Struct GnssMeasurementOptions¶
Defined in File gnss_measurement.h
Struct Documentation¶
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struct GnssMeasurementOptions¶
Public Members
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std::vector<GnssObservable> observables = {GnssObservable::PSEUDORANGE, GnssObservable::DOPPLER, GnssObservable::CARRIER_PHASE}¶
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GnssMeasurementStateIndices indices¶
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ClockBiasUnit clock_bias_unit = ClockBiasUnit::SECONDS¶
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Time receive_time_scale = Time::TAI¶
Epochs passed to
GNSSMeasurements::Compute/Precomputeare receiver signal-reception epochs in this time scale.
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Time ephemeris_time_scale = Time::TAI¶
GNSS constellation ephemeris epochs are represented in this scale.
GnssConstellationstores its tables as TAI seconds by convention.
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bool solve_light_time = true¶
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bool recompute_transmit_time_from_ephemeris = false¶
If true,
GnssMeasurement::Computeresolves the transmit epoch from the current user state and the channel ephemeris coefficients instead of reusing the transmit epoch stored in the precomputed channel. This is intended for estimated/filter measurements; truth generation can keep the precomputed light-time solution tied to the truth state.
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int light_time_max_iterations = 10¶
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bool apply_transmitter_relativity = true¶
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bool apply_shapiro_delay = true¶
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Vec3 shapiro_body_position = Vec3::Zero()¶
Deprecated: Shapiro delay is currently evaluated using SunPosition().
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bool apply_visibility = true¶
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bool apply_cn0_threshold = true¶
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bool apply_ionosphere_plasma_delay = false¶
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std::vector<GnssObservable> observables = {GnssObservable::PSEUDORANGE, GnssObservable::DOPPLER, GnssObservable::CARRIER_PHASE}¶