ardupilot/ArduPlane/mode_training.cpp

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#include "mode.h"
#include "Plane.h"
void ModeTraining::update()
{
plane.training_manual_roll = false;
plane.training_manual_pitch = false;
plane.update_load_factor();
// if the roll is past the set roll limit, then
// we set target roll to the limit
if (ahrs.roll_sensor >= plane.roll_limit_cd) {
plane.nav_roll_cd = plane.roll_limit_cd;
} else if (ahrs.roll_sensor <= -plane.roll_limit_cd) {
plane.nav_roll_cd = -plane.roll_limit_cd;
} else {
plane.training_manual_roll = true;
plane.nav_roll_cd = 0;
}
// if the pitch is past the set pitch limits, then
// we set target pitch to the limit
if (ahrs.pitch_sensor >= plane.aparm.pitch_limit_max*100) {
plane.nav_pitch_cd = plane.aparm.pitch_limit_max*100;
} else if (ahrs.pitch_sensor <= plane.pitch_limit_min*100) {
plane.nav_pitch_cd = plane.pitch_limit_min*100;
} else {
plane.training_manual_pitch = true;
plane.nav_pitch_cd = 0;
}
if (plane.fly_inverted()) {
plane.nav_pitch_cd = -plane.nav_pitch_cd;
}
}
/*
a special stabilization function for training mode
*/
void ModeTraining::run()
{
const float rexpo = plane.roll_in_expo(false);
const float pexpo = plane.pitch_in_expo(false);
if (plane.training_manual_roll) {
SRV_Channels::set_output_scaled(SRV_Channel::k_aileron, rexpo);
} else {
// calculate what is needed to hold
plane.stabilize_roll();
if ((plane.nav_roll_cd > 0 && rexpo < SRV_Channels::get_output_scaled(SRV_Channel::k_aileron)) ||
(plane.nav_roll_cd < 0 && rexpo > SRV_Channels::get_output_scaled(SRV_Channel::k_aileron))) {
// allow user to get out of the roll
SRV_Channels::set_output_scaled(SRV_Channel::k_aileron, rexpo);
}
}
if (plane.training_manual_pitch) {
SRV_Channels::set_output_scaled(SRV_Channel::k_elevator, pexpo);
} else {
plane.stabilize_pitch();
if ((plane.nav_pitch_cd > 0 && pexpo < SRV_Channels::get_output_scaled(SRV_Channel::k_elevator)) ||
(plane.nav_pitch_cd < 0 && pexpo > SRV_Channels::get_output_scaled(SRV_Channel::k_elevator))) {
// allow user to get back to level
SRV_Channels::set_output_scaled(SRV_Channel::k_elevator, pexpo);
}
}
// Always manual rudder control
output_rudder_and_steering(plane.rudder_in_expo(false));
output_pilot_throttle();
}