ardupilot/libraries/AP_Motors/AP_Motors_Class.cpp

225 lines
7.8 KiB
C++

// -*- 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_Motors.cpp - ArduCopter motors library
* Code by RandyMackay. DIYDrones.com
*
*/
#include "AP_Motors_Class.h"
#include <AP_HAL.h>
extern const AP_HAL::HAL& hal;
// parameters for the motor class
const AP_Param::GroupInfo AP_Motors::var_info[] PROGMEM = {
// 0 was used by TB_RATIO
// @Param: TCRV_ENABLE
// @DisplayName: Thrust Curve Enable
// @Description: Controls whether a curve is used to linearize the thrust produced by the motors
// @User: Advanced
// @Values: 0:Disabled,1:Enable
AP_GROUPINFO("TCRV_ENABLE", 1, AP_Motors, _throttle_curve_enabled, THROTTLE_CURVE_ENABLED),
// @Param: TCRV_MIDPCT
// @DisplayName: Thrust Curve mid-point percentage
// @Description: Set the pwm position that produces half the maximum thrust of the motors
// @User: Advanced
// @Range: 20 80
// @Increment: 1
AP_GROUPINFO("TCRV_MIDPCT", 2, AP_Motors, _throttle_curve_mid, THROTTLE_CURVE_MID_THRUST),
// @Param: TCRV_MAXPCT
// @DisplayName: Thrust Curve max thrust percentage
// @Description: Set to the lowest pwm position that produces the maximum thrust of the motors. Most motors produce maximum thrust below the maximum pwm value that they accept.
// @User: Advanced
// @Range: 50 100
// @Increment: 1
AP_GROUPINFO("TCRV_MAXPCT", 3, AP_Motors, _throttle_curve_max, THROTTLE_CURVE_MAX_THRUST),
// @Param: SPIN_ARMED
// @DisplayName: Motors always spin when armed
// @Description: Controls whether motors always spin when armed (must be below THR_MIN)
// @Values: 0:Do Not Spin,70:VerySlow,100:Slow,130:Medium,150:Fast
// @User: Standard
AP_GROUPINFO("SPIN_ARMED", 5, AP_Motors, _spin_when_armed, AP_MOTORS_SPIN_WHEN_ARMED),
AP_GROUPEND
};
// Constructor
AP_Motors::AP_Motors( RC_Channel* rc_roll, RC_Channel* rc_pitch, RC_Channel* rc_throttle, RC_Channel* rc_yaw, uint16_t speed_hz ) :
_rc_roll(rc_roll),
_rc_pitch(rc_pitch),
_rc_throttle(rc_throttle),
_rc_yaw(rc_yaw),
_speed_hz(speed_hz),
_min_throttle(AP_MOTORS_DEFAULT_MIN_THROTTLE),
_max_throttle(AP_MOTORS_DEFAULT_MAX_THROTTLE),
_hover_out(AP_MOTORS_DEFAULT_MID_THROTTLE),
_spin_when_armed_ramped(0)
{
uint8_t i;
AP_Param::setup_object_defaults(this, var_info);
// initialise motor map
#if CONFIG_HAL_BOARD == HAL_BOARD_APM1
set_motor_to_channel_map(APM1_MOTOR_TO_CHANNEL_MAP);
#else
set_motor_to_channel_map(APM2_MOTOR_TO_CHANNEL_MAP);
#endif
// slow start motors from zero to min throttle
_flags.slow_start_low_end = true;
// clear output arrays
for(i=0; i<AP_MOTORS_MAX_NUM_MOTORS; i++) {
motor_out[i] = 0;
}
};
// init
void AP_Motors::Init()
{
// set-up throttle curve - motors classes will decide whether to use it based on _throttle_curve_enabled parameter
setup_throttle_curve();
};
void AP_Motors::armed(bool arm)
{
_flags.armed = arm;
if (!_flags.armed) {
_flags.slow_start_low_end = true;
}
AP_Notify::flags.armed = arm;
};
// set_min_throttle - sets the minimum throttle that will be sent to the engines when they're not off (i.e. to prevents issues with some motors spinning and some not at very low throttle)
void AP_Motors::set_min_throttle(uint16_t min_throttle)
{
_min_throttle = (float)min_throttle * (_rc_throttle->radio_max - _rc_throttle->radio_min) / 1000.0f;
}
// set_mid_throttle - sets the mid throttle which is close to the hover throttle of the copter
// this is used to limit the amount that the stability patch will increase the throttle to give more room for roll, pitch and yaw control
void AP_Motors::set_mid_throttle(uint16_t mid_throttle)
{
_hover_out = _rc_throttle->radio_min + (float)(_rc_throttle->radio_max - _rc_throttle->radio_min) * mid_throttle / 1000.0f;
}
// throttle_pass_through - passes pilot's throttle input directly to all motors - dangerous but used for initialising ESCs
void AP_Motors::throttle_pass_through()
{
if (armed()) {
// send the pilot's input directly to each enabled motor
for (int16_t i=0; i < AP_MOTORS_MAX_NUM_MOTORS; i++) {
if (motor_enabled[i]) {
hal.rcout->write(_motor_to_channel_map[i], _rc_throttle->radio_in);
}
}
}
}
// output - sends commands to the motors
void AP_Motors::output()
{
// update max throttle
update_max_throttle();
// output to motors
if (_flags.armed ) {
output_armed();
}else{
output_disarmed();
}
};
// setup_throttle_curve - used to linearlise thrust output by motors
// returns true if set up successfully
bool AP_Motors::setup_throttle_curve()
{
int16_t min_pwm = _rc_throttle->radio_min;
int16_t max_pwm = _rc_throttle->radio_max;
int16_t mid_throttle_pwm = (max_pwm + min_pwm) / 2;
int16_t mid_thrust_pwm = min_pwm + (float)(max_pwm - min_pwm) * ((float)_throttle_curve_mid/100.0f);
int16_t max_thrust_pwm = min_pwm + (float)(max_pwm - min_pwm) * ((float)_throttle_curve_max/100.0f);
bool retval = true;
// some basic checks that the curve is valid
if( mid_thrust_pwm >= (min_pwm+_min_throttle) && mid_thrust_pwm <= max_pwm && max_thrust_pwm >= mid_thrust_pwm && max_thrust_pwm <= max_pwm ) {
// clear curve
_throttle_curve.clear();
// curve initialisation
retval &= _throttle_curve.add_point(min_pwm, min_pwm);
retval &= _throttle_curve.add_point(min_pwm+_min_throttle, min_pwm+_min_throttle);
retval &= _throttle_curve.add_point(mid_throttle_pwm, mid_thrust_pwm);
retval &= _throttle_curve.add_point(max_pwm, max_thrust_pwm);
// return success
return retval;
}else{
retval = false;
}
// disable throttle curve if not set-up corrrectly
if( !retval ) {
_throttle_curve_enabled = false;
hal.console->println_P(PSTR("AP_Motors: failed to create throttle curve"));
}
return retval;
}
// slow_start - set to true to slew motors from current speed to maximum
// Note: this must be set immediately before a step up in throttle
void AP_Motors::slow_start(bool true_false)
{
// set slow_start flag
_flags.slow_start = true;
// initialise maximum throttle to current throttle
_max_throttle = constrain_int16(_rc_throttle->servo_out, 0, AP_MOTORS_DEFAULT_MAX_THROTTLE);
}
// update_max_throttle - updates the limits on _max_throttle if necessary taking into account slow_start_throttle flag
void AP_Motors::update_max_throttle()
{
// ramp up minimum spin speed if necessary
if (_flags.slow_start_low_end) {
_spin_when_armed_ramped += AP_MOTOR_SLOW_START_LOW_END_INCREMENT;
if (_spin_when_armed_ramped >= _spin_when_armed) {
_spin_when_armed_ramped = _spin_when_armed;
_flags.slow_start_low_end = false;
}
}
// return max throttle if we're not slow_starting
if (!_flags.slow_start) {
return;
}
// increase slow start throttle
_max_throttle += AP_MOTOR_SLOW_START_INCREMENT;
// turn off slow start if we've reached max throttle
if (_max_throttle >= _rc_throttle->servo_out) {
_max_throttle = AP_MOTORS_DEFAULT_MAX_THROTTLE;
_flags.slow_start = false;
}
}