Paparazzi UAS
v5.14.0_stable-0-g3f680d1
Paparazzi is a free software Unmanned Aircraft System.
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Fixed wing horizontal control. More...
Go to the source code of this file.
Functions | |
void | h_ctl_init (void) |
void | h_ctl_course_loop (void) |
void | h_ctl_attitude_loop (void) |
Variables | |
float | h_ctl_course_setpoint |
float | h_ctl_course_pre_bank |
float | h_ctl_course_pre_bank_correction |
float | h_ctl_course_pgain |
float | h_ctl_course_dgain |
float | h_ctl_roll_max_setpoint |
bool | h_ctl_disabled |
bool | h_ctl_auto1_rate |
float | h_ctl_roll_setpoint |
float | h_ctl_roll_pgain |
pprz_t | h_ctl_aileron_setpoint |
float | h_ctl_roll_slew |
float | h_ctl_pitch_setpoint |
float | h_ctl_pitch_loop_setpoint |
float | h_ctl_pitch_pgain |
float | h_ctl_pitch_dgain |
pprz_t | h_ctl_elevator_setpoint |
float | h_ctl_aileron_of_throttle |
float | h_ctl_elevator_of_roll |
float | h_ctl_roll_attitude_gain |
float | h_ctl_roll_rate_gain |
Fixed wing horizontal control.
Definition in file stabilization_attitude.h.
void h_ctl_attitude_loop | ( | void | ) |
Definition at line 413 of file stabilization_adaptive.c.
References h_ctl_disabled, h_ctl_pitch_loop(), and h_ctl_roll_loop().
Referenced by attitude_loop().
void h_ctl_course_loop | ( | void | ) |
Definition at line 374 of file stabilization_adaptive.c.
References autopilot, h_ctl_course_dgain, h_ctl_course_pgain, h_ctl_course_pre_bank, h_ctl_course_pre_bank_correction, h_ctl_course_setpoint, h_ctl_roll_max_setpoint, h_ctl_roll_setpoint, h_ctl_roll_slew, pprz_autopilot::launch, Max, Min, FloatEulers::psi, stateGetHorizontalSpeedDir_f(), stateGetHorizontalSpeedNorm_f(), stateGetNedToBodyEulers_f(), v_ctl_altitude_error, V_CTL_AUTO_THROTTLE_AGRESSIVE, V_CTL_AUTO_THROTTLE_BLENDED, and v_ctl_auto_throttle_submode.
Referenced by h_ctl_guidance_loop(), and navigation_task().
void h_ctl_init | ( | void | ) |
Definition at line 298 of file stabilization_adaptive.c.
References DefaultPeriodic, h_ctl_aileron_of_throttle, h_ctl_aileron_setpoint, h_ctl_course_dgain, H_CTL_COURSE_DGAIN, h_ctl_course_pgain, h_ctl_course_pre_bank, h_ctl_course_pre_bank_correction, H_CTL_COURSE_PRE_BANK_CORRECTION, h_ctl_course_setpoint, h_ctl_disabled, h_ctl_elevator_of_roll, h_ctl_elevator_setpoint, h_ctl_pitch_dgain, H_CTL_PITCH_DGAIN, H_CTL_PITCH_IGAIN, H_CTL_PITCH_KFFA, H_CTL_PITCH_KFFD, h_ctl_pitch_loop_setpoint, h_ctl_pitch_pgain, h_ctl_pitch_setpoint, h_ctl_ref, H_CTL_REF_MAX_P, H_CTL_REF_MAX_P_DOT, H_CTL_REF_MAX_Q, H_CTL_REF_MAX_Q_DOT, h_ctl_roll_attitude_gain, H_CTL_ROLL_IGAIN, H_CTL_ROLL_KFFA, H_CTL_ROLL_KFFD, h_ctl_roll_max_setpoint, h_ctl_roll_pgain, h_ctl_roll_rate_gain, H_CTL_ROLL_RATE_GAIN, h_ctl_roll_setpoint, h_ctl_roll_slew, HCtlAdaptRef::max_p, HCtlAdaptRef::max_p_dot, HCtlAdaptRef::max_q, HCtlAdaptRef::max_q_dot, register_periodic_telemetry(), send_calibration(), send_ctl_a(), and send_tune_roll().
float h_ctl_aileron_of_throttle |
Definition at line 195 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_roll_loop().
pprz_t h_ctl_aileron_setpoint |
Definition at line 164 of file stabilization_adaptive.c.
Referenced by attitude_loop(), file_logger_periodic(), h_ctl_init(), and h_ctl_roll_loop().
bool h_ctl_auto1_rate |
Definition at line 91 of file stabilization_adaptive.c.
Referenced by h_ctl_roll_loop(), and navigation_task().
float h_ctl_course_dgain |
Definition at line 84 of file stabilization_adaptive.c.
Referenced by h_ctl_course_loop(), and h_ctl_init().
float h_ctl_course_pgain |
Definition at line 83 of file stabilization_adaptive.c.
Referenced by fly_to_xy(), h_ctl_course_loop(), and h_ctl_init().
float h_ctl_course_pre_bank |
Definition at line 81 of file stabilization_adaptive.c.
Referenced by h_ctl_course_loop(), h_ctl_init(), and nav_periodic_task().
float h_ctl_course_pre_bank_correction |
Definition at line 82 of file stabilization_adaptive.c.
Referenced by h_ctl_course_loop(), and h_ctl_init().
float h_ctl_course_setpoint |
Definition at line 80 of file stabilization_adaptive.c.
Referenced by fly_to_xy(), h_ctl_course_loop(), h_ctl_init(), and send_desired().
bool h_ctl_disabled |
Definition at line 88 of file stabilization_adaptive.c.
Referenced by h_ctl_attitude_loop(), and h_ctl_init().
float h_ctl_elevator_of_roll |
Definition at line 196 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
pprz_t h_ctl_elevator_setpoint |
Definition at line 178 of file stabilization_adaptive.c.
Referenced by attitude_loop(), file_logger_periodic(), h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_pitch_dgain |
Definition at line 173 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_pitch_loop_setpoint |
Definition at line 171 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), h_ctl_pitch_loop(), and send_desired().
float h_ctl_pitch_pgain |
Definition at line 172 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_pitch_setpoint |
Definition at line 170 of file stabilization_adaptive.c.
Referenced by attitude_loop(), autopilot_static_on_rc_frame(), h_ctl_guidance_loop(), h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_roll_attitude_gain |
Definition at line 158 of file stabilization_adaptive.c.
Referenced by h_ctl_init().
float h_ctl_roll_max_setpoint |
Definition at line 85 of file stabilization_adaptive.c.
Referenced by fly_to_xy(), gvf_control_2D(), h_ctl_course_loop(), and h_ctl_init().
float h_ctl_roll_pgain |
Definition at line 167 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_roll_loop().
float h_ctl_roll_rate_gain |
Definition at line 159 of file stabilization_adaptive.c.
Referenced by h_ctl_init().
float h_ctl_roll_setpoint |
Definition at line 157 of file stabilization_adaptive.c.
Referenced by autopilot_static_on_rc_frame(), fly_to_xy(), gvf_control_2D(), h_ctl_course_loop(), h_ctl_init(), h_ctl_roll_loop(), nav_without_gps(), send_desired(), and v_ctl_landing_loop().
float h_ctl_roll_slew |
Definition at line 165 of file stabilization_adaptive.c.
Referenced by h_ctl_course_loop(), and h_ctl_init().