Spacecraft Control Framework 1.0
Spacecraft Control Library
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Structure for storing the data input for the mesurement function. More...
#include <sc_star_sun_mag_meas.h>
Public Attributes | |
ml_matrix | q |
ml_matrix | r_eci |
Nominal quaternion from eci to body. | |
ml_matrix | star_uv |
Position in the eci frame. | |
ml_matrix | q_b_to_sun_sensor |
Star unit vectors. | |
ml_matrix | q_b_to_star_sensor |
Quaternion from the body to the sun sensor frame. | |
ml_matrix | m_b_to_star_sensor |
Quaternion from the body to the star sensor frame. | |
ml_matrix | q_b_to_magnetometer |
Matrix from the body to the star sensor frame. | |
ml_matrix | r_magnetometer |
Quaternion from the body to the magnetometer frame. | |
ml_int_array | sun_sensor_id |
Magnetometer noise covariance. | |
double | f_scale |
ID of sun sensor data. | |
double | j_d |
Optical scale factor. | |
double | r_star |
Julian date for magnetic field. | |
double | r_sun |
Covariance for star measurement. | |
bool | use_stars |
Covariance for sun measurement. | |
bool | use_sun |
Use star measurements if true. | |
bool | use_mag |
Use sun measurements if true. | |
double | row_origin |
Use magnetometer measurements if true. More... | |
double | col_origin |
Imager column origin. | |
Structure for storing the data input for the mesurement function.
double star_sun_mag_meas_data::row_origin |
Use magnetometer measurements if true.
Imager row origin