django-vue3-admin-web/node_modules/astronomia/lib/saturnring.cjs

'use strict';

Object.defineProperty(exports, '__esModule', { value: true });

var base = require('./base.cjs');
var coord = require('./coord.cjs');
var nutation = require('./nutation.cjs');
var planetposition = require('./planetposition.cjs');

/**
 * @copyright 2013 Sonia Keys
 * @copyright 2016 commenthol
 * @license MIT
 * @module saturnring
 */

/**
 * Ring computes quantities of the ring of Saturn.
 *
 *  B  Saturnicentric latitude of the Earth referred to the plane of the ring.
 *  Bʹ  Saturnicentric latitude of the Sun referred to the plane of the ring.
 *  ΔU  Difference between Saturnicentric longitudes of the Sun and the Earth.
 *  P  Geometric position angle of the northern semiminor axis of the ring.
 *  aEdge  Major axis of the out edge of the outer ring.
 *  bEdge  Minor axis of the out edge of the outer ring.
 *
 * All results in radians.
 */
function ring (jde, earth, saturn) { // (jde float64, earth, saturn *pp.V87Planet)  (B, Bʹ, ΔU, P, aEdge, bEdge float64)
  const [f1, f2] = cl(jde, earth, saturn);
  const [ΔU, B] = f1();
  const [Bʹ, P, aEdge, bEdge] = f2();
  return [B, Bʹ, ΔU, P, aEdge, bEdge]
}

/**
 * UB computes quantities required by illum.Saturn().
 *
 * Same as ΔU and B returned by Ring().  Results in radians.
 */
function ub (jde, earth, saturn) { // (jde float64, earth, saturn *pp.V87Planet)  (ΔU, B float64)
  const [f1, f2] = cl(jde, earth, saturn); // eslint-disable-line no-unused-vars
  return f1()
}

/**
 * cl splits the work into two closures.
 */
function cl (jde, earth, saturn) { // (jde float64, earth, saturn *pp.V87Planet)  (f1 func() (ΔU, B float64),
  // f2 func() (Bʹ, P, aEdge, bEdge float64))
  const p = Math.PI / 180;
  let i, Ω;
  let l0, b0, R;
  let Δ = 9.0;
  let λ, β;
  let si, ci, sβ, cβ, sB;
  let sbʹ, cbʹ, slʹΩ, clʹΩ;
  const f1 = function () { // (ΔU, B float64)
    // (45.1), p. 318
    const T = base["default"].J2000Century(jde);
    i = base["default"].horner(T, 28.075216 * p, -0.012998 * p, 0.000004 * p);
    Ω = base["default"].horner(T, 169.50847 * p, 1.394681 * p, 0.000412 * p);
    // Step 2.0
    const earthPos = earth.position(jde);
    R = earthPos.range;
    const fk5 = planetposition["default"].toFK5(earthPos.lon, earthPos.lat, jde);
    l0 = fk5.lon;
    b0 = fk5.lat;
    const [sl0, cl0] = base["default"].sincos(l0);
    const sb0 = Math.sin(b0);
    // Steps 3, 4.0
    let l = 0;
    let b = 0;
    let r = 0;
    let x = 0;
    let y = 0;
    let z = 0;

    const f = function () {
      const τ = base["default"].lightTime(Δ);
      const saturnPos = saturn.position(jde - τ);
      r = saturnPos.range;
      const fk5 = planetposition["default"].toFK5(saturnPos.lon, saturnPos.lat, jde);
      l = fk5.lon;
      b = fk5.lat;
      const [sl, cl] = base["default"].sincos(l);
      const [sb, cb] = base["default"].sincos(b);
      x = r * cb * cl - R * cl0;
      y = r * cb * sl - R * sl0;
      z = r * sb - R * sb0;
      Δ = Math.sqrt(x * x + y * y + z * z);
    };
    f();
    f();
    // Step 5.0
    λ = Math.atan2(y, x);
    β = Math.atan(z / Math.hypot(x, y));
    // First part of step 6.0
    si = Math.sin(i);
    ci = Math.cos(i);
    sβ = Math.sin(β);
    cβ = Math.cos(β);
    sB = si * cβ * Math.sin(λ - Ω) - ci * sβ;
    const B = Math.asin(sB); // return value
    // Step 7.0
    const N = 113.6655 * p + 0.8771 * p * T;
    const lʹ = l - 0.01759 * p / r;
    const bʹ = b - 0.000764 * p * Math.cos(l - N) / r;
    // Setup for steps 8, 9.0
    sbʹ = Math.sin(bʹ);
    cbʹ = Math.cos(bʹ);
    slʹΩ = Math.sin(lʹ - Ω);
    clʹΩ = Math.cos(lʹ - Ω);
    // Step 9.0
    const [sλΩ, cλΩ] = base["default"].sincos(λ - Ω);
    const U1 = Math.atan2(si * sbʹ + ci * cbʹ * slʹΩ, cbʹ * clʹΩ);
    const U2 = Math.atan2(si * sβ + ci * cβ * sλΩ, cβ * cλΩ);
    const ΔU = Math.abs(U1 - U2); // return value
    return [ΔU, B]
  };
  const f2 = function () { // (Bʹ, P, aEdge, bEdge) {
    // Remainder of step 6.0
    const aEdge = 375.35 / 3600 * p / Δ; // return value
    const bEdge = aEdge * Math.abs(sB); // return value
    // Step 8.0
    const sBʹ = si * cbʹ * slʹΩ - ci * sbʹ;
    const Bʹ = Math.asin(sBʹ); // return value
    // Step 10.0
    const [Δψ, Δε] = nutation["default"].nutation(jde);
    const ε = nutation["default"].meanObliquity(jde) + Δε;
    // Step 11.0
    let λ0 = Ω - Math.PI / 2;
    const β0 = Math.PI / 2 - i;
    // Step 12.0
    const [sl0λ, cl0λ] = base["default"].sincos(l0 - λ);
    λ += 0.005693 * p * cl0λ / cβ;
    β += 0.005693 * p * sl0λ * sβ;
    // Step 13.0
    λ0 += Δψ;
    λ += Δψ;
    // Step 14.0
    let eq = new coord["default"].Ecliptic(λ0, β0).toEquatorial(ε);
    const [α0, δ0] = [eq.ra, eq.dec];
    eq = new coord["default"].Ecliptic(λ, β).toEquatorial(ε);
    const [α, δ] = [eq.ra, eq.dec];
    // Step 15.0
    const [sδ0, cδ0] = base["default"].sincos(δ0);
    const [sδ, cδ] = base["default"].sincos(δ);
    const [sα0α, cα0α] = base["default"].sincos(α0 - α);
    const P = Math.atan2(cδ0 * sα0α, sδ0 * cδ - cδ0 * sδ * cα0α); // return value
    return [Bʹ, P, aEdge, bEdge]
  };
  return [f1, f2]
}

var saturnring = {
  ring,
  ub
};

exports["default"] = saturnring;
exports.ring = ring;
exports.ub = ub;