ardupilot/ArduCopter/control_stabilize.pde

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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
// acro_init - initialise acro controller
static bool acro_init(bool ignore_checks)
{
return true;
}
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// acro_run - runs the acro controller
// should be called at 100hz or more
static void acro_run()
{
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Vector3f rate_target; // for roll, pitch, yaw body-frame rate targets
// convert the input to the desired body frame rate
rate_target.x = g.rc_1.control_in * g.acro_rp_p;
rate_target.y = g.rc_2.control_in * g.acro_rp_p;
rate_target.z = g.rc_4.control_in * g.acro_yaw_p;
// To-Do: handle acro trainer here?
// To-Do: handle helicopter
acro_level_mix = constrain_float(1-max(max(abs(g.rc_1.control_in), abs(g.rc_2.control_in)), abs(g.rc_4.control_in))/4500.0, 0, 1)*cos_pitch_x;
// set targets for body frame rate controller
attitude_control.rate_stab_bf_targets(rate_target);
// convert stabilize rates to regular rates
attitude_control.rate_stab_bf_to_rate_bf_roll();
attitude_control.rate_stab_bf_to_rate_bf_pitch();
attitude_control.rate_stab_bf_to_rate_bf_yaw();
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// call get_acro_level_rates() here?
// To-Do: convert body-frame stabilized angles to earth frame angles and update controll_roll, pitch and yaw?
// body-frame rate controller is run directly from 100hz loop
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}
// stabilize_init - initialise stabilize controller
static bool stabilize_init(bool ignore_checks)
{
// set target altitude to zero for reporting
// To-Do: make pos controller aware when it's active/inactive so it can always report the altitude error?
pos_control.set_alt_target(0);
return true;
}
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// stabilize_run - runs the main stabilize controller
// should be called at 100hz or more
static void stabilize_run()
{
int16_t target_roll, target_pitch;
float target_yaw_rate;
int16_t pilot_throttle_scaled;
// if not armed or throttle at zero, set throttle to zero and exit immediately
if(!motors.armed() || g.rc_3.control_in <= 0) {
attitude_control.init_targets();
attitude_control.set_throttle_out(0, false);
return;
}
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// apply SIMPLE mode transform to pilot inputs
update_simple_mode();
// convert pilot input to lean angles
// To-Do: convert get_pilot_desired_lean_angles to return angles as floats
get_pilot_desired_lean_angles(g.rc_1.control_in, g.rc_2.control_in, target_roll, target_pitch);
// get pilot's desired yaw rate
target_yaw_rate = get_pilot_desired_yaw_rate(g.rc_4.control_in);
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// get pilot's desired throttle
pilot_throttle_scaled = get_pilot_desired_throttle(g.rc_3.control_in);
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// reset target lean angles and heading while landed
if (ap.land_complete) {
attitude_control.init_targets();
}else{
// call attitude controller
attitude_control.angleef_rp_rateef_y(target_roll, target_pitch, target_yaw_rate);
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// body-frame rate controller is run directly from 100hz loop
}
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// output pilot's throttle
attitude_control.set_throttle_out(pilot_throttle_scaled, true);
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// refetch angle targets for reporting
const Vector3f angle_target = attitude_control.angle_ef_targets();
control_roll = angle_target.x;
control_pitch = angle_target.y;
control_yaw = angle_target.z;
// update estimate of throttle cruise
#if FRAME_CONFIG == HELI_FRAME
update_throttle_cruise(motors.get_collective_out());
#else
update_throttle_cruise(pilot_throttle_scaled);
#endif //HELI_FRAME
// update take-off complete flag
if (!ap.takeoff_complete) {
if (pilot_throttle_scaled > g.throttle_cruise) {
// we must be in the air by now
set_takeoff_complete(true);
}
}
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}
// althold_init - initialise althold controller
static bool althold_init(bool ignore_checks)
{
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// initialise altitude target to stopping point
pos_control.set_target_to_stopping_point_z();
return true;
}
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// althold_run - runs the althold controller
// should be called at 100hz or more
static void althold_run()
{
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int16_t target_roll, target_pitch;
float target_yaw_rate;
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int16_t target_climb_rate;
// if not auto armed set throttle to zero and exit immediately
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if(!ap.auto_armed) {
// To-Do: reset altitude target if we're somehow not landed?
attitude_control.init_targets();
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attitude_control.set_throttle_out(0, false);
return;
}
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// apply SIMPLE mode transform to pilot inputs
update_simple_mode();
// get pilot desired lean angles
// To-Do: convert get_pilot_desired_lean_angles to return angles as floats
get_pilot_desired_lean_angles(g.rc_1.control_in, g.rc_2.control_in, target_roll, target_pitch);
// get pilot's desired yaw rate
target_yaw_rate = get_pilot_desired_yaw_rate(g.rc_4.control_in);
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// get pilot desired climb rate
target_climb_rate = get_pilot_desired_climb_rate(g.rc_3.control_in);
// check for pilot requested take-off
if (ap.land_complete && target_climb_rate > 0) {
// indicate we are taking off
set_land_complete(false);
// clear i term when we're taking off
set_throttle_takeoff();
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}
// reset target lean angles and heading while landed
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if (ap.land_complete) {
attitude_control.init_targets();
// move throttle to minimum to keep us on the ground
attitude_control.set_throttle_out(0, false);
}else{
// call attitude controller
attitude_control.angleef_rp_rateef_y(target_roll, target_pitch, target_yaw_rate);
// body-frame rate controller is run directly from 100hz loop
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// call throttle controller
if (sonar_alt_health >= SONAR_ALT_HEALTH_MAX) {
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// if sonar is ok, use surface tracking
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get_throttle_surface_tracking(target_climb_rate);
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}else{
// if no sonar fall back stabilize rate controller
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pos_control.climb_at_rate(target_climb_rate);
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}
}
// refetch angle targets for reporting
const Vector3f angle_target = attitude_control.angle_ef_targets();
control_roll = angle_target.x;
control_pitch = angle_target.y;
control_yaw = angle_target.z;
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}
// auto_init - initialise auto controller
static bool auto_init(bool ignore_checks)
{
return true;
}
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// auto_run - runs the auto controller
// should be called at 100hz or more
static void auto_run()
{
Vector3f angle_target;
// run way point controller
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// copy latest output from nav controller to stabilize controller
angle_target.x = wp_nav.get_roll();
angle_target.y = wp_nav.get_pitch();
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// To-Do: handle pilot input for yaw and different methods to update yaw (ROI, face next wp)
angle_target.z = control_yaw;
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// To-Do: shorten below by moving these often used steps into a single function in the AC_AttitudeControl lib
// set earth-frame angular targets
attitude_control.angle_ef_targets(angle_target);
// convert earth-frame angle targets to earth-frame rate targets
attitude_control.angle_to_rate_ef_roll();
attitude_control.angle_to_rate_ef_pitch();
attitude_control.angle_to_rate_ef_yaw();
// convert earth-frame rates to body-frame rates
attitude_control.rate_ef_targets_to_bf();
// body-frame rate controller is run directly from 100hz loop
}
// circle_init - initialise circle controller
static bool circle_init(bool ignore_checks)
{
return true;
}
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// circle_run - runs the circle controller
// should be called at 100hz or more
static void circle_run()
{
}
// loiter_init - initialise loiter controller
static bool loiter_init(bool ignore_checks)
{
if (GPS_ok() || ignore_checks) {
// set target to current position
// To-Do: supply zero velocity below?
wp_nav.init_loiter_target();
return true;
}else{
return false;
}
}
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// loiter_run - runs the loiter controller
// should be called at 100hz or more
static void loiter_run()
{
float target_yaw_rate = 0;
float target_climb_rate = 0;
// if not auto armed set throttle to zero and exit immediately
if(!ap.auto_armed || !inertial_nav.position_ok()) {
wp_nav.init_loiter_target();
attitude_control.init_targets();
attitude_control.set_throttle_out(0, false);
return;
}
// process pilot inputs
if (!failsafe.radio) {
// apply SIMPLE mode transform to pilot inputs
update_simple_mode();
// process pilot's roll and pitch input
// To-Do: do we need to clear out feed forward if this is not called?
wp_nav.set_pilot_desired_acceleration(g.rc_1.control_in, g.rc_2.control_in);
// get pilot's desired yaw rate
target_yaw_rate = get_pilot_desired_yaw_rate(g.rc_4.control_in);
// get pilot desired climb rate
target_climb_rate = get_pilot_desired_climb_rate(g.rc_3.control_in);
// check for pilot requested take-off
if (ap.land_complete && target_climb_rate > 0) {
// indicate we are taking off
set_land_complete(false);
// clear i term when we're taking off
set_throttle_takeoff();
}
}
// when landed reset targets and output zero throttle
if (ap.land_complete) {
wp_nav.init_loiter_target();
attitude_control.init_targets();
attitude_control.set_throttle_out(0, false);
}else{
// run loiter controller
wp_nav.update_loiter();
// call attitude controller
attitude_control.angleef_rp_rateef_y(wp_nav.get_roll(), wp_nav.get_pitch(), target_yaw_rate);
// body-frame rate controller is run directly from 100hz loop
// run altitude controller
if (sonar_alt_health >= SONAR_ALT_HEALTH_MAX) {
// if sonar is ok, use surface tracking
get_throttle_surface_tracking(target_climb_rate);
}else{
// if no sonar fall back stabilize rate controller
pos_control.climb_at_rate(target_climb_rate);
}
}
// refetch angle targets for reporting
const Vector3f angle_target = attitude_control.angle_ef_targets();
control_roll = angle_target.x;
control_pitch = angle_target.y;
control_yaw = angle_target.z;
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}
// guided_init - initialise guided controller
static bool guided_init(bool ignore_checks)
{
return true;
}
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// guided_run - runs the guided controller
// should be called at 100hz or more
static void guided_run()
{
}
// land_init - initialise land controller
static bool land_init(bool ignore_checks)
{
return true;
}
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// land_run - runs the land controller
// should be called at 100hz or more
static void land_run()
{
verify_land();
}
// rtl_init - initialise rtl controller
static bool rtl_init(bool ignore_checks)
{
return true;
}
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// rtl_run - runs the return-to-launch controller
// should be called at 100hz or more
static void rtl_run()
{
verify_RTL();
}
// ofloiter_init - initialise ofloiter controller
static bool ofloiter_init(bool ignore_checks)
{
return true;
}
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// ofloiter_run - runs the optical flow loiter controller
// should be called at 100hz or more
static void ofloiter_run()
{
}
// drift_init - initialise drift controller
static bool drift_init(bool ignore_checks)
{
return true;
}
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// drift_run - runs the drift controller
// should be called at 100hz or more
static void drift_run()
{
}
// sport_init - initialise sport controller
static bool sport_init(bool ignore_checks)
{
return true;
}
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// sport_run - runs the sport controller
// should be called at 100hz or more
static void sport_run()
{
}