MAV'RIC
/home/travis/build/lis-epfl/MAVRIC_Library/util/coord_conventions.hpp
00001 /*******************************************************************************
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00031 
00032 /*******************************************************************************
00033  * \file coord_conventions.h
00034  *
00035  * \author MAV'RIC Team
00036  * \author Julien Lecoeur
00037  *
00038  * \brief Coordinate conventions
00039  *
00040  ******************************************************************************/
00041 
00042 
00043 #ifndef COORD_CONVENTIONS_HPP_
00044 #define COORD_CONVENTIONS_HPP_
00045 
00046 #include <cstdint>
00047 #include <array>
00048 
00049 extern "C"
00050 {
00051 #include "util/quaternions.h"
00052 }
00053 
00054 
00055 #define EARTH_RADIUS 6378137.0f                 ///< radius of the earth in meters
00056 
00057 
00061 typedef struct
00062 {
00063     double longitude;           
00064     double latitude;            
00065     float altitude;             
00066 } global_position_t;
00067 
00068 typedef std::array<float,3> local_position_t;
00069 
00070 typedef std::array<float,3> local_velocity_t;
00071 
00072 /*
00073  * \brief       Attitude with aeronautics convention
00074  *
00075  * \details     Expressed with the NED frame: X front, Y right, Z down.
00076  *              The rotations are done in the following order:
00077  *              - first around the local yaw axis,
00078  *              - then around new local pitch axis,
00079  *              - and finally around the new roll axis
00080 */
00081 typedef struct
00082 {
00083     float rpy[3];   
00084 } aero_attitude_t;
00085 
00086 
00097 void coord_conventions_local_to_global_position(const local_position_t& input, const global_position_t& origin, global_position_t& output);
00098 
00099 
00107 void coord_conventions_global_to_local_position(const global_position_t& input, const global_position_t& origin, local_position_t& output);
00108 
00109 
00117 aero_attitude_t coord_conventions_quat_to_aero(quat_t qe);
00118 
00119 
00127 quat_t coord_conventions_quaternion_from_aero(aero_attitude_t aero);
00128 
00136 quat_t coord_conventions_quaternion_from_rpy(const float rpy[3]);
00137 quat_t coord_conventions_quaternion_from_rpy(float roll, float pitch, float yaw);
00138 
00139 
00146 void coord_conventions_rpy_from_quaternion(const quat_t& quat, float rpy[3]);
00147 
00148 
00156 float coord_conventions_get_yaw(quat_t qe);
00157 
00158 
00167 quat_t coord_conventions_quaternion_from_angle_axis(float angle, const float axis[3]);
00168 
00169 
00170 #endif /* STABILISATION_HPP_ */
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