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use crate::historical_sofa::{historical_sofa_for_tai_to_utc, historical_sofa_for_utc_to_tai};
use crate::leap_seconds::get_leap_seconds;
use crate::{
ATTOS_PER_SEC, ATTOS_PER_SEC_I128, ClockDrift, ClockModel, Dt, J2000_JD_TT,
J2000_SEC_PER_CENTURY, LB_DEN, LB_NUM, LG_DEN, LG_NUM, LM_DEN, LM_NUM, MARS_MSD_REF_JD_INT,
MARS_MSD_REF_TOD_SEC, MARS_MSD_REF_TOD_SUBSEC, MARS_REF_TT, MARS_SOL_ATTOS,
MARS_SOL_LENGTH_SEC, Real, SEC_PER_DAYI64, SEC_PER_DAYI128, Scale, TAI_SEC_AT_1972,
TCG_TCB_REF_JD_INT, TCG_TCB_REF_TOD_SEC, TCG_TCB_REF_TOD_SUBSEC, TDB0_ATTOS, TSpan,
TT_TAI_OFFSET_SPAN, floor_f, sin_approx, to_sec_f,
};
impl Dt {
#[inline(always)]
pub const fn to_span(&self) -> TSpan {
TSpan {
sec: self.sec,
attos: self.attos,
}
}
pub const fn from(sec: i64, attos: u64, scale: Scale) -> Dt {
// Create a raw Dt with the input numbers on the requested scale
let raw = Dt::new(sec, attos);
match scale {
Scale::TAI | Scale::Custom | Scale::UT1 => raw,
Scale::TT => raw.sub(TT_TAI_OFFSET_SPAN),
Scale::UTC => raw.add(TSpan::from_sec(get_leap_seconds(&raw, true).offset)),
Scale::UTCSpice => {
let tai = raw.add(TSpan::from_sec(get_leap_seconds(&raw, true).offset));
if sec < TAI_SEC_AT_1972 - 10 {
tai.add(TSpan::from_sec_f(f!(9.0)))
} else {
tai
}
}
Scale::UTCSofa => {
let tai = raw.add(TSpan::from_sec(get_leap_seconds(&raw, true).offset));
if let Some(offset) = historical_sofa_for_utc_to_tai(&raw) {
tai.add(TSpan::from_sec_f(offset))
} else {
tai
}
}
Scale::GPS | Scale::QZSS | Scale::GST => raw.add(TSpan::SEC_19),
Scale::BDT => raw.add(TSpan::SEC_33),
Scale::TDB | Scale::ET => Self::tdb_to_tai(raw),
Scale::TCG => {
let tt = Self::tcg_to_tt(raw);
tt.sub(TT_TAI_OFFSET_SPAN)
}
Scale::TCB => {
let tdb = Self::tcb_to_tdb(raw);
Self::tdb_to_tai(tdb)
}
Scale::LTC => {
let tt = Self::ltc_to_tt(raw);
tt.sub(TT_TAI_OFFSET_SPAN)
}
}
}
/// Returns a bare [`TSpan`] containing the numerical `sec`/`attos` values
/// of this instant **on its own [`Scale`]** (same physical moment).
///
/// This is the recommended way for callers to obtain the representation on
/// a particular scale after construction via [`Self::from`].
pub const fn to(&self, scale: Scale) -> TSpan {
match scale {
Scale::TAI | Scale::Custom | Scale::UT1 => self.to_span(),
Scale::TT => self.add(TT_TAI_OFFSET_SPAN).to_span(),
Scale::UTC => self
.sub(TSpan::from_sec(get_leap_seconds(&self, false).offset))
.to_span(),
Scale::UTCSpice => {
if self.sec < TAI_SEC_AT_1972 {
self.sub(TSpan::from_sec(get_leap_seconds(&self, false).offset))
.sub(TSpan::from_sec_f(f!(9.0)))
.to_span()
} else {
self.sub(TSpan::from_sec(get_leap_seconds(&self, false).offset))
.to_span()
}
}
Scale::UTCSofa => {
if let Some(offset) = historical_sofa_for_tai_to_utc(&self) {
self.sub(TSpan::from_sec(get_leap_seconds(&self, false).offset))
.sub(TSpan::from_sec_f(offset))
.to_span()
} else {
self.sub(TSpan::from_sec(get_leap_seconds(&self, false).offset))
.to_span()
}
}
Scale::GPS | Scale::QZSS | Scale::GST => self.sub(TSpan::SEC_19).to_span(),
Scale::BDT => self.sub(TSpan::SEC_33).to_span(),
Scale::TDB | Scale::ET => Self::tai_to_tdb(*self).to_span(),
Scale::TCG => Self::tai_to_tcg(*self).to_span(),
Scale::TCB => Self::tai_to_tcb(*self).to_span(),
Scale::LTC => {
let tt = self.add(TT_TAI_OFFSET_SPAN);
Self::tt_to_ltc(tt).to_span()
}
}
}
/// Converts this instant to any other [`Scale`] while applying an exact quadratic relativistic
/// or clock-drift correction defined by a [`ClockDrift`] model relative to a reference instant.
#[inline]
pub const fn convert_using_drift(self, reference: Self, drift: ClockDrift) -> Self {
let span = self.to_tai_since(reference);
let correction = drift.time_diff_after(&span);
self.add(correction)
}
/// Performs the inverse conversion of [`Self::convert_using_drift`], recovering the original proper
/// time on the source clock scale.
///
/// A fixed-point iteration (at most 16 steps) is used to solve the implicit equation. For the common
/// case of a pure constant offset the function returns immediately without iteration.
pub const fn convert_back_using_drift(self, reference: Self, drift: ClockDrift) -> Self {
if drift.rate().is_zero() && drift.accel().is_zero() {
return self.sub(*drift.constant());
}
let mut guess = self;
let mut i = 0u32;
while i < 16 {
let span = guess.to_tai_since(reference);
let correction = drift.time_diff_after(&span);
guess = self.sub(correction);
i += 1;
}
guess
}
/// Converts this instant using a self-describing [`ClockModel`].
///
/// This is the recommended high-level API for onboard or custom time scales (Proper, Custom,
/// or any model with a defined base and drift).
#[inline]
pub const fn convert_using_model(self, model: ClockModel) -> Self {
self.convert_using_drift(model.reference, model.drift)
}
/// Performs the inverse conversion of [`Self::convert_using_model`].
#[inline]
pub const fn convert_back_using_model(self, model: ClockModel) -> Self {
self.convert_back_using_drift(model.reference, model.drift)
}
/// Computes the difference TDB − TT (in seconds) using the four dominant
/// periodic terms from the Fairhead & Bretagnon (1990) analytical series,
/// as extracted from the SOFA/ERFA library (`eraDtdb`).
///
/// This is currently the most accurate practical analytical model for the
/// periodic part of TDB−TT. It captures approximately 99.85% of the total
/// power present in the full 787-term Fairhead-Bretagnon series while
/// remaining extremely fast and fully `const fn` compatible.
///
/// The model includes:
/// - Main annual term (Earth's orbital eccentricity)
/// - Semi-annual harmonic
/// - 11.86-year perturbation term (lunar/planetary)
/// - Venus perturbation term
///
/// **Accuracy**: better than ±0.5 µs near J2000.0 for the periodic component
/// (this 4-term model captures the dominant variation), with slow degradation
/// over millennia. For nanosecond-level work over long timescales, numerical
/// integration against a modern solar-system ephemeris (DE440/DE441, INPOP,
/// etc.) remains the definitive method.
///
/// References (all directly from the SOFA/ERFA implementation):
///
/// - Fairhead, L. & Bretagnon, P., "An analytical formula for the time
/// transformation TB-TT", Astron. Astrophys. 229, 240-247 (1990).
///
/// - IAU 2006 Resolution 3 (re-definition of Barycentric Dynamical Time).
///
/// - McCarthy, D. D. & Petit, G. (eds.), IERS Conventions (2003),
/// IERS Technical Note No. 32, BKG (2004).
///
/// - Moyer, T. D., "Transformation from proper time on Earth to coordinate
/// time in solar system barycentric space", Cel. Mech. 23, 33 (1981).
///
/// - Murray, C. A., Vectorial Astrometry, Adam Hilger (1983).
///
/// - Seidelmann, P. K. et al., Explanatory Supplement to the Astronomical
/// Almanac, Chapter 2, University Science Books (1992).
///
/// - Simon, J. L., Bretagnon, P., Chapront, J., Chapront-Touze, M.,
/// Francou, G. & Laskar, J., "Numerical expressions for precession
/// formulae and mean elements for the Moon and planets",
/// Astron. Astrophys. 282, 663-683 (1994).
///
/// - SOFA/ERFA `eraDtdb` implementation (2021 May 11 revision):
/// https://raw.githubusercontent.com/liberfa/erfa/master/src/dtdb.c
const fn tdb_minus_tt(sec: i64, attos: u64) -> TSpan {
let seconds_since_j2000_tt = f!(sec) + f!(attos) / f!(ATTOS_PER_SEC);
let t = seconds_since_j2000_tt / J2000_SEC_PER_CENTURY;
// Mean anomaly of Earth (from Fairhead & Bretagnon 1990 / Simon et al. 1994)
let g =
f!(2.0) * core::f64::consts::PI * (f!(357.52910918) + f!(35999.050290) * t) / f!(360.0);
// Main annual term with first-order eccentricity correction
let sin_g = sin_approx(g + f!(0.01671) * sin_approx(g));
// Semi-annual harmonic
let sin_2g = sin_approx(f!(2.0) * g);
// Lunar monthly term (27.3 days) — amplitude 4.770086 µs
let lunar = sin_approx(f!(52.9690965) * t + f!(0.444401603));
// Venus perturbation — amplitude 4.676740 µs
let venus = sin_approx(f!(606.977675) * t + f!(4.021195093));
let correction = f!(0.001656674564) * sin_g
+ f!(0.000022417471) * sin_2g
+ f!(0.000004770086) * lunar
+ f!(0.000004676740) * venus;
TSpan::from_sec_f(correction)
}
const fn tai_to_tdb(tai: Self) -> Self {
let tt = tai.add(TT_TAI_OFFSET_SPAN);
let span = Self::tdb_minus_tt(tt.sec, tt.attos);
tt.add(span)
}
const fn tdb_to_tai(tdb: Self) -> Self {
let mut tt = tdb;
let mut i = 0u32;
while i < 8 {
tt = tdb.sub(Self::tdb_minus_tt(tt.sec, tt.attos));
i += 1;
}
tt.sub(TT_TAI_OFFSET_SPAN)
}
const fn tai_to_tcg(tai: Self) -> Self {
let tt = tai.add(TT_TAI_OFFSET_SPAN);
Self::tt_to_tcg(tt)
}
const fn tai_to_tcb(tai: Self) -> Self {
let tdb = Self::tai_to_tdb(tai);
Self::tdb_to_tcb(tdb)
}
/// Exact integer helper: elapsed attoseconds since the TCG/TCB reference epoch (1977-01-01.0 TAI),
/// using only the numerical `sec`/`attos` of the supplied `Dt` (scale is ignored).
const fn elapsed_to_attos_since_ref(numerical: Self) -> i128 {
let days_since_j2000 = numerical.sec.div_euclid(SEC_PER_DAYI64);
let tod_sec = numerical.sec.rem_euclid(SEC_PER_DAYI64);
let jd_days = J2000_JD_TT + days_since_j2000;
let days_diff = jd_days - TCG_TCB_REF_JD_INT;
let mut sec_diff =
(days_diff as i128) * SEC_PER_DAYI128 + (tod_sec as i128 - TCG_TCB_REF_TOD_SEC as i128);
let mut attos_diff = (numerical.attos as i128) - (TCG_TCB_REF_TOD_SUBSEC as i128);
if attos_diff < 0 {
attos_diff += ATTOS_PER_SEC_I128;
sec_diff -= 1;
}
sec_diff * ATTOS_PER_SEC_I128 + attos_diff
}
/// Exact fixed-point multiplication: `attos * num / den` (handles negative values safely, no overflow for library time range).
const fn mul_rate(attos: i128, num: i128, den: i128) -> i128 {
if attos == 0 {
return 0;
}
let sign = if attos < 0 { -1i128 } else { 1i128 };
let a = if attos < 0 { -attos } else { attos };
let q = a / den;
let r = a % den;
sign * (q * num + (r * num) / den)
}
#[inline]
const fn mul_lg(attos: i128) -> i128 {
Self::mul_rate(attos, LG_NUM, LG_DEN)
}
#[inline]
const fn mul_lb(attos: i128) -> i128 {
Self::mul_rate(attos, LB_NUM, LB_DEN)
}
#[inline]
const fn mul_lm(attos: i128) -> i128 {
Self::mul_rate(attos, LM_NUM, LM_DEN)
}
const fn tt_to_tcg(tt: Self) -> Self {
let elapsed = Self::elapsed_to_attos_since_ref(tt);
let span_attos = Self::mul_lg(elapsed);
tt.add(TSpan::from_attos(span_attos))
}
const fn tcg_to_tt(tcg: Self) -> Self {
let elapsed_cg = Self::elapsed_to_attos_since_ref(tcg);
let span_attos = Self::mul_rate(elapsed_cg, LG_NUM, LG_DEN + LG_NUM);
tcg.sub(TSpan::from_attos(span_attos))
}
const fn tcb_to_tdb(tcb: Self) -> Self {
let elapsed_cg = Self::elapsed_to_attos_since_ref(tcb);
let span_attos = Self::mul_rate(elapsed_cg, LB_NUM, LB_DEN + LB_NUM);
tcb.sub(TSpan::from_attos(span_attos))
.sub(TSpan::from_attos(TDB0_ATTOS))
}
const fn tdb_to_tcb(tdb: Self) -> Self {
let elapsed = Self::elapsed_to_attos_since_ref(tdb);
let span_attos = Self::mul_lb(elapsed);
tdb.add(TSpan::from_attos(span_attos))
.add(TSpan::from_attos(TDB0_ATTOS))
}
const fn tt_to_ltc(tt: Self) -> Self {
let elapsed = Self::elapsed_to_attos_since_ref(tt);
let span_attos = Self::mul_lm(elapsed);
tt.add(TSpan::from_attos(span_attos))
}
const fn ltc_to_tt(ltc: Self) -> Self {
let elapsed = Self::elapsed_to_attos_since_ref(ltc);
let span_attos = Self::mul_rate(elapsed, LM_NUM, LM_DEN + LM_NUM);
ltc.sub(TSpan::from_attos(span_attos))
}
/// Exact helper: elapsed attoseconds since the Mars MSD reference epoch (JD 2405522.0028779 TT).
const fn elapsed_to_attos_since_mars_ref(numerical_tt: TSpan) -> i128 {
let days_since_j2000 = numerical_tt.sec.div_euclid(SEC_PER_DAYI64);
let tod_sec = numerical_tt.sec.rem_euclid(SEC_PER_DAYI64);
let jd_days = J2000_JD_TT + days_since_j2000;
let days_diff = jd_days - MARS_MSD_REF_JD_INT;
let mut sec_diff = (days_diff as i128) * SEC_PER_DAYI128
+ (tod_sec as i128 - MARS_MSD_REF_TOD_SEC as i128);
let mut attos_diff = (numerical_tt.attos as i128) - (MARS_MSD_REF_TOD_SUBSEC as i128);
if attos_diff < 0 {
attos_diff += ATTOS_PER_SEC_I128;
sec_diff -= 1;
}
sec_diff * ATTOS_PER_SEC_I128 + attos_diff
}
/// Returns the exact Mars Sol Date (MSD) as a tuple of integer sols and the fractional part of a sol.
///
/// The computation follows the canonical NASA GISS / AM2000 formulation and works for any input
/// [`Scale`]. Leap seconds are automatically accounted for when converting from UTC.
pub const fn to_msd_exact(self) -> (i64, u128) {
let tt = self.to(Scale::TT);
let elapsed = Self::elapsed_to_attos_since_mars_ref(tt);
let attos_per_sol = MARS_SOL_ATTOS;
let whole_sols = elapsed.div_euclid(attos_per_sol) as i64;
let frac_attos = elapsed.rem_euclid(attos_per_sol) as u128;
(whole_sols, frac_attos)
}
/// Returns Mars Coordinated Time (MTC) as a [`TSpan`] representing
/// seconds into the current sol (range `[0, one Martian sol)`).
#[inline]
pub const fn to_mtc(self) -> TSpan {
let (_, frac_attos) = self.to_msd_exact();
TSpan::from_attos(frac_attos as i128)
}
/// Creates a `Dt` (in TT) from an exact Mars Sol Date using full library precision.
pub const fn from_msd_exact(whole_sols: i64, frac_attos: u128) -> Self {
let elapsed_attos = (whole_sols as i128) * MARS_SOL_ATTOS + frac_attos as i128;
let tt = MARS_REF_TT.add(TSpan::from_attos(elapsed_attos));
Self::from(tt.sec, tt.attos, Scale::TT)
}
/// Creates a `Dt` (in TT) from a floating-point Mars Sol Date.
/// Non-exact Real.
pub const fn from_msd(msd: Real) -> Self {
let whole = floor_f(msd) as i64;
let frac = msd - f!(whole);
let frac_span = TSpan::from_sec_f(frac * MARS_SOL_LENGTH_SEC);
Self::from_msd_exact(whole, frac_span.to_attos() as u128)
}
/// Returns the Mars Sol Date (MSD) as a floating-point value (matches NASA Mars24 output).
/// Non-exact Real.
#[inline]
pub const fn to_msd(self) -> Real {
let (whole, frac) = self.to_msd_exact();
f!(whole) + to_sec_f(frac) / MARS_SOL_LENGTH_SEC
}
}