Paparazzi UAS  v7.0_unstable
Paparazzi is a free software Unmanned Aircraft System.
guidance_common.h File Reference

Vertical control for fixed wing vehicles. More...

#include <inttypes.h>
#include "paparazzi.h"
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Go to the source code of this file.

Macros

#define V_CTL_MODE_MANUAL   0
 
#define V_CTL_MODE_AUTO_THROTTLE   1
 
#define V_CTL_MODE_AUTO_CLIMB   2
 
#define V_CTL_MODE_AUTO_ALT   3
 
#define V_CTL_MODE_LANDING   4
 
#define V_CTL_MODE_NB   5
 
#define V_CTL_CLIMB_MODE_AUTO_THROTTLE   0
 
#define V_CTL_CLIMB_MODE_AUTO_PITCH   1
 
#define V_CTL_AUTO_THROTTLE_STANDARD   0
 
#define V_CTL_AUTO_THROTTLE_AGRESSIVE   1
 
#define V_CTL_AUTO_THROTTLE_BLENDED   2
 
#define guidance_v_SetCruiseThrottle(_v)
 
#define guidance_v_SetAutoThrottleIgain(_v)
 

Functions

void v_ctl_init (void)
 
void v_ctl_altitude_loop (void)
 outer loop More...
 
void v_ctl_climb_loop (void)
 Auto-throttle inner loop. More...
 
void v_ctl_landing_loop (void)
 
void v_ctl_guidance_loop (void)
 General guidance logic This will call the proper control loops according to the sub-modes. More...
 
void v_ctl_throttle_slew (void)
 Computes throttle_slewed from throttle_setpoint. More...
 

Variables

uint8_t v_ctl_mode
 
float v_ctl_climb_setpoint
 
uint8_t v_ctl_climb_mode
 
uint8_t v_ctl_auto_throttle_submode
 
float v_ctl_auto_throttle_sum_err
 
float v_ctl_altitude_error
 in meters, (setpoint - alt) -> positive = too low More...
 
float v_ctl_auto_airspeed_controlled
 
float v_ctl_auto_groundspeed_setpoint
 in meters per second More...
 
float v_ctl_auto_throttle_cruise_throttle
 
pprz_t v_ctl_throttle_setpoint
 
pprz_t v_ctl_throttle_slewed
 
float v_ctl_pitch_setpoint
 

Detailed Description

Vertical control for fixed wing vehicles.

Definition in file guidance_common.h.

Macro Definition Documentation

◆ guidance_v_SetAutoThrottleIgain

#define guidance_v_SetAutoThrottleIgain (   _v)
Value:
{ \
v_ctl_auto_throttle_igain = _v; \
v_ctl_auto_throttle_sum_err = 0; \
}

Definition at line 88 of file guidance_common.h.

◆ guidance_v_SetCruiseThrottle

#define guidance_v_SetCruiseThrottle (   _v)
Value:
{ \
v_ctl_auto_throttle_cruise_throttle = (_v ? _v : v_ctl_auto_throttle_nominal_cruise_throttle); \
}
float v_ctl_auto_throttle_nominal_cruise_throttle
Definition: energy_ctrl.c:104
float v_ctl_auto_throttle_min_cruise_throttle
Definition: guidance_v.c:58
float v_ctl_auto_throttle_max_cruise_throttle
Definition: guidance_v.c:59
float v_ctl_auto_throttle_cruise_throttle
Definition: energy_ctrl.c:103

Definition at line 83 of file guidance_common.h.

◆ V_CTL_AUTO_THROTTLE_AGRESSIVE

#define V_CTL_AUTO_THROTTLE_AGRESSIVE   1

Definition at line 52 of file guidance_common.h.

◆ V_CTL_AUTO_THROTTLE_BLENDED

#define V_CTL_AUTO_THROTTLE_BLENDED   2

Definition at line 53 of file guidance_common.h.

◆ V_CTL_AUTO_THROTTLE_STANDARD

#define V_CTL_AUTO_THROTTLE_STANDARD   0

Definition at line 51 of file guidance_common.h.

◆ V_CTL_CLIMB_MODE_AUTO_PITCH

#define V_CTL_CLIMB_MODE_AUTO_PITCH   1

Definition at line 48 of file guidance_common.h.

◆ V_CTL_CLIMB_MODE_AUTO_THROTTLE

#define V_CTL_CLIMB_MODE_AUTO_THROTTLE   0

Definition at line 47 of file guidance_common.h.

◆ V_CTL_MODE_AUTO_ALT

#define V_CTL_MODE_AUTO_ALT   3

Definition at line 39 of file guidance_common.h.

◆ V_CTL_MODE_AUTO_CLIMB

#define V_CTL_MODE_AUTO_CLIMB   2

Definition at line 38 of file guidance_common.h.

◆ V_CTL_MODE_AUTO_THROTTLE

#define V_CTL_MODE_AUTO_THROTTLE   1

Definition at line 37 of file guidance_common.h.

◆ V_CTL_MODE_LANDING

#define V_CTL_MODE_LANDING   4

Definition at line 40 of file guidance_common.h.

◆ V_CTL_MODE_MANUAL

#define V_CTL_MODE_MANUAL   0

Definition at line 36 of file guidance_common.h.

◆ V_CTL_MODE_NB

#define V_CTL_MODE_NB   5

Definition at line 41 of file guidance_common.h.

Function Documentation

◆ v_ctl_altitude_loop()

◆ v_ctl_climb_loop()

void v_ctl_climb_loop ( void  )

Auto-throttle inner loop.

Definition at line 324 of file energy_ctrl.c.

References ac_char_update(), accel_imu_meas, ACCELS_FLOAT_OF_BFP, AIRSPEED_SETPOINT_SLEW, autopilot, autopilot_throttle_killed(), controlled_throttle, dt_attidude, pprz_autopilot::launch, low_pass_vdot(), MAX_PPRZ, nav_pitch, stateGetAirspeed_f(), stateGetHorizontalSpeedNorm_f(), stateGetNedToBodyEulers_f(), stateGetSpeedEnu_f(), TRIM_UPPRZ, v_ctl_airspeed_pgain, v_ctl_auto_airspeed_controlled, v_ctl_auto_airspeed_setpoint, v_ctl_auto_airspeed_setpoint_slew, v_ctl_auto_groundspeed_igain, V_CTL_AUTO_GROUNDSPEED_MAX_SUM_ERR, v_ctl_auto_groundspeed_pgain, v_ctl_auto_groundspeed_setpoint, v_ctl_auto_groundspeed_sum_err, v_ctl_auto_pitch_of_airspeed_dgain, v_ctl_auto_pitch_of_airspeed_igain, v_ctl_auto_pitch_of_airspeed_pgain, v_ctl_auto_throttle_climb_throttle_increment, v_ctl_auto_throttle_cruise_throttle, v_ctl_auto_throttle_nominal_cruise_pitch, v_ctl_auto_throttle_nominal_cruise_throttle, v_ctl_auto_throttle_of_airspeed_igain, v_ctl_auto_throttle_of_airspeed_pgain, v_ctl_auto_throttle_pitch_of_vz_pgain, v_ctl_climb_auto_throttle_loop(), v_ctl_climb_mode, V_CTL_CLIMB_MODE_AUTO_PITCH, V_CTL_CLIMB_MODE_AUTO_THROTTLE, v_ctl_climb_setpoint, v_ctl_desired_acceleration, v_ctl_energy_diff_igain, v_ctl_energy_diff_pgain, v_ctl_energy_total_igain, v_ctl_energy_total_pgain, V_CTL_GLIDE_RATIO, v_ctl_max_acceleration, v_ctl_mode, V_CTL_MODE_AUTO_CLIMB, v_ctl_pitch_setpoint, v_ctl_set_pitch(), v_ctl_set_throttle(), V_CTL_SPEED_AIRSPEED, V_CTL_SPEED_GROUNDSPEED, v_ctl_speed_mode, V_CTL_SPEED_THROTTLE, v_ctl_throttle_setpoint, FloatVect3::x, and EnuCoor_f::z.

Referenced by attitude_loop(), and v_ctl_guidance_loop().

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◆ v_ctl_guidance_loop()

void v_ctl_guidance_loop ( void  )

◆ v_ctl_init()

void v_ctl_init ( void  )

Definition at line 208 of file energy_ctrl.c.

References accel_cb(), accel_ev, controlled_throttle, v_ctl_airspeed_pgain, v_ctl_altitude_error, V_CTL_ALTITUDE_MAX_CLIMB, v_ctl_altitude_max_climb, v_ctl_altitude_pgain, v_ctl_altitude_pre_climb, v_ctl_altitude_pre_climb_correction, V_CTL_ALTITUDE_PRE_CLIMB_CORRECTION, v_ctl_altitude_setpoint, v_ctl_auto_airspeed_controlled, v_ctl_auto_airspeed_pitch_dgain, v_ctl_auto_airspeed_pitch_igain, v_ctl_auto_airspeed_pitch_pgain, v_ctl_auto_airspeed_pitch_sum_err, v_ctl_auto_airspeed_setpoint, v_ctl_auto_airspeed_setpoint_slew, v_ctl_auto_airspeed_throttle_dgain, v_ctl_auto_airspeed_throttle_igain, v_ctl_auto_airspeed_throttle_pgain, v_ctl_auto_airspeed_throttle_sum_err, v_ctl_auto_groundspeed_igain, v_ctl_auto_groundspeed_pgain, v_ctl_auto_groundspeed_setpoint, v_ctl_auto_groundspeed_sum_err, v_ctl_auto_pitch_dgain, V_CTL_AUTO_PITCH_DGAIN, v_ctl_auto_pitch_igain, V_CTL_AUTO_PITCH_IGAIN, v_ctl_auto_pitch_of_airspeed_dgain, v_ctl_auto_pitch_of_airspeed_igain, v_ctl_auto_pitch_of_airspeed_pgain, v_ctl_auto_pitch_pgain, v_ctl_auto_pitch_sum_err, v_ctl_auto_throttle_climb_throttle_increment, v_ctl_auto_throttle_cruise_throttle, V_CTL_AUTO_THROTTLE_DGAIN, v_ctl_auto_throttle_dgain, v_ctl_auto_throttle_igain, v_ctl_auto_throttle_max_cruise_throttle, v_ctl_auto_throttle_min_cruise_throttle, v_ctl_auto_throttle_nominal_cruise_pitch, v_ctl_auto_throttle_nominal_cruise_throttle, v_ctl_auto_throttle_of_airspeed_igain, v_ctl_auto_throttle_of_airspeed_pgain, v_ctl_auto_throttle_pgain, v_ctl_auto_throttle_pitch_of_vz_dgain, V_CTL_AUTO_THROTTLE_PITCH_OF_VZ_DGAIN, v_ctl_auto_throttle_pitch_of_vz_pgain, V_CTL_AUTO_THROTTLE_STANDARD, v_ctl_auto_throttle_submode, v_ctl_auto_throttle_sum_err, v_ctl_climb_mode, V_CTL_CLIMB_MODE_AUTO_THROTTLE, v_ctl_climb_setpoint, v_ctl_energy_diff_igain, v_ctl_energy_diff_pgain, V_CTL_ENERGY_IMU_ID, v_ctl_energy_total_igain, v_ctl_energy_total_pgain, v_ctl_max_acceleration, V_CTL_MAX_ACCELERATION, v_ctl_max_climb, v_ctl_mode, V_CTL_MODE_MANUAL, v_ctl_pitch_setpoint, V_CTL_PITCH_TRIM, v_ctl_pitch_trim, v_ctl_speed_mode, V_CTL_SPEED_THROTTLE, and v_ctl_throttle_setpoint.

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◆ v_ctl_landing_loop()

void v_ctl_landing_loop ( void  )

◆ v_ctl_throttle_slew()

void v_ctl_throttle_slew ( void  )

Computes throttle_slewed from throttle_setpoint.

Computes throttle_slewed from throttle_setpoint.

Definition at line 437 of file energy_ctrl.c.

References MAX_PPRZ, TRIM_PPRZ, v_ctl_throttle_setpoint, V_CTL_THROTTLE_SLEW, and v_ctl_throttle_slewed.

Referenced by attitude_loop().

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Variable Documentation

◆ v_ctl_altitude_error

float v_ctl_altitude_error
extern

in meters, (setpoint - alt) -> positive = too low

Definition at line 92 of file energy_ctrl.c.

Referenced by h_ctl_course_loop(), v_ctl_altitude_loop(), v_ctl_climb_auto_throttle_loop(), and v_ctl_init().

◆ v_ctl_auto_airspeed_controlled

float v_ctl_auto_airspeed_controlled
extern

Definition at line 123 of file energy_ctrl.c.

Referenced by send_airspeed(), v_ctl_climb_loop(), and v_ctl_init().

◆ v_ctl_auto_groundspeed_setpoint

float v_ctl_auto_groundspeed_setpoint
extern

in meters per second

Definition at line 125 of file energy_ctrl.c.

Referenced by send_airspeed(), v_ctl_climb_loop(), and v_ctl_init().

◆ v_ctl_auto_throttle_cruise_throttle

float v_ctl_auto_throttle_cruise_throttle
extern

◆ v_ctl_auto_throttle_submode

uint8_t v_ctl_auto_throttle_submode
extern

◆ v_ctl_auto_throttle_sum_err

float v_ctl_auto_throttle_sum_err
extern

◆ v_ctl_climb_mode

uint8_t v_ctl_climb_mode
extern

Definition at line 75 of file energy_ctrl.c.

Referenced by v_ctl_altitude_loop(), v_ctl_climb_loop(), and v_ctl_init().

◆ v_ctl_climb_setpoint

◆ v_ctl_mode

◆ v_ctl_pitch_setpoint

◆ v_ctl_throttle_setpoint

◆ v_ctl_throttle_slewed

pprz_t v_ctl_throttle_slewed
extern

Definition at line 132 of file energy_ctrl.c.

Referenced by attitude_loop(), and v_ctl_throttle_slew().