AerialVehicleControl.jl
cont_power_distribution.h
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1 /*******************************************************************************
2 * Copyright (C) Marcus Greiff 2020
3 *
4 * @file cont_power_distribution.h
5 * @author Marcus Greiff
6 * @date June 2020
7 *******************************************************************************/
8 #ifndef __CONT_POWER_DISTRIBUTION_H__
9 #define __CONT_POWER_DISTRIBUTION_H__
10 
11 #include "cont_math.h"
12 
13 /***************************************************************************/
47 int compute_power_distribution(
48  con_state_qw_fsf_t * controller,
49  matrix_double_t * dutyCycles
50 );
51 
52 #endif /* __CONT_POWER_DISTRIBUTION_H__ */
cont_math.h
matrix_double_s
Matrix object used for all matrix manipulation.
Definition: cont_types.h:50
con_state_qw_fsf_s
Complete state of the attitude FSF on SO(3) or SU(2)
Definition: cont_types.h:67
compute_power_distribution
int compute_power_distribution(con_state_qw_fsf_t *controller, matrix_double_t *dutyCycles)
Compute the desired rotor thrusts.
Definition: cont_power_distribution.c:10