ardupilot/libraries/AP_Motors/AP_MotorsTri.cpp

// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
/*
   This program 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 3 of the License, or
   (at your option) any later version.

   This program 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 this program.  If not, see <http://www.gnu.org/licenses/>.
 */

/*
 *       AP_MotorsTri.cpp - ArduCopter motors library
 *       Code by RandyMackay. DIYDrones.com
 *
 */
#include <AP_HAL.h>
#include <AP_Math.h>
#include "AP_MotorsTri.h"

extern const AP_HAL::HAL& hal;

// init
void AP_MotorsTri::Init()
{
    // call parent Init function to set-up throttle curve
    AP_Motors::Init();

    // set update rate for the 3 motors (but not the servo on channel 7)
    set_update_rate(_speed_hz);

    // set the motor_enabled flag so that the ESCs can be calibrated like other frame types
    motor_enabled[AP_MOTORS_MOT_1] = true;
    motor_enabled[AP_MOTORS_MOT_2] = true;
    motor_enabled[AP_MOTORS_MOT_4] = true;

    // disable CH7 from being used as an aux output (i.e. for camera gimbal, etc)
    RC_Channel_aux::disable_aux_channel(AP_MOTORS_CH_TRI_YAW);
}

// set update rate to motors - a value in hertz
void AP_MotorsTri::set_update_rate( uint16_t speed_hz )
{
    // record requested speed
    _speed_hz = speed_hz;

    // set update rate for the 3 motors (but not the servo on channel 7)
    uint32_t mask = 
	    1U << pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_1]) |
	    1U << pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_2]) |
	    1U << pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_4]);
    hal.rcout->set_freq(mask, _speed_hz);
}

// enable - starts allowing signals to be sent to motors
void AP_MotorsTri::enable()
{
    // enable output channels
    hal.rcout->enable_ch(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_1]));
    hal.rcout->enable_ch(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_2]));
    hal.rcout->enable_ch(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_4]));
    hal.rcout->enable_ch(AP_MOTORS_CH_TRI_YAW);
}

// output_min - sends minimum values out to the motors
void AP_MotorsTri::output_min()
{
    // set lower limit flag
    limit.throttle_lower = true;

    // send minimum value to each motor
    hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_1]), _rc_throttle.radio_min);
    hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_2]), _rc_throttle.radio_min);
    hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_4]), _rc_throttle.radio_min);
    hal.rcout->write(AP_MOTORS_CH_TRI_YAW, _rc_yaw.radio_trim);
}

// get_motor_mask - returns a bitmask of which outputs are being used for motors or servos (1 means being used)
//  this can be used to ensure other pwm outputs (i.e. for servos) do not conflict
uint16_t AP_MotorsTri::get_motor_mask()
{
    // tri copter uses channels 1,2,4 and 7
    return (1U << pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_1])) |
        (1U << pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_2])) |
        (1U << pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_4])) |
        (1U << AP_MOTORS_CH_TRI_YAW);
}

void AP_MotorsTri::output_armed_not_stabilizing()
{
    int16_t out_min = _rc_throttle.radio_min + _min_throttle;
    int16_t out_max = _rc_throttle.radio_max;
    int16_t motor_out[AP_MOTORS_MOT_4+1];

    // initialize limits flags
    limit.roll_pitch = true;
    limit.yaw = true;
    limit.throttle_lower = false;
    limit.throttle_upper = false;

    int16_t min_thr = rel_pwm_to_thr_range(_spin_when_armed_ramped);

    if (_rc_throttle.servo_out <= min_thr) {
        _rc_throttle.servo_out = min_thr;
        limit.throttle_lower = true;
    }

    if (_rc_throttle.servo_out >= _hover_out) {
        _rc_throttle.servo_out = _hover_out;
        limit.throttle_upper = true;
    }

    _rc_yaw.servo_out=0;
    _rc_yaw.calc_pwm();

    _rc_throttle.calc_pwm();

    motor_out[AP_MOTORS_MOT_1] = _rc_throttle.radio_out;
    motor_out[AP_MOTORS_MOT_2] = _rc_throttle.radio_out;
    motor_out[AP_MOTORS_MOT_4] = _rc_throttle.radio_out;

    if(_rc_throttle.radio_out >= out_min) {
        // adjust for thrust curve and voltage scaling
        motor_out[AP_MOTORS_MOT_1] = apply_thrust_curve_and_volt_scaling(motor_out[AP_MOTORS_MOT_1], out_min, out_max);
        motor_out[AP_MOTORS_MOT_2] = apply_thrust_curve_and_volt_scaling(motor_out[AP_MOTORS_MOT_2], out_min, out_max);
        motor_out[AP_MOTORS_MOT_4] = apply_thrust_curve_and_volt_scaling(motor_out[AP_MOTORS_MOT_4], out_min, out_max);
    }

    // send output to each motor
    hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_1]), motor_out[AP_MOTORS_MOT_1]);
    hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_2]), motor_out[AP_MOTORS_MOT_2]);
    hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_4]), motor_out[AP_MOTORS_MOT_4]);

    if( _rc_tail.get_reverse() == true ) {
        hal.rcout->write(AP_MOTORS_CH_TRI_YAW, _rc_yaw.radio_trim - (_rc_yaw.radio_out - _rc_yaw.radio_trim));
    }else{
        hal.rcout->write(AP_MOTORS_CH_TRI_YAW, _rc_yaw.radio_out);
    }
}

// sends commands to the motors
// TODO pull code that is common to output_armed_not_stabilizing into helper functions
void AP_MotorsTri::output_armed_stabilizing()
{
    int16_t out_min = _rc_throttle.radio_min + _min_throttle;
    int16_t out_max = _rc_throttle.radio_max;
    int16_t motor_out[AP_MOTORS_MOT_4+1];

    // initialize limits flags
    limit.roll_pitch = false;
    limit.yaw = false;
    limit.throttle_lower = false;
    limit.throttle_upper = false;

    // Throttle is 0 to 1000 only
    if (_rc_throttle.servo_out <= 0) {
        _rc_throttle.servo_out = 0;
        limit.throttle_lower = true;
    }
    if (_rc_throttle.servo_out >= _max_throttle) {
        _rc_throttle.servo_out = _max_throttle;
        limit.throttle_upper = true;
    }

    // tricopters limit throttle to 80%
    // To-Do: implement improved stability patch and remove this limit
    if (_rc_throttle.servo_out > 800) {
        _rc_throttle.servo_out = 800;
        limit.throttle_upper = true;
    }

    // capture desired roll, pitch, yaw and throttle from receiver
    _rc_roll.calc_pwm();
    _rc_pitch.calc_pwm();
    _rc_throttle.calc_pwm();
    _rc_yaw.calc_pwm();

    // if we are not sending a throttle output, we cut the motors
    if(_rc_throttle.servo_out == 0) {
        // range check spin_when_armed
        if (_spin_when_armed_ramped < 0) {
            _spin_when_armed_ramped = 0;
        }
        if (_spin_when_armed_ramped > _min_throttle) {
            _spin_when_armed_ramped = _min_throttle;
        }
        motor_out[AP_MOTORS_MOT_1] = _rc_throttle.radio_min + _spin_when_armed_ramped;
        motor_out[AP_MOTORS_MOT_2] = _rc_throttle.radio_min + _spin_when_armed_ramped;
        motor_out[AP_MOTORS_MOT_4] = _rc_throttle.radio_min + _spin_when_armed_ramped;

    }else{
        int16_t roll_out            = (float)_rc_roll.pwm_out * 0.866f;
        int16_t pitch_out           = _rc_pitch.pwm_out / 2;

        // check if throttle is below limit
        if (_rc_throttle.servo_out <= _min_throttle) {
            limit.throttle_lower = true;
            _rc_throttle.servo_out = _min_throttle;
            _rc_throttle.calc_pwm();    // recalculate radio.out
        }

        // TODO: set limits.roll_pitch and limits.yaw

        //left front
        motor_out[AP_MOTORS_MOT_2] = _rc_throttle.radio_out + roll_out + pitch_out;
        //right front
        motor_out[AP_MOTORS_MOT_1] = _rc_throttle.radio_out - roll_out + pitch_out;
        // rear
        motor_out[AP_MOTORS_MOT_4] = _rc_throttle.radio_out - _rc_pitch.pwm_out;

        // Tridge's stability patch
        if(motor_out[AP_MOTORS_MOT_1] > out_max) {
            motor_out[AP_MOTORS_MOT_2] -= (motor_out[AP_MOTORS_MOT_1] - out_max);
            motor_out[AP_MOTORS_MOT_4] -= (motor_out[AP_MOTORS_MOT_1] - out_max);
            motor_out[AP_MOTORS_MOT_1] = out_max;
        }

        if(motor_out[AP_MOTORS_MOT_2] > out_max) {
            motor_out[AP_MOTORS_MOT_1] -= (motor_out[AP_MOTORS_MOT_2] - out_max);
            motor_out[AP_MOTORS_MOT_4] -= (motor_out[AP_MOTORS_MOT_2] - out_max);
            motor_out[AP_MOTORS_MOT_2] = out_max;
        }

        if(motor_out[AP_MOTORS_MOT_4] > out_max) {
            motor_out[AP_MOTORS_MOT_1] -= (motor_out[AP_MOTORS_MOT_4] - out_max);
            motor_out[AP_MOTORS_MOT_2] -= (motor_out[AP_MOTORS_MOT_4] - out_max);
            motor_out[AP_MOTORS_MOT_4] = out_max;
        }

        // adjust for thrust curve and voltage scaling
        motor_out[AP_MOTORS_MOT_1] = apply_thrust_curve_and_volt_scaling(motor_out[AP_MOTORS_MOT_1], out_min, out_max);
        motor_out[AP_MOTORS_MOT_2] = apply_thrust_curve_and_volt_scaling(motor_out[AP_MOTORS_MOT_2], out_min, out_max);
        motor_out[AP_MOTORS_MOT_4] = apply_thrust_curve_and_volt_scaling(motor_out[AP_MOTORS_MOT_4], out_min, out_max);

        // ensure motors don't drop below a minimum value and stop
        motor_out[AP_MOTORS_MOT_1] = max(motor_out[AP_MOTORS_MOT_1],    out_min);
        motor_out[AP_MOTORS_MOT_2] = max(motor_out[AP_MOTORS_MOT_2],    out_min);
        motor_out[AP_MOTORS_MOT_4] = max(motor_out[AP_MOTORS_MOT_4],    out_min);
    }

    // send output to each motor
    hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_1]), motor_out[AP_MOTORS_MOT_1]);
    hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_2]), motor_out[AP_MOTORS_MOT_2]);
    hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_4]), motor_out[AP_MOTORS_MOT_4]);

    // also send out to tail command (we rely on any auto pilot to have updated the rc_yaw->radio_out to the correct value)
    // note we do not save the radio_out to the motor_out array so it may not appear in the ch7out in the status screen of the mission planner
    // note: we use _rc_tail's (aka channel 7's) REV parameter to control whether the servo is reversed or not but this is a bit nonsensical.
    //       a separate servo object (including min, max settings etc) would be better or at least a separate parameter to specify the direction of the tail servo
    if( _rc_tail.get_reverse() == true ) {
        hal.rcout->write(AP_MOTORS_CH_TRI_YAW, _rc_yaw.radio_trim - (_rc_yaw.radio_out - _rc_yaw.radio_trim));
    }else{
        hal.rcout->write(AP_MOTORS_CH_TRI_YAW, _rc_yaw.radio_out);
    }
}

// output_disarmed - sends commands to the motors
void AP_MotorsTri::output_disarmed()
{
    // Send minimum values to all motors
    output_min();
}

// output_test - spin a motor at the pwm value specified
//  motor_seq is the motor's sequence number from 1 to the number of motors on the frame
//  pwm value is an actual pwm value that will be output, normally in the range of 1000 ~ 2000
void AP_MotorsTri::output_test(uint8_t motor_seq, int16_t pwm)
{
    // exit immediately if not armed
    if (!armed()) {
        return;
    }

    // output to motors and servos
    switch (motor_seq) {
        case 1:
            // front right motor
            hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_1]), pwm);
            break;
        case 2:
            // back motor
            hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_4]), pwm);
            break;
        case 3:
            // back servo
            hal.rcout->write(AP_MOTORS_CH_TRI_YAW, pwm);
            break;
        case 4:
            // front left motor
            hal.rcout->write(pgm_read_byte(&_motor_to_channel_map[AP_MOTORS_MOT_2]), pwm);
            break;
        default:
            // do nothing
            break;
    }
}