPASS_MAX_INSTANCES; i++) {
            Vector3f magOffsets;
            if (ahrs.getMagOffsets(i, magOffsets)) {
                compass.set_and_save_offsets(i, magOffsets);
            }
        }
    }

    // log disarm to the dataflash
    Log_Write_Event(DATA_DISARMED);

    // send disarm command to motors
    motors.armed(false);

    // reset the mission
    mission.reset();

    AP::logger().set_vehicle_armed(false);

    // disable gps velocity based centrefugal force compensation
    ahrs.set_correct_centrifugal(false);
    hal.util->set_soft_armed(false);

    // clear input holds
    clear_input_hold();
}

// motors_output - send output to motors library which will adjust and send to ESCs and servos
void Sub::motors_output()
{
    // check if we are performing the motor test
    if (ap.motor_test) {
        verify_motor_test();
    } else {
        motors.set_interlock(true);
        motors.output();
    }
}

// Initialize new style motor test
// Perform checks to see if it is ok to begin the motor test
// Returns true if motor test has begun
bool Sub::init_motor_test()
{
    uint32_t tnow = AP_HAL::millis();

    // Ten second cooldown period required with no do_set_motor requests required
    // after failure.
    if (tnow < last_do_motor_test_fail_ms + 10000 && last_do_motor_test_fail_ms > 0) {
        gcs().send_text(MAV_SEVERITY_CRITICAL, "10 second cool down required");
        return false;
    }

    // check if safety switch has been pushed
    if (hal.util->safety_switch_state() == AP_HAL::Util::SAFETY_DISARMED) {
        gcs().send_text(MAV_SEVERITY_CRITICAL,"Disarm hardware safety switch before testing motors.");
        return false;
    }

    // Make sure we are on the ground
    if (!motors.armed()) {
        gcs().send_text(MAV_SEVERITY_WARNING, "Arm motors before testing motors.");
        return false;
    }

    enable_motor_output(); // set all motor outputs to zero
    ap.motor_test = true;

    return true;
}

// Verify new style motor test
// The motor test will fail if the interval between received
// MAV_CMD_DO_SET_MOTOR requests exceeds a timeout period
// Returns true if it is ok to proceed with new style motor test
bool Sub::verify_motor_test()
{
    bool pass = true;

    // Require at least 2 Hz incoming do_set_motor requests
    if (AP_HAL::millis() > last_do_motor_test_ms + 500) {
        gcs().send_text(MAV_SEVERITY_WARNING, "Motor test timed out!");
        pass = false;
    }

    if (!pass) {
        ap.motor_test = false;
        motors.armed(false); // disarm motors
        last_do_motor_test_fail_ms = AP_HAL::millis();
        return false;
    }

    return true;
}

bool Sub::handle_do_motor_test(mavlink_command_long_t command) {
    last_do_motor_test_ms = AP_HAL::millis();

    // If we are not already testing motors, initialize test
    if(!ap.motor_test) {
        if (!init_motor_test()) {
            gcs().send_text(MAV_SEVERITY_WARNING, "motor test initialization failed!");
            return false; // init fail
        }
    }

    float motor_number = command.param1;
    float throttle_type = command.param2;
    float throttle = command.param3;
    // float timeout_s = command.param4; // not used
    // float motor_count = command.param5; // not used
    float test_type = command.param6;

    if (!is_equal(test_type, (float)MOTOR_TEST_ORDER_BOARD)) {
        gcs().send_text(MAV_SEVERITY_WARNING, "bad test type %0.2f", (double)test_type);
        return false; // test type not supported here
    }

    if (is_equal(throttle_type, (float)MOTOR_TEST_THROTTLE_PILOT)) {
        gcs().send_text(MAV_SEVERITY_WARNING, "bad throttle type %0.2f", (double)throttle_type);

        return false; // throttle type not supported here
    }

    if (is_equal(throttle_type, (float)MOTOR_TEST_THROTTLE_PWM)) {
        return motors.output_test_num(motor_number, throttle); // true if motor output is set
    }

    if (is_equal(throttle_type, (float)MOTOR_TEST_THROTTLE_PERCENT)) {
        throttle = constrain_float(throttle, 0.0f, 100.0f);
        throttle = channel_throttle->get_radio_min() + throttle / 100.0f * (channel_throttle->get_radio_max() - channel_throttle->get_radio_min());
        return motors.output_test_num(motor_number, throttle); // true if motor output is set
    }

    return false;
}


// translate wpnav roll/pitch outputs to lateral/forward
void Sub::translate_wpnav_rp(float &lateral_out, float &forward_out)
{
    // get roll and pitch targets in centidegrees
    int32_t lateral = wp_nav.get_roll();
    int32_t forward = -wp_nav.get_pitch(); // output is reversed

    // constrain target forward/lateral values
    // The outputs of wp_nav.get_roll and get_pitch should already be constrained to these values
    lateral = constrain_int16(lateral, -aparm.angle_max, aparm.angle_max);
    forward = constrain_int16(forward, -aparm.angle_max, aparm.angle_max);

    // Normalize
    lateral_out = (float)lateral/(float)aparm.angle_max;
    forward_out = (float)forward/(float)aparm.angle_max;
}

// translate wpnav roll/pitch outputs to lateral/forward
void Sub::translate_circle_nav_rp(float &lateral_out, float &forward_out)
{
    // get roll and pitch targets in centidegrees
    int32_t lateral = circle_nav.get_roll();
    int32_t forward = -circle_nav.get_pitch(); // output is reversed

    // constrain target forward/lateral values
    lateral = constrain_int16(lateral, -aparm.angle_max, aparm.angle_max);
    forward = constrain_int16(forward, -aparm.angle_max, aparm.angle_max);

    // Normalize
    lateral_out = (float)lateral/(float)aparm.angle_max;
    forward_out = (float)forward/(float)aparm.angle_max;
}

// translate pos_control roll/pitch outputs to lateral/forward
void Sub::translate_pos_control_rp(float &lateral_out, float &forward_out)
{
    // get roll and pitch targets in centidegrees
    int32_t lateral = pos_control.get_roll();
    int32_t forward = -pos_control.get_pitch(); // output is reversed

    // constrain target forward/lateral values
    lateral = constrain_int16(lateral, -aparm.angle_max, aparm.angle_max);
    forward = constrain_int16(forward, -aparm.angle_max, aparm.angle_max);

    // Normalize
    lateral_out = (float)lateral/(float)aparm.angle_max;
    forward_out = (float)forward/(float)aparm.angle_max;
}