Paparazzi UAS  v4.0.4_stable-3-gf39211a
Paparazzi is a free software Unmanned Aircraft System.
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stabilization_attitude.h File Reference
#include <inttypes.h>
#include "std.h"
#include "paparazzi.h"
#include "generated/airframe.h"
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Functions

void h_ctl_init (void)
 
void h_ctl_course_loop (void)
 
void h_ctl_attitude_loop (void)
 

Variables

float h_ctl_course_setpoint
 fixed wing horizontal control More...
 
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_t h_ctl_disabled
 
bool_t 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
 

Function Documentation

void h_ctl_attitude_loop ( void  )

Definition at line 239 of file stabilization_adaptive.c.

References h_ctl_disabled, h_ctl_pitch_loop(), and h_ctl_roll_loop().

Referenced by attitude_loop().

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Variable Documentation

float h_ctl_aileron_of_throttle

Definition at line 93 of file stabilization_adaptive.c.

Referenced by h_ctl_init(), and h_ctl_roll_loop().

pprz_t h_ctl_aileron_setpoint

Definition at line 76 of file stabilization_adaptive.c.

Referenced by attitude_loop(), h_ctl_init(), and h_ctl_roll_loop().

bool_t h_ctl_auto1_rate

Definition at line 52 of file stabilization_adaptive.c.

Referenced by h_ctl_roll_loop(), and navigation_task().

float h_ctl_course_dgain

Definition at line 45 of file stabilization_adaptive.c.

Referenced by h_ctl_course_loop(), and h_ctl_init().

float h_ctl_course_pgain

Definition at line 44 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 42 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 43 of file stabilization_adaptive.c.

Referenced by h_ctl_course_loop(), and h_ctl_init().

float h_ctl_course_setpoint

fixed wing horizontal control

fixed wing horizontal control

Definition at line 41 of file stabilization_adaptive.c.

Referenced by fly_to_xy(), h_ctl_course_loop(), and h_ctl_init().

bool_t h_ctl_disabled

Definition at line 49 of file stabilization_adaptive.c.

Referenced by h_ctl_attitude_loop(), and h_ctl_init().

float h_ctl_elevator_of_roll

Definition at line 94 of file stabilization_adaptive.c.

Referenced by h_ctl_init(), and h_ctl_pitch_loop().

pprz_t h_ctl_elevator_setpoint

Definition at line 90 of file stabilization_adaptive.c.

Referenced by attitude_loop(), h_ctl_init(), and h_ctl_pitch_loop().

float h_ctl_pitch_dgain

Definition at line 85 of file stabilization_adaptive.c.

Referenced by h_ctl_init(), and h_ctl_pitch_loop().

float h_ctl_pitch_loop_setpoint

Definition at line 83 of file stabilization_adaptive.c.

Referenced by h_ctl_init(), and h_ctl_pitch_loop().

float h_ctl_pitch_pgain

Definition at line 84 of file stabilization_adaptive.c.

Referenced by h_ctl_init(), and h_ctl_pitch_loop().

float h_ctl_pitch_setpoint
float h_ctl_roll_attitude_gain

Definition at line 70 of file stabilization_adaptive.c.

Referenced by h_ctl_init(), and h_ctl_roll_loop().

float h_ctl_roll_max_setpoint

Definition at line 46 of file stabilization_adaptive.c.

Referenced by fly_to_xy(), h_ctl_course_loop(), and h_ctl_init().

float h_ctl_roll_pgain

Definition at line 79 of file stabilization_adaptive.c.

Referenced by h_ctl_init(), and h_ctl_roll_loop().

float h_ctl_roll_rate_gain

Definition at line 71 of file stabilization_adaptive.c.

Referenced by h_ctl_init(), and h_ctl_roll_loop().

float h_ctl_roll_setpoint
float h_ctl_roll_slew

Definition at line 77 of file stabilization_adaptive.c.

Referenced by h_ctl_course_loop(), and h_ctl_init().