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sidereon_core/
lib.rs

1//! # sidereon-core
2//!
3//! The complete Sidereon engine in one crate. It folds the numerical
4//! astrodynamics core (orbit propagation, force models, frames, time, SGP4)
5//! together with the GNSS domain layer (SP3, broadcast ephemeris, multi-GNSS
6//! positioning, RTK/PPP, ionosphere/troposphere, DOP).
7//!
8//! - The propagation/astro layer is always present under the [`astro`] module.
9//! - The GNSS layer lives behind the default-on `gnss` cargo feature, so a
10//!   propagation-only consumer can build with `--no-default-features` (plus
11//!   any astro features it wants) and never compile the IONEX/SP3 parsers.
12//!
13//! The GNSS façade is organized by user-facing tasks:
14//!
15//! - [`ephemeris`] - precise SP3 and broadcast ephemeris products,
16//! - [`rinex`] - RINEX navigation/observation parsing and CRINEX decoding,
17//! - [`antex`] - ANTEX receiver and satellite antenna calibration parsing,
18//! - [`combinations`] - observable linear combinations such as ionosphere-free,
19//! - [`observables`] - forward range, Doppler, and azimuth/elevation prediction,
20//! - [`velocity`] - receiver velocity and clock-drift solve from range-rate data,
21//! - [`positioning`] - single-point positioning and DOP diagnostics,
22//! - [`dgnss`] - code-differential pseudorange correction and rover pairing,
23//! - [`quality`] - pseudorange weighting, RAIM, and FDE integrity checks,
24//! - [`observation_qc`] - RINEX observation completeness and signal rollups,
25//! - [`signal`] - GPS C/A code generation, correlation, and acquisition,
26//! - [`ppp_corrections`] - static-arc PPP correction precomputation,
27//! - [`atmosphere`] - ionosphere and troposphere corrections,
28//! - [`scenario`] - deterministic synthetic GNSS observation scenarios,
29//! - [`orbit`] - compact reduced-orbit fitting/evaluation.
30//!
31//! Implementation modules (`sp3`, `rinex_nav`, `spp`, etc.) are crate-private.
32//! This is a clean public surface rather than a compatibility shim around the
33//! original implementation-shaped module layout.
34//!
35//! ## Units policy (internal representation)
36//!
37//! All quantities are stored and computed in **SI base units**, with the frame
38//! and datum encoded in the type name (per the spec's frames-in-the-type-system
39//! rule), never hidden behind a bare `position_m`:
40//!
41//! - **Length / position:** meters (`_m`). SP3 positions are ITRF/IGS-frame
42//!   ECEF meters; SPP receiver positions are WGS84/ITRF-compatible ECEF meters.
43//!   (The [`astro`] state layer works in kilometers; conversions happen
44//!   explicitly at the boundary, never implicitly.)
45//! - **Time / clock:** seconds (`_s`). Epochs are represented by the [`astro`]
46//!   time family (`Instant`/`TimeScale`), always scale-tagged; there is no bare
47//!   ambiguous epoch.
48//! - **Velocity:** meters per second (`_m_s`).
49//! - **Angles:** radians (`_rad`) internally. Degrees appear only at I/O edges
50//!   and are named `_deg`.
51//! - **Frequency:** hertz (`_hz`).
52//!
53//! Field and parameter names carry the unit suffix so the unit is visible at
54//! every call site. Matrix/vector linear algebra uses `nalgebra`
55//! (`DMatrix`/`DVector`) per the spec.
56
57extern crate self as sidereon_core;
58
59// ---------------------------------------------------------------------------
60// Astro / propagation layer. Always present. The GNSS layer below depends on
61// it via `crate::astro::*`.
62// ---------------------------------------------------------------------------
63
64mod validate;
65
66#[cfg(all(test, sidereon_repo_tests))]
67mod test_parity;
68
69pub mod astro;
70pub(crate) mod format;
71
72// ---------------------------------------------------------------------------
73// GNSS domain layer. Behind the default-on `gnss` feature so a propagation-only
74// consumer can opt out. Additional product modules are added as each lands.
75// ---------------------------------------------------------------------------
76
77mod ambiguity; // shared RTK/PPP cycle-slip policy + wide-lane/narrow-lane prep
78mod antenna; // shared ANTEX PCV/PCO zenith/azimuth interpolation kernels
79pub mod antex; // ANTEX receiver/satellite antenna parser + PCO/PCV lookup
80pub mod araim; // advanced RAIM multi-hypothesis protection levels
81pub mod bias; // Bias-SINEX and DCB bias products
82mod broadcast; // broadcast-ephemeris (GPS LNAV / Galileo I/NAV) orbit + clock
83pub mod broadcast_comparison; // broadcast-vs-precise (SISRE orbit/clock) accuracy
84pub mod carrier_phase; // carrier-phase combinations, cycle-slip detection, Hatch smoothing
85pub mod clock_stability; // Allan-family receiver clock stability estimators
86pub mod constants; // shared physical/time constants (used by astro + gnss)
87pub mod constellation; // GNSS constellation identity catalog (CelesTrak/NAVCEN)
88mod crinex; // Hatanaka (CRINEX) observation-file decoder
89pub mod data; // sans-IO GNSS product filename and archive URL catalog
90pub mod dop; // dilution-of-precision geometry (GDOP/PDOP/HDOP/VDOP/TDOP)
91pub mod error_metrics; // covariance-derived CEP, radial, and ellipse metrics
92pub mod frequencies; // canonical GNSS carrier-frequency table
93mod glonass; // GLONASS PZ-90.11 state-vector RK4 propagation
94mod ionex; // Klobuchar broadcast model + IONEX ionospheric maps
95pub mod navigation; // navigation-message bit-level codecs (GPS LNAV)
96pub mod nmea; // NMEA 0183 sentence parsing, stream grouping, and GGA writing
97pub mod ntrip; // NTRIP client sans-I/O request, response, and stream handling
98pub mod observables; // forward GNSS observable prediction
99pub mod ppp_corrections; // static-arc PPP correction tables
100pub mod precise_positioning; // static multi-epoch PPP float solve
101mod reduced_orbit; // compact mean-element orbit approximation (fitted)
102mod rinex_clock; // RINEX clock satellite-bias parsing and interpolation
103mod rinex_common; // shared RINEX header concepts (time-system label mapping)
104mod rinex_nav; // RINEX 3 navigation-message parsing (GPS/Galileo broadcast)
105mod rinex_obs; // RINEX 3 observation parsing + single-frequency pseudoranges
106mod rinex_qc; // RINEX observation/navigation lint and mechanical repair
107pub mod rtcm; // RTCM 3 differential-GNSS stream decode/encode (MSM, station, ephemeris)
108pub mod rtk; // RTK double-difference construction
109pub mod sbas;
110pub mod sbas_pl; // SBAS single-hypothesis protection levels
111pub mod scenario; // scenario-driven synthetic GNSS observable generation
112pub mod sidereal; // repeating-geometry residual filtering and period diagnostics
113pub mod signal; // GPS C/A code, coherent correlation, and acquisition
114pub mod source_localization; // ToA/TDOA source localization from arrival times
115mod sp3; // SP3-c / SP3-d parser + arbitrary-epoch interpolation
116mod spp; // single-point positioning (least-squares PVT)
117pub mod ssr; // SSR correction store and corrected broadcast ephemeris source
118pub mod staleness; // product-staleness graceful degradation for time-varying products
119mod static_positioning; // multi-epoch static position fusion
120mod tropo; // Saastamoinen zenith + Niell (NMF) mapping troposphere
121pub mod velocity; // receiver velocity / clock-drift least-squares solve
122
123mod error;
124pub mod frame;
125pub mod frame_catalog;
126mod id;
127
128pub mod atmosphere;
129pub mod combinations;
130pub mod dgnss;
131pub mod ephemeris;
132pub mod estimation; // Phase-2 estimation substrate: named operation-order recipes
133pub mod geodesic; // WGS84 geodesic direct and inverse solvers
134pub mod geodetic_time_series; // robust station velocity, trajectory, steps, and fields
135pub mod geofence; // geodesic geofence containment and uncertainty gates
136pub mod geoid; // geoid undulation grid + bilinear interpolation (orthometric heights)
137pub mod geometry;
138pub mod geometry_quality;
139pub mod ils; // integer least squares ambiguity-resolution kernels
140pub mod inertial; // ECEF strapdown INS frames, mechanization, and IMU error model
141pub mod integrity; // shared protection and covariance primitives
142pub mod observation_qc; // RINEX observation completeness and signal rollups
143pub mod qc_obs {
144    //! RINEX observation quality-control rollups.
145    pub use crate::observation_qc::*;
146}
147pub mod orbit;
148pub mod orbit_determination;
149pub mod positioning;
150pub mod prelude;
151pub mod quality; // measurement weighting, RAIM, and FDE integrity checks
152pub mod rinex;
153pub mod rtk_filter; // sequential RTK baseline filter - serializable state ABI (kernel migration)
154pub mod terrain;
155pub mod terrain_store;
156pub mod tides;
157pub mod tolerances;
158
159pub mod fusion; // GNSS/INS error-state prediction and EKF correction over the inertial surface
160
161pub use crate::astro::frames::{
162    EarthOrientation, EarthOrientationProvider, TdbEarthOrientationProvider,
163};
164pub use crate::error_metrics::{
165    error_ellipse_from_enu_m2, horizontal_radius_at, metrics_from_ecef_covariance_m2,
166    metrics_from_enu_covariance_m2, metrics_from_kinematic_solution,
167    metrics_from_position_covariance, spherical_radius_at, vertical_radius_at, ErrorEllipse,
168    ErrorMetricsError, PercentileRadius, PositionErrorMetrics,
169};
170pub use crate::estimation::{
171    alpha_beta_apply_measurement, alpha_beta_filter_step, alpha_beta_predict,
172    alpha_beta_steady_state_gains, cfar_ca_false_alarm_probability, cfar_ca_multiplier_from_pfa,
173    cfar_ca_pfa_from_multiplier, cfar_ca_threshold, ewma_update, ewma_update_power_of_two,
174    kalman_cv_steady_state_gains, mad_spread, nis_expected_value, nis_gate_test,
175    nis_gate_threshold, nis_statistic, normalized_innovation, AlphaBetaGains, AlphaBetaState,
176    AlphaBetaStep, PrimitiveError, ScalarKalmanGains, MAD_GAUSSIAN_CONSISTENCY,
177};
178pub use crate::quality::{
179    reliability_araim, reliability_design, wtest_noncentrality, wtest_noncentrality_components,
180    ObservationReliability, RangeReliabilityRow, ReliabilityOptions, ReliabilityReport,
181    ReliabilitySummary, WtestNoncentralityComponents,
182};
183pub use araim::ProtectionModel;
184pub use error::{Error, Result};
185pub use frame::{
186    geodetic_to_itrf, itrf_to_geodetic, FrameValueError, ItrfPositionM, ItrfVelocityMS,
187    Wgs84Geodetic,
188};
189pub use frame_catalog::{
190    catalog, catalog_entry, propagate_position, transform, transform_from_epoch, FrameCatalogError,
191    HelmertParameters, HelmertRates, HelmertTransform, TerrestrialFrame, TerrestrialPositionM,
192    TerrestrialState, TerrestrialVelocityMPerYear, TERRESTRIAL_FRAME_CATALOG,
193};
194pub use fusion::{
195    loose_coupling_correction, smooth_fusion_rts, ukf_correct_closed_loop,
196    validate_time_sync_gnss_order, validate_time_sync_imu_order, F64Bits, FusionFilterKind,
197    FusionRtsEpoch, FusionRtsHistory, FusionRtsHistoryBuilder, FusionStateCodecError, FusionUpdate,
198    GnssFixMeasurement, IggIiiMeasurementReweighting, InertialFilter, InertialFilterConfig,
199    LooseCouplingConfig, SerializableErrorStateLayout, SerializableFusionSnapshot,
200    SerializableFusionState, SerializableImuSample, SerializableImuSampleKind,
201    SerializableInsFilterState, SerializableLooseMeasurement, SerializableNavState,
202    SerializableRateEndpoint, SerializableSatelliteId, SerializableStoredCheckpoint,
203    SerializableStoredGnssMeasurement, SerializableStoredImuSample,
204    SerializableTightCarrierPhaseObservation, SerializableTightFilterState,
205    SerializableTightGnssEpoch, SerializableTightGnssObservation,
206    SerializableTightRangeRateObservation, SerializableTimeSyncHistory,
207    SerializableTimeSyncHistoryConfig, SmoothedFusionEpoch, SmoothedFusionTrajectory,
208    TimeSyncHistoryConfig, TimeSyncHistoryStatus, TimeSyncUpdate, UkfUpdateOptions,
209    UnscentedTransformOptions, YangPredictionAdaptiveFactor, DEFAULT_TIME_SYNC_CHECKPOINT_CAPACITY,
210    DEFAULT_TIME_SYNC_IMU_CAPACITY, FUSION_STATE_CODEC_VERSION,
211};
212pub use geodesic::{geodesic_direct, geodesic_inverse, GeodesicError};
213pub use geofence::{
214    containment, containment_probability, containment_probability_with_options, crossing,
215    crossing_probability, crossing_probability_with_options, distance_to_boundary, CrossingEvent,
216    CrossingKind, Fence, GeofenceError, GeofencePositionEstimate, PositionUncertainty,
217    ProbabilityHysteresis, ProbabilityMethod, ProbabilityOptions, GEOFENCE_BOUNDARY_TOLERANCE_M,
218    PLANAR_FAST_PATH_MAX_RADIUS_M,
219};
220pub use geoid::{
221    egm96_undulations_deg, egm96_undulations_rad, ellipsoidal_height_m, geoid_undulation,
222    geoid_undulations_deg, geoid_undulations_rad, orthometric_height_m, Egm2008GridSpacing,
223    Egm2008RasterWindow, GeoidError, GeoidGrid,
224};
225pub use id::{GnssSatelliteId, GnssSystem, SatelliteIdError};
226pub use inertial::{
227    gauss_markov_bias_decay, gauss_markov_bias_variance_increment, gravity_ecef_mps2,
228    mechanize_ecef, normal_gravity_mps2, rodrigues_delta_dcm, simulate_imu_samples,
229    simulate_imu_samples_from_increments, true_imu_increment_between, AttitudeQuaternion,
230    ConingCorrection, CorrectedImuIncrement, ImuBias, ImuCalibration, ImuErrorModel, ImuGrade,
231    ImuRateRandomWalk, ImuSample, ImuSampleKind, ImuSimulationOptions, ImuSimulationOutput,
232    ImuSimulator, ImuSpec, InertialError, MechanizationConfig, NavState, SimulatedImuSequence,
233    StrapdownMechanizer, DEFAULT_IMU_SIM_SEED, WGS84_NORMAL_GRAVITY_EQUATOR_MPS2,
234    WGS84_NORMAL_GRAVITY_POLE_MPS2, WGS84_SOMIGLIANA_K,
235};
236pub use observables::{
237    emission_media_batch_at_j2000_s, observable_media_corrections, predict_batch_with_media,
238    predict_batch_with_media_parallel, predict_ranges_with_media, predict_with_media,
239    AppliedMediaCorrections, EmissionMediaBatch, EmissionMediaBatchOptions, EmissionMediaStatus,
240    MediaPredictOptions, MediaPredictedObservables, MediaRangePrediction,
241    ObservableIonosphereCorrection, ObservableMediaOptions, ObservableTroposphereCorrection,
242};
243pub use sbas_pl::{
244    sbas_protection_levels, AirborneModel, DegradationParams, ProtectionGeometry, ProtectionRow,
245    SbasErrorModel, SbasKMultipliers, SbasPlError, SbasProtection, SbasSisError,
246};
247pub use sidereal::{
248    orbit_repeat_lag, periodicity_strength, periodicity_strength_with_sample_interval,
249    repeat_period, sidereal_filter, solar_day_period, SiderealFilterError, SiderealFilterOptions,
250    SiderealFilterOutput, SiderealTemplateMethod, SIDEREAL_DAY_NANOS, SIDEREAL_DAY_SECONDS,
251};