Files
astro/basic/local_ephemeris_test.go
T
b612 16c62a97d5 feat: 完善时标与天象几何计算并扩展输出接口
- 新增时标、ΔT 模型、质心时间与 UT1 支持
- 改进日月食、月掩、行星事件及路径边界计算
- 完善恒星三维自行与动态距离传播
- 扩展 SVG、GeoJSON、KML 输出与底层距离换算工具
- 整理中英文手册、示例资源及回归测试
2026-09-23 18:55:12 +08:00

158 lines
6.8 KiB
Go
Raw Blame History

This file contains ambiguous Unicode characters
This file contains Unicode characters that might be confused with other characters. If you think that this is intentional, you can safely ignore this warning. Use the Escape button to reveal them.
package basic
import (
"math"
"testing"
"time"
)
func TestSolarEclipseLocalEphemerisBoundedError(t *testing.T) {
events := []struct {
name string
seed float64
}{
{"2010-01-15", JDCalc(2010, 1, 15)},
{"2014-04-29", JDCalc(2014, 4, 29)},
{"2023-04-20", JDCalc(2023, 4, 20)},
{"2031-05-21", JDCalc(2031, 5, 21)},
{"2309-06-09", JDCalc(2309, 6, 9)},
}
for _, event := range events {
t.Run(event.name, func(t *testing.T) {
center := CalcMoonSHByJDE(event.seed, 0)
ephemeris := newSolarEclipseLocalEphemeris(center)
for offset := -4.5; offset <= 4.5; offset += 0.25 {
jd := center + offset/24
approxSun, approxMoon, ok := ephemeris.equatorialAt(jd)
if !ok {
t.Fatalf("interpolator rejected in-window time %.3fh", offset)
}
exactSun, exactMoon := solarEclipseSunMoonEquatorial(jd)
for name, pair := range map[string][2][3]float64{
"sun": {solarEclipseLLRToXYZ(approxSun[0], approxSun[1], approxSun[2]), solarEclipseLLRToXYZ(exactSun[0], exactSun[1], exactSun[2])},
"moon": {solarEclipseLLRToXYZ(approxMoon[0], approxMoon[1], approxMoon[2]), solarEclipseLLRToXYZ(exactMoon[0], exactMoon[1], exactMoon[2])},
} {
if errorKM := vectorDifferenceKM(pair[0], pair[1]); errorKM > 1 {
t.Fatalf("%s interpolation error at %.3fh = %.6f km", name, offset, errorKM)
}
}
}
if _, _, ok := ephemeris.equatorialAt(center + 6.1/24); ok {
t.Fatal("interpolator should reject times outside its bounded window")
}
})
}
}
func TestOccultationLocalEphemerisBoundedError(t *testing.T) {
star := hr4799OccultationCoordinateForTest()
starTT := occultationTimeToTT(time.Date(2025, 6, 5, 20, 0, 0, 0, time.UTC))
starEphemeris := newStarOccultationLocalEphemeris(starTT, star)
for offset := -4.5; offset <= 4.5; offset += 0.25 {
jd := starTT + offset/24
got, ok := starEphemeris.stateAt(jd)
if !ok {
t.Fatalf("star interpolator rejected in-window time %.3fh", offset)
}
want := starOccultationEphemerisStateAt(jd, star)
if difference := angularSeparationDegrees(got.moonRA, got.moonDec, want.moonRA, want.moonDec); difference > 1e-5 {
t.Fatalf("moon direction interpolation error at %.3fh = %.9f deg", offset, difference)
}
if difference := angularSeparationDegrees(got.starRA, got.starDec, want.starRA, want.starDec); difference > 1e-5 {
t.Fatalf("star direction interpolation error at %.3fh = %.9f deg", offset, difference)
}
}
config, ok := planetOccultationConfigFor(OccultationSaturn)
if !ok {
t.Fatal("Saturn occultation config is unavailable")
}
planetTT := occultationTimeToTT(time.Date(2024, 8, 21, 2, 40, 0, 0, time.UTC))
planetEphemeris := newPlanetOccultationLocalEphemeris(planetTT, config)
for offset := -4.5; offset <= 4.5; offset += 0.25 {
jd := planetTT + offset/24
got, ok := planetEphemeris.stateAt(jd)
if !ok {
t.Fatalf("planet interpolator rejected in-window time %.3fh", offset)
}
want := planetOccultationEphemerisStateAt(jd, config)
if difference := angularSeparationDegrees(got.moonRA, got.moonDec, want.moonRA, want.moonDec); difference > 1e-5 {
t.Fatalf("moon direction interpolation error at %.3fh = %.9f deg", offset, difference)
}
if difference := angularSeparationDegrees(got.planetRA, got.planetDec, want.planetRA, want.planetDec); difference > 1e-5 {
t.Fatalf("planet direction interpolation error at %.3fh = %.9f deg", offset, difference)
}
if math.Abs(got.planetDistanceKM-want.planetDistanceKM) > 100 {
t.Fatalf("planet distance interpolation error at %.3fh = %.6f km", offset, math.Abs(got.planetDistanceKM-want.planetDistanceKM))
}
}
}
func TestOccultationLocalEphemerisFullWindowBoundedError(t *testing.T) {
star := hr4799OccultationCoordinateForTest()
starTT := occultationTimeToTT(time.Date(2025, 6, 5, 20, 0, 0, 0, time.UTC))
starEphemeris := newStarOccultationLocalEphemeris(starTT, star)
config, ok := planetOccultationConfigFor(OccultationSaturn)
if !ok {
t.Fatal("Saturn occultation config is unavailable")
}
planetTT := occultationTimeToTT(time.Date(2024, 8, 21, 2, 40, 0, 0, time.UTC))
planetEphemeris := newPlanetOccultationLocalEphemeris(planetTT, config)
for _, offset := range []float64{-47.5, -40, -24, 24, 40, 47.5} {
starJD := starTT + offset/24
gotStar, starOK := starEphemeris.stateAt(starJD)
wantStar := starOccultationEphemerisStateAt(starJD, star)
if !starOK {
t.Fatalf("star interpolator rejected in-window time %.3fh", offset)
}
if difference := angularSeparationDegrees(gotStar.moonRA, gotStar.moonDec, wantStar.moonRA, wantStar.moonDec); difference > 1e-5 {
t.Fatalf("star-event moon direction error at %.3fh = %.9f deg", offset, difference)
}
if difference := angularSeparationDegrees(gotStar.starRA, gotStar.starDec, wantStar.starRA, wantStar.starDec); difference > 1e-5 {
t.Fatalf("star direction error at %.3fh = %.9f deg", offset, difference)
}
planetJD := planetTT + offset/24
gotPlanet, planetOK := planetEphemeris.stateAt(planetJD)
wantPlanet := planetOccultationEphemerisStateAt(planetJD, config)
if !planetOK {
t.Fatalf("planet interpolator rejected in-window time %.3fh", offset)
}
if difference := angularSeparationDegrees(gotPlanet.moonRA, gotPlanet.moonDec, wantPlanet.moonRA, wantPlanet.moonDec); difference > 1e-5 {
t.Fatalf("planet-event moon direction error at %.3fh = %.9f deg", offset, difference)
}
if difference := angularSeparationDegrees(gotPlanet.planetRA, gotPlanet.planetDec, wantPlanet.planetRA, wantPlanet.planetDec); difference > 1e-5 {
t.Fatalf("planet direction error at %.3fh = %.9f deg", offset, difference)
}
if difference := math.Abs(gotPlanet.planetDistanceKM - wantPlanet.planetDistanceKM); difference > 100 {
t.Fatalf("planet distance error at %.3fh = %.6f km", offset, difference)
}
}
}
func vectorDifferenceKM(a, b [3]float64) float64 {
return math.Sqrt((a[0]-b[0])*(a[0]-b[0]) + (a[1]-b[1])*(a[1]-b[1]) + (a[2]-b[2])*(a[2]-b[2]))
}
// 矢量回读的赤经必须落在 [0,360):atan2 给 (−180,180],而精确分支
// (LoBoToRaDec、starMeanToApparentRaDec)与 rise/set 的矢量回读都在 [0,360),
// 不归一会让同一时刻的密集/精确状态相差 360 度,误导比较与日志。
func TestOccultationPathVectorRaDecKeepsNormalizedRA(t *testing.T) {
for _, want := range []float64{0.5, 90, 189.1975, 270, 359.9} {
vector := occultationPathRaDecVector(want, -5.8, 2.5)
got, dec, distance, ok := occultationPathVectorRaDec(vector)
if !ok {
t.Fatalf("RA %.4f 的回读失败", want)
}
if math.Abs(got-want) > 1e-9 {
t.Fatalf("RA %.4f 回读为 %.4f,want [0,360) 内的同一读数", want, got)
}
if math.Abs(dec+5.8) > 1e-9 || math.Abs(distance-2.5) > 1e-12 {
t.Fatalf("RA %.4f 的赤纬/距离 = %.6f / %.6f,want -5.8 / 2.5", want, dec, distance)
}
}
if _, _, _, ok := occultationPathVectorRaDec(occultationPathVector{}); ok {
t.Fatal("零矢量应判为无效")
}
}