AerialVehicleControl.jl
cont_attitude_FSF_SU2_discontinuous.h
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1 /*******************************************************************************
2 * Copyright (C) Marcus Greiff 2020
3 *
4 * @file cont_attitude_FSF_SU2_discontinuous.h
5 * @author Marcus Greiff
6 * @date June 2020
7 *******************************************************************************/
8 #ifndef __CONT_ATTITUDE_FSF_SU2_DISCONTINUOUS_H__
9 #define __CONT_ATTITUDE_FSF_SU2_DISCONTINUOUS_H__
10 
11 #include "cont_attitude_utils.h"
12 
13 /***************************************************************************/
28 int update_attitude_FSF_SU2_discontinuous(
29  ref_state_qw_t * reference,
30  dyn_state_qw_t * state,
31  con_state_qw_fsf_t * controller
32 );
33 
34 #endif /* __CONT_ATTITUDE_FSF_SU2_DISCONTINUOUS_H__ */
cont_attitude_utils.h
ref_state_qw_s
Reference signal structure for the attitude FSF on S(3) or SU(2)
Definition: cont_types.h:111
con_state_qw_fsf_s
Complete state of the attitude FSF on SO(3) or SU(2)
Definition: cont_types.h:67
update_attitude_FSF_SU2_discontinuous
int update_attitude_FSF_SU2_discontinuous(ref_state_qw_t *reference, dyn_state_qw_t *state, con_state_qw_fsf_t *controller)
Update using the discontinuous full state feedback (FSF) on SU(2)
Definition: cont_attitude_FSF_SU2_discontinuous.c:10
dyn_state_qw_s
Dynamical states, assumed known in the attitude FSF on SO(3) or SU(2)
Definition: cont_types.h:59