Struct LunarGnssODTSConfig¶

Defined in File lunar_gnss_odts_simulation.h

Struct Documentation¶

struct LunarGnssODTSConfig¶

Public Members

int seed = 42¶

int monte_carlo_runs = 1¶

double duration_s = 3600.0¶

double dt_s = 60.0¶

double ephemeris_dt_s = 60.0¶

std::filesystem::path output_dir = "output/gnss_filtering"¶

std::filesystem::path links_file¶

std::filesystem::path delays_file¶

ReceiverAppConfig receiver_app¶

DesignConfig design¶

PlasmaDelayConfig plasma¶

ConstellationSourceConfig constellation¶

std::string start_epoch_utc = "2025-01-01T12:00:00"¶

double receiver_a_m = 6541.4e3¶

double receiver_ecc = 0.6¶

double receiver_inc_rad = 65.5 * lupnt::RAD ¶

double receiver_raan_rad = 60.0 * lupnt::RAD ¶

double receiver_argp_rad = 90.0 * lupnt::RAD ¶

double receiver_mean_anomaly_rad = 0.0¶

double clock_bias_s = 0.0¶

double clock_drift_sps = 0.0¶

int moon_gravity_degree_truth = 20¶

int moon_gravity_order_truth = 20¶

int moon_gravity_degree_filter = 12¶

int moon_gravity_order_filter = 12¶

int moon_gravity_degree_constellation = 12¶

int moon_gravity_order_constellation = 12¶

bool include_earth = true¶

bool include_sun = true¶

bool use_relativity = true¶

bool use_srp_truth = false¶

bool use_srp_filter = false¶

double srp_coeff_truth_m2_kg = 2.0e-3¶

double srp_coeff_filter_m2_kg = 2.0e-3¶

double pseudorange_sigma_m = 2.0¶

double doppler_sigma_hz = 0.1¶

bool use_pseudorange = true¶

bool use_doppler = true¶

bool use_tdcp = false¶

double carrier_phase_sigma_m = 0.01¶

double tdcp_sigma_m = 0.02¶

bool estimate_srp_coefficient = false¶

double initial_srp_coeff_m2_kg = 2.0e-3¶

double initial_position_sigma_m = 100.0¶

double initial_velocity_sigma_mps = 0.1¶

double initial_clock_bias_sigma_s = 1.0e-6¶

double initial_clock_drift_sigma_sps = 1.0e-9¶

double initial_srp_coeff_sigma_m2_kg = 1.0e-3¶

double process_accel_sigma_mps2 = 1.0e-7¶

double process_clock_bias_sigma_s_sqrt_s = 1.0e-11¶

double process_clock_drift_sigma_sps_sqrt_s = 1.0e-13¶

double process_srp_coeff_sigma_m2_kg_sqrt_s = 1.0e-10¶

double integration_step_s = 20.0¶