概述
首先从copter.cpp中的fast_loop开始
进入到motors_output()函数中
上述函数中完成的有一些解锁检查, 进入之后如下图所示
这个函数中完成由
τ
tau
τ , thrust到 PWM的输出转换过程
首先在output_armed_stabilizing()函数中完成系数因子*
τ
tau
τ, 具体代码为
for (i = 0; i < AP_MOTORS_MAX_NUM_MOTORS; i++) {
if (motor_enabled[i]) {
// calculate the thrust outputs for roll and pitch
_thrust_rpyt_out[i] = roll_thrust * _roll_factor[i] + pitch_thrust * _pitch_factor[i];
// record lowest roll + pitch command
if (_thrust_rpyt_out[i] < rp_low) {
rp_low = _thrust_rpyt_out[i];
}
// record highest roll + pitch command
if (_thrust_rpyt_out[i] > rp_high && (!_thrust_boost || i != _motor_lost_index)) {
rp_high = _thrust_rpyt_out[i];
}
// Check the maximum yaw control that can be used on this channel
// Exclude any lost motors if thrust boost is enabled
if (!is_zero(_yaw_factor[i]) && (!_thrust_boost || i != _motor_lost_index)){
if (is_positive(yaw_thrust * _yaw_factor[i])) {
yaw_allowed = MIN(yaw_allowed, fabsf(MAX(1.0f - (throttle_thrust_best_rpy + _thrust_rpyt_out[i]), 0.0f)/_yaw_factor[i]));
} else {
yaw_allowed = MIN(yaw_allowed, fabsf(MAX(throttle_thrust_best_rpy + _thrust_rpyt_out[i], 0.0f)/_yaw_factor[i]));
}
}
}
}
关键参数为 _roll_factor[i], _pitch_factor[i], 以及后面出现的_yaw_facotr[i], 对应的thrust为
// add scaled roll, pitch, constrained yaw and throttle for each motor
for (i = 0; i < AP_MOTORS_MAX_NUM_MOTORS; i++) {
if (motor_enabled[i]) {
_thrust_rpyt_out[i] = throttle_thrust_best_rpy + thr_adj + (rpy_scale * _thrust_rpyt_out[i]);
}
}
随后在void AP_MotorsMatrix::output_to_motors()函数中, 将上述计算出来的_thrust_rpyt_out转换赋值给_actuator[i], 具体代码为
最后完成输出.
PS: 比例因子的给定在 AP_Vehicle .cpp 中的init_ardupilot()中的 init_rc_out()函数中完成的初始化
// init
void AP_MotorsMatrix::init(motor_frame_class frame_class, motor_frame_type frame_type)
{
// record requested frame class and type
_last_frame_class = frame_class;
_last_frame_type = frame_type;
// setup the motors
setup_motors(frame_class, frame_type);
// enable fast channels or instant pwm
set_update_rate(_speed_hz);
}
最后
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