stabilisation_wing_t Struct Reference

Structure containing the pointers to the data needed in this module. More...

#include <stabilisation_wing.hpp>

Collaboration diagram for stabilisation_wing_t:

List of all members.

Public Attributes
stabiliser_stack_wing_t	stabiliser_stack
	The pointer to the PID parameters values for the stacked controller.
control_command_t *	controls
	The pointer to the control structure.
torque_command_t *	torque_command
	The pointer to the torque command (output)
thrust_command_t *	thrust_command
	The pointer to the thrust command (output)
const Imu *	imu
	The pointer to the IMU structure.
const ahrs_t *	ahrs
	The pointer to the attitude estimation structure.
const INS *	ins
	The pointer to the position estimation structure.
const Airspeed_analog *	airspeed_analog
	The pointer to the analog airspeed sensor structure.
const Navigation *	navigation
	The pointer to the navigation structure.
const Gps *	gps
	The pointer to the GPS structure.
float	thrust_apriori
	A priori on the thrust for velocity control.
float	pitch_angle_apriori
	Constant a priori on the pitch angle.
float	pitch_angle_apriori_gain
	Gain of the pitch angle a priori which is function of the roll value.
float	max_roll_angle
	Maximum roll value that the velocity layer could ask to follow.
float	take_off_thrust
	Thrust value used during the take-off.
float	take_off_pitch
	Pitch angle used during the take-off.
float	landing_pitch
	Pitch angle used during the landing.
float	landing_max_roll
	Maximum roll angle during landing.
float	dt_s
	Time interval between to updates.
float	last_update_s
	Last update in seconds.

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Detailed Description

Structure containing the pointers to the data needed in this module.

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The documentation for this struct was generated from the following file:

• /home/travis/build/lis-epfl/MAVRIC_Library/control/unsupported/stabilisation_wing.hpp