mirror of https://github.com/ArduPilot/ardupilot
194 lines
5.5 KiB
C++
194 lines
5.5 KiB
C++
/*
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This program is free software: you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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/*
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* AP_Motors.cpp - ArduCopter motors library
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* Code by RandyMackay. DIYDrones.com
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*
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*/
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#include "AP_Motors_Class.h"
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#include <AP_HAL/AP_HAL.h>
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#include <SRV_Channel/SRV_Channel.h>
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#include <GCS_MAVLink/GCS.h>
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extern const AP_HAL::HAL& hal;
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// singleton instance
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AP_Motors *AP_Motors::_singleton;
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// Constructor
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AP_Motors::AP_Motors(uint16_t loop_rate, uint16_t speed_hz) :
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_loop_rate(loop_rate),
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_speed_hz(speed_hz),
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_throttle_filter(),
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_spool_desired(DesiredSpoolState::SHUT_DOWN),
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_spool_state(SpoolState::SHUT_DOWN),
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_air_density_ratio(1.0f)
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{
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_singleton = this;
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// setup throttle filtering
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_throttle_filter.set_cutoff_frequency(0.0f);
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_throttle_filter.reset(0.0f);
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// init limit flags
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limit.roll = true;
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limit.pitch = true;
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limit.yaw = true;
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limit.throttle_lower = true;
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limit.throttle_upper = true;
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_thrust_boost = false;
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_thrust_balanced = true;
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};
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void AP_Motors::armed(bool arm)
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{
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if (_flags.armed != arm) {
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_flags.armed = arm;
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AP_Notify::flags.armed = arm;
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if (!arm) {
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save_params_on_disarm();
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}
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}
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};
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void AP_Motors::set_desired_spool_state(DesiredSpoolState spool)
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{
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if (_flags.armed || (spool == DesiredSpoolState::SHUT_DOWN)) {
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_spool_desired = spool;
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}
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};
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// pilot input in the -1 ~ +1 range for roll, pitch and yaw. 0~1 range for throttle
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void AP_Motors::set_radio_passthrough(float roll_input, float pitch_input, float throttle_input, float yaw_input)
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{
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_roll_radio_passthrough = roll_input;
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_pitch_radio_passthrough = pitch_input;
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_throttle_radio_passthrough = throttle_input;
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_yaw_radio_passthrough = yaw_input;
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}
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/*
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write to an output channel
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*/
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void AP_Motors::rc_write(uint8_t chan, uint16_t pwm)
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{
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SRV_Channel::Aux_servo_function_t function = SRV_Channels::get_motor_function(chan);
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SRV_Channels::set_output_pwm(function, pwm);
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}
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/*
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write to an output channel for an angle actuator
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*/
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void AP_Motors::rc_write_angle(uint8_t chan, int16_t angle_cd)
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{
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SRV_Channel::Aux_servo_function_t function = SRV_Channels::get_motor_function(chan);
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SRV_Channels::set_output_scaled(function, angle_cd);
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}
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/*
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set frequency of a set of channels
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*/
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void AP_Motors::rc_set_freq(uint32_t mask, uint16_t freq_hz)
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{
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if (freq_hz > 50) {
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_motor_fast_mask |= mask;
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}
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mask = rc_map_mask(mask);
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hal.rcout->set_freq(mask, freq_hz);
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switch (pwm_type(_pwm_type.get())) {
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case PWM_TYPE_ONESHOT:
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if (freq_hz > 50 && mask != 0) {
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hal.rcout->set_output_mode(mask, AP_HAL::RCOutput::MODE_PWM_ONESHOT);
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}
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break;
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case PWM_TYPE_ONESHOT125:
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if (freq_hz > 50 && mask != 0) {
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hal.rcout->set_output_mode(mask, AP_HAL::RCOutput::MODE_PWM_ONESHOT125);
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}
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break;
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case PWM_TYPE_BRUSHED:
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hal.rcout->set_output_mode(mask, AP_HAL::RCOutput::MODE_PWM_BRUSHED);
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break;
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case PWM_TYPE_DSHOT150:
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hal.rcout->set_output_mode(mask, AP_HAL::RCOutput::MODE_PWM_DSHOT150);
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break;
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case PWM_TYPE_DSHOT300:
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hal.rcout->set_output_mode(mask, AP_HAL::RCOutput::MODE_PWM_DSHOT300);
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break;
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case PWM_TYPE_DSHOT600:
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hal.rcout->set_output_mode(mask, AP_HAL::RCOutput::MODE_PWM_DSHOT600);
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break;
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case PWM_TYPE_DSHOT1200:
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hal.rcout->set_output_mode(mask, AP_HAL::RCOutput::MODE_PWM_DSHOT1200);
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break;
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default:
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hal.rcout->set_output_mode(mask, AP_HAL::RCOutput::MODE_PWM_NORMAL);
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break;
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}
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}
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/*
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map an internal motor mask to real motor mask, accounting for
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SERVOn_FUNCTION mappings, and allowing for multiple outputs per
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motor number
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*/
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uint32_t AP_Motors::rc_map_mask(uint32_t mask) const
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{
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uint32_t mask2 = 0;
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for (uint8_t i = 0; i < 32; i++) {
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uint32_t bit = 1UL << i;
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if (mask & bit) {
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SRV_Channel::Aux_servo_function_t function = SRV_Channels::get_motor_function(i);
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mask2 |= SRV_Channels::get_output_channel_mask(function);
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}
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}
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return mask2;
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}
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/*
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add a motor, setting up default output function as needed
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*/
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void AP_Motors::add_motor_num(int8_t motor_num)
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{
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// ensure valid motor number is provided
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if (motor_num >= 0 && motor_num < AP_MOTORS_MAX_NUM_MOTORS) {
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uint8_t chan;
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SRV_Channel::Aux_servo_function_t function = SRV_Channels::get_motor_function(motor_num);
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SRV_Channels::set_aux_channel_default(function, motor_num);
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if (!SRV_Channels::find_channel(function, chan)) {
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gcs().send_text(MAV_SEVERITY_ERROR, "Motors: unable to setup motor %u", motor_num);
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}
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}
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}
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// set limit flag for pitch, roll and yaw
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void AP_Motors::set_limit_flag_pitch_roll_yaw(bool flag)
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{
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limit.roll = flag;
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limit.pitch = flag;
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limit.yaw = flag;
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}
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namespace AP {
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AP_Motors *motors()
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{
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return AP_Motors::get_singleton();
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}
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}
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