CTS-SAT-1-OBC-Firmware
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ADCS_orbit_params_struct_t Struct Reference

#include <adcs_types.h>

Public Attributes

double inclination_deg
 
double eccentricity
 
double ascending_node_right_ascension_deg
 
double perigee_argument_deg
 
double b_star_drag_term
 
double mean_motion_orbits_per_day
 
double mean_anomaly_deg
 
double epoch_year_point_day
 

Member Data Documentation

◆ ascending_node_right_ascension_deg

double ADCS_orbit_params_struct_t::ascending_node_right_ascension_deg

◆ b_star_drag_term

double ADCS_orbit_params_struct_t::b_star_drag_term

◆ eccentricity

double ADCS_orbit_params_struct_t::eccentricity

◆ epoch_year_point_day

double ADCS_orbit_params_struct_t::epoch_year_point_day

◆ inclination_deg

double ADCS_orbit_params_struct_t::inclination_deg

◆ mean_anomaly_deg

double ADCS_orbit_params_struct_t::mean_anomaly_deg

◆ mean_motion_orbits_per_day

double ADCS_orbit_params_struct_t::mean_motion_orbits_per_day

◆ perigee_argument_deg

double ADCS_orbit_params_struct_t::perigee_argument_deg

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