AerialVehicleControl.jl
dyn_state_qw_s Struct Reference

Dynamical states, assumed known in the attitude FSF on SO(3) or SU(2) More...

#include <cont_types.h>

Data Fields

double quaternion [4]
 
double omega [3]
 

Detailed Description

Dynamical states, assumed known in the attitude FSF on SO(3) or SU(2)

Definition at line 59 of file cont_types.h.

Field Documentation

◆ omega

double dyn_state_qw_s::omega[3]

Attitude rates

Definition at line 61 of file cont_types.h.

◆ quaternion

double dyn_state_qw_s::quaternion[4]

Quaternion attitude

Definition at line 60 of file cont_types.h.


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