Paparazzi UAS
v5.18.0_stable
Paparazzi is a free software Unmanned Aircraft System.

Go to the source code of this file.
Macros  
#define  H_CTL_ROLL_SUM_ERR_MAX (MAX_PPRZ/2.) 
#define  H_CTL_PITCH_SUM_ERR_MAX (MAX_PPRZ/2.) 
#define  stabilization_adaptive_SetRollIGain(_gain) 
#define  stabilization_adaptive_SetPitchIGain(_gain) 
Variables  
float  h_ctl_roll_sum_err 
float  h_ctl_pitch_sum_err 
float  h_ctl_roll_igain 
float  h_ctl_pitch_igain 
float  h_ctl_roll_Kffa 
float  h_ctl_roll_Kffd 
float  h_ctl_pitch_Kffa 
float  h_ctl_pitch_Kffd 
float  h_ctl_pitch_of_roll 
bool  use_airspeed_ratio 
Fixed wing horizontal adaptive control.
Definition in file stabilization_adaptive.h.
#define H_CTL_PITCH_SUM_ERR_MAX (MAX_PPRZ/2.) 
Definition at line 54 of file stabilization_adaptive.h.
#define H_CTL_ROLL_SUM_ERR_MAX (MAX_PPRZ/2.) 
Definition at line 53 of file stabilization_adaptive.h.
#define stabilization_adaptive_SetPitchIGain  (  _gain  ) 
Definition at line 61 of file stabilization_adaptive.h.
#define stabilization_adaptive_SetRollIGain  (  _gain  ) 
Definition at line 56 of file stabilization_adaptive.h.
float h_ctl_pitch_igain 
Definition at line 174 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_pitch_Kffa 
Definition at line 176 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_pitch_Kffd 
Definition at line 177 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_pitch_of_roll 
Definition at line 197 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_pitch_sum_err 
Definition at line 175 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), h_ctl_pitch_loop(), and send_ctl_a().
float h_ctl_roll_igain 
Definition at line 160 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_roll_loop().
float h_ctl_roll_Kffa 
Definition at line 162 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_roll_loop().
float h_ctl_roll_Kffd 
Definition at line 163 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_roll_loop().
float h_ctl_roll_sum_err 
Definition at line 161 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), h_ctl_roll_loop(), and send_ctl_a().
bool use_airspeed_ratio 
Definition at line 199 of file stabilization_adaptive.c.
Referenced by h_ctl_init().