siderust 0.6.0

High-precision astronomy and satellite mechanics in Rust.
Documentation 
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// SPDX-License-Identifier: AGPL-3.0-or-later
// Copyright (C) 2026 Vallés Puig, Ramon

//! Frame-rotation providers for the **Earth orientation chain**.
//!
//! Implements the IAU 2000/2006 CIO-based rotation path from celestial
//! to terrestrial frames:
//!
//! ```text
//! GCRS → CIRS → TIRS → ITRF → ECEF
//! ```
//!
//! Each step is a single rotation:
//!
//! - **GCRS → CIRS**: CIP/CIO matrix (celestial-pole + CIO locator).
//! - **CIRS → TIRS**: Earth Rotation Angle (ERA) as Rz(−θ).
//! - **TIRS → ITRF**: Polar-motion matrix W(t) from EOP (xp, yp).
//! - **ITRF → ECEF**: Identity (ECEF is an alias for ITRF at this level).
//!
//! Cross-frame pairs (e.g. `EclipticMeanJ2000 ↔ ECEF`) are generated by
//! the [`impl_via_icrs_bidirectional`] macro, composing through ICRS.

use super::*;

impl FrameRotationProvider<GCRSFrame, CIRS> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        gcrs_to_cirs_rotation(jd, ctx)
    }
}

impl FrameRotationProvider<CIRS, GCRSFrame> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        inverse_rotation::<CIRS, GCRSFrame, Eph, Eop, Nut>(jd, ctx)
    }
}

impl FrameRotationProvider<CIRS, TIRS> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        cirs_to_tirs_rotation(jd, ctx)
    }
}

impl FrameRotationProvider<TIRS, CIRS> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        inverse_rotation::<TIRS, CIRS, Eph, Eop, Nut>(jd, ctx)
    }
}

impl FrameRotationProvider<TIRS, ITRF> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        tirs_to_itrf_rotation(jd, ctx)
    }
}

impl FrameRotationProvider<ITRF, TIRS> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        inverse_rotation::<ITRF, TIRS, Eph, Eop, Nut>(jd, ctx)
    }
}

impl FrameRotationProvider<ITRF, ECEF> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        _jd: JulianDate,
        _ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        Rotation3::IDENTITY
    }
}

impl FrameRotationProvider<ECEF, ITRF> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        inverse_rotation::<ECEF, ITRF, Eph, Eop, Nut>(jd, ctx)
    }
}

impl FrameRotationProvider<ICRS, CIRS> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        <() as FrameRotationProvider<GCRSFrame, CIRS>>::rotation(jd, ctx)
    }
}

impl FrameRotationProvider<CIRS, ICRS> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        inverse_rotation::<CIRS, ICRS, Eph, Eop, Nut>(jd, ctx)
    }
}

impl FrameRotationProvider<ICRS, TIRS> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        compose_rotation::<ICRS, CIRS, TIRS, Eph, Eop, Nut>(jd, ctx)
    }
}

impl FrameRotationProvider<TIRS, ICRS> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        inverse_rotation::<TIRS, ICRS, Eph, Eop, Nut>(jd, ctx)
    }
}

impl FrameRotationProvider<ICRS, ITRF> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        compose_rotation::<ICRS, TIRS, ITRF, Eph, Eop, Nut>(jd, ctx)
    }
}

impl FrameRotationProvider<ITRF, ICRS> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        inverse_rotation::<ITRF, ICRS, Eph, Eop, Nut>(jd, ctx)
    }
}

impl FrameRotationProvider<ICRS, ECEF> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        <() as FrameRotationProvider<ICRS, ITRF>>::rotation(jd, ctx)
    }
}

impl FrameRotationProvider<ECEF, ICRS> for () {
    #[inline]
    fn rotation<Eph, Eop: EopProvider, Nut>(
        jd: JulianDate,
        ctx: &AstroContext<Eph, Eop, Nut>,
    ) -> Rotation3 {
        inverse_rotation::<ECEF, ICRS, Eph, Eop, Nut>(jd, ctx)
    }
}

impl_via_icrs_bidirectional!(EclipticMeanJ2000, CIRS);
impl_via_icrs_bidirectional!(EquatorialMeanJ2000, CIRS);
impl_via_icrs_bidirectional!(EME2000, CIRS);
impl_via_icrs_bidirectional!(EquatorialMeanOfDate, CIRS);
impl_via_icrs_bidirectional!(EquatorialTrueOfDate, CIRS);
impl_via_icrs_bidirectional!(ICRF, CIRS);
impl_via_icrs_bidirectional!(TEME, CIRS);
impl_via_icrs_bidirectional!(Galactic, CIRS);
impl_via_icrs_bidirectional!(FK4B1950, CIRS);

impl_via_icrs_bidirectional!(GCRSFrame, TIRS);
impl_via_icrs_bidirectional!(EclipticMeanJ2000, TIRS);
impl_via_icrs_bidirectional!(EquatorialMeanJ2000, TIRS);
impl_via_icrs_bidirectional!(EME2000, TIRS);
impl_via_icrs_bidirectional!(EquatorialMeanOfDate, TIRS);
impl_via_icrs_bidirectional!(EquatorialTrueOfDate, TIRS);
impl_via_icrs_bidirectional!(ICRF, TIRS);
impl_via_icrs_bidirectional!(TEME, TIRS);
impl_via_icrs_bidirectional!(Galactic, TIRS);
impl_via_icrs_bidirectional!(FK4B1950, TIRS);

impl_via_icrs_bidirectional!(GCRSFrame, ITRF);
impl_via_icrs_bidirectional!(EclipticMeanJ2000, ITRF);
impl_via_icrs_bidirectional!(EquatorialMeanJ2000, ITRF);
impl_via_icrs_bidirectional!(EME2000, ITRF);
impl_via_icrs_bidirectional!(EquatorialMeanOfDate, ITRF);
impl_via_icrs_bidirectional!(EquatorialTrueOfDate, ITRF);
impl_via_icrs_bidirectional!(ICRF, ITRF);
impl_via_icrs_bidirectional!(TEME, ITRF);
impl_via_icrs_bidirectional!(Galactic, ITRF);
impl_via_icrs_bidirectional!(FK4B1950, ITRF);

impl_via_icrs_bidirectional!(GCRSFrame, ECEF);
impl_via_icrs_bidirectional!(EclipticMeanJ2000, ECEF);
impl_via_icrs_bidirectional!(EquatorialMeanJ2000, ECEF);
impl_via_icrs_bidirectional!(EME2000, ECEF);
impl_via_icrs_bidirectional!(EquatorialMeanOfDate, ECEF);
impl_via_icrs_bidirectional!(EquatorialTrueOfDate, ECEF);
impl_via_icrs_bidirectional!(ICRF, ECEF);
impl_via_icrs_bidirectional!(TEME, ECEF);
impl_via_icrs_bidirectional!(Galactic, ECEF);
impl_via_icrs_bidirectional!(FK4B1950, ECEF);