ardupilot/ArduCopter/mode_stabilize.cpp
Peter Barker 676d75c391 Copter: correct namespacing of Copter modes
This makes us look like Rover and Plane in terms of namespacing for the
Mode classes, and removes a wart where we #include mode.h in the middle
of the Mode class.

This was done mechanically for the most part.

I've had to remove the convenience reference for ap as part of this.
2019-06-11 09:18:22 +09:00

62 lines
2.1 KiB
C++

#include "Copter.h"
/*
* Init and run calls for stabilize flight mode
*/
// stabilize_run - runs the main stabilize controller
// should be called at 100hz or more
void ModeStabilize::run()
{
// apply simple mode transform to pilot inputs
update_simple_mode();
// convert pilot input to lean angles
float target_roll, target_pitch;
get_pilot_desired_lean_angles(target_roll, target_pitch, copter.aparm.angle_max, copter.aparm.angle_max);
// get pilot's desired yaw rate
float target_yaw_rate = get_pilot_desired_yaw_rate(channel_yaw->get_control_in());
if (!motors->armed()) {
// Motors should be Stopped
motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::SHUT_DOWN);
} else if (copter.ap.throttle_zero) {
// Attempting to Land
motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::GROUND_IDLE);
} else {
motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
}
switch (motors->get_spool_state()) {
case AP_Motors::SpoolState::SHUT_DOWN:
// Motors Stopped
attitude_control->set_yaw_target_to_current_heading();
attitude_control->reset_rate_controller_I_terms();
break;
case AP_Motors::SpoolState::GROUND_IDLE:
// Landed
attitude_control->set_yaw_target_to_current_heading();
attitude_control->reset_rate_controller_I_terms();
break;
case AP_Motors::SpoolState::THROTTLE_UNLIMITED:
// clear landing flag above zero throttle
if (!motors->limit.throttle_lower) {
set_land_complete(false);
}
break;
case AP_Motors::SpoolState::SPOOLING_UP:
case AP_Motors::SpoolState::SPOOLING_DOWN:
// do nothing
break;
}
// call attitude controller
attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(target_roll, target_pitch, target_yaw_rate);
// output pilot's throttle
attitude_control->set_throttle_out(get_pilot_desired_throttle(),
true,
g.throttle_filt);
}