ardupilot/ArduCopter/control_stabilize.pde

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2013-12-06 02:08:11 -04:00
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
// acro_run - runs the acro controller
// should be called at 100hz or more
static void acro_run()
{
}
// stabilize_run - runs the main stabilize controller
// should be called at 100hz or more
static void stabilize_run()
{
Vector3f angle_target; // for roll and pitch angle targets
Vector3f rate_stab_ef_target; // for yaw rate target
int16_t target_roll, target_pitch;
// 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);
angle_target.x = target_roll;
angle_target.y = target_pitch;
// 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();
// get pilot's desired yaw rate
rate_stab_ef_target.z = get_pilot_desired_yaw_rate(g.rc_4.control_in);
// set earth-frame rate stabilize target for yaw with pilot's desired yaw
// To-Do: this is quite wasteful to update the entire target vector when only yaw is used
attitude_control.rate_stab_ef_targets(rate_stab_ef_target);
// convert earth-frame stabilize rate to regular rate target
// To-Do: replace G_Dt below
attitude_control.rate_stab_ef_to_rate_ef_yaw(G_Dt);
// 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
// To-Do: add throttle control for stabilize mode here?
}
// althold_run - runs the althold controller
// should be called at 100hz or more
static void althold_run()
{
}
// auto_run - runs the auto controller
// should be called at 100hz or more
static void auto_run()
{
Vector3f angle_target;
// user input, although ignored is put into control_roll and pitch for reporting purposes
control_roll = g.rc_1.control_in;
control_pitch = g.rc_2.control_in;
// copy latest output from nav controller to stabilize controller
angle_target.x = wp_nav.get_desired_roll();
angle_target.y = wp_nav.get_desired_pitch();
// To-Do: handle yaw
angle_target.z = control_yaw;
// copy angle targets for reporting purposes
control_roll = angle_target.x;
control_pitch = angle_target.y;
// 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_run - runs the circle controller
// should be called at 100hz or more
static void circle_run()
{
}
// loiter_run - runs the loiter controller
// should be called at 100hz or more
static void loiter_run()
{
}
// guided_run - runs the guided controller
// should be called at 100hz or more
static void guided_run()
{
}
// land_run - runs the land controller
// should be called at 100hz or more
static void land_run()
{
verify_land();
}
// rtl_run - runs the return-to-launch controller
// should be called at 100hz or more
static void rtl_run()
{
verify_RTL();
}
// ofloiter_run - runs the optical flow loiter controller
// should be called at 100hz or more
static void ofloiter_run()
{
}
// drift_run - runs the drift controller
// should be called at 100hz or more
static void drift_run()
{
}
// sport_run - runs the sport controller
// should be called at 100hz or more
static void sport_run()
{
}