Files
astro/mercury/truncated.go
T
b612 044f2f4381 feat: 引入可切换星历模型并扩展天象观测链路
- 新增半解析、旧模型、自定义与多源堆叠星历实例,提供 Context、Instance、SPK 读取及状态与视位置计算
- 统一太阳、月球和行星实例接口,扩展黄经穿越、留、相位、最近角距、偕日可见、任意高度升落、轨道节点及凌日等天象查询
- 完善日月食、月掩与凌日的月缘剖面、有限盘面接触、站心修正、局地可见性、全球路径和地图输出
- 新增 SVG、GeoJSON、KML 天象输出及凌日、月掩和月缘地形相关缓存与几何求解
- 新增恒星星表导入与查询,支持 CSV、Hipparcos、BSC5、Stellarium 等格式及名称、交叉标识、锥面检索和星等过滤
- 补充 IAU 2006、地球定向、折射消光、大气观测、轨道传播及半解析行星/月球数据支持
- 将默认未来民用时标切换为 TimeScaleLeapHour,更新 2027–2400 农历速查表、中文日期解析和时区边界处理
- 增加事件基线、跨模型回归、几何边界、月缘地形和输出契约测试,完善中英文手册、示例资源、NOTICE 与忽略规则
2026-10-15 23:54:15 +08:00

131 lines
5.4 KiB
Go

package mercury
import (
"time"
"b612.me/astro/basic"
"b612.me/astro/calendar"
)
// N variants keep the same semantics as the non-N APIs; n < 0 means full series.
// ApparentLoN 视黄经(n 变体) / n-parameterised apparent ecliptic longitude.
func (module *Mercury) ApparentLoN(date time.Time, n int) float64 {
jd := calendar.Date2JD(date.UTC())
return basic.MercuryApparentLoNWithInstance(basic.UTC2TT(jd), n, module.inst)
}
// ApparentBoN 视黄纬(n 变体) / n-parameterised apparent ecliptic latitude.
func (module *Mercury) ApparentBoN(date time.Time, n int) float64 {
jd := calendar.Date2JD(date.UTC())
return basic.MercuryApparentBoNWithInstance(basic.UTC2TT(jd), n, module.inst)
}
// ApparentRaN 视赤经(n 变体) / n-parameterised apparent right ascension.
func (module *Mercury) ApparentRaN(date time.Time, n int) float64 {
jd := calendar.Date2JD(date.UTC())
return basic.MercuryApparentRaNWithInstance(basic.UTC2TT(jd), n, module.inst)
}
// ApparentDecN 视赤纬(n 变体) / n-parameterised apparent declination.
func (module *Mercury) ApparentDecN(date time.Time, n int) float64 {
jd := calendar.Date2JD(date.UTC())
return basic.MercuryApparentDecNWithInstance(basic.UTC2TT(jd), n, module.inst)
}
// ApparentRaDecN 视赤经赤纬(n 变体) / n-parameterised apparent right ascension and declination.
func (module *Mercury) ApparentRaDecN(date time.Time, n int) (float64, float64) {
jd := calendar.Date2JD(date.UTC())
return basic.MercuryApparentRaDecNWithInstance(basic.UTC2TT(jd), n, module.inst)
}
// ApparentMagnitudeN 视星等(n 变体) / n-parameterised apparent magnitude.
func (module *Mercury) ApparentMagnitudeN(date time.Time, n int) float64 {
jd := calendar.Date2JD(date.UTC())
return basic.MercuryMagNWithInstance(basic.UTC2TT(jd), n, module.inst)
}
// EarthDistanceN 地球距离(n 变体) / n-parameterised Earth distance.
func (module *Mercury) EarthDistanceN(date time.Time, n int) float64 {
jd := calendar.Date2JD(date.UTC())
return basic.EarthMercuryAwayNWithInstance(basic.UTC2TT(jd), n, module.inst)
}
// SunDistanceN 太阳距离(n 变体) / n-parameterised Sun distance.
func (module *Mercury) SunDistanceN(date time.Time, n int) float64 {
jd := calendar.Date2JD(date.UTC())
return basic.PlanetCoordinateNWithInstance(1, 2, basic.UTC2TT(jd), n, module.inst)
}
// AltitudeN 站心视高度角(n 变体) / n-parameterised topocentric apparent altitude.
func (module *Mercury) AltitudeN(date time.Time, lon, lat float64, n int) float64 {
localJD := basic.Date2JD(date)
_, loc := date.Zone()
timezone := float64(loc) / 3600.0
return basic.MercuryHeightNWithInstance(localJD, lon, lat, timezone, n, module.inst)
}
// ZenithN 天顶距(n 变体) / n-parameterised zenith distance.
func (module *Mercury) ZenithN(date time.Time, lon, lat float64, n int) float64 {
return 90 - module.AltitudeN(date, lon, lat, n)
}
// AzimuthN 站心方位角(n 变体) / n-parameterised topocentric azimuth.
func (module *Mercury) AzimuthN(date time.Time, lon, lat float64, n int) float64 {
localJD := basic.Date2JD(date)
_, loc := date.Zone()
timezone := float64(loc) / 3600.0
return basic.MercuryAzimuthNWithInstance(localJD, lon, lat, timezone, n, module.inst)
}
// HourAngleN 时角(n 变体) / n-parameterised hour angle.
func (module *Mercury) HourAngleN(date time.Time, lon float64, n int) float64 {
localJD := basic.Date2JD(date)
_, loc := date.Zone()
timezone := float64(loc) / 3600.0
return basic.MercuryHourAngleNWithInstance(localJD, lon, timezone, n, module.inst)
}
// CulminationTimeN 中天时间(n 变体) / n-parameterised culmination time.
func (module *Mercury) CulminationTimeN(date time.Time, lon float64, n int) time.Time {
date = time.Date(date.Year(), date.Month(), date.Day(), 0, 0, 0, 0, date.Location())
localJD := basic.Date2JD(date)
_, loc := date.Zone()
timezone := float64(loc) / 3600.0
calcJD := basic.MercuryCulminationTimeNWithInstance(localJD, lon, timezone, n, module.inst) - timezone/24.0
return basic.JD2DateByZone(calcJD, date.Location(), false)
}
// RiseTimeN 升起时间(n 变体) / n-parameterised rise time.
func (module *Mercury) RiseTimeN(date time.Time, lon, lat, height float64, aero bool, n int) (time.Time, error) {
var aeroFloat float64
if aero {
aeroFloat = 1
}
date = time.Date(date.Year(), date.Month(), date.Day(), 0, 0, 0, 0, date.Location())
localJD := basic.Date2JD(date)
_, loc := date.Zone()
timezone := float64(loc) / 3600.0
riseJD, err := basic.MercuryRiseTimeNWithInstance(localJD, lon, lat, timezone, aeroFloat, height, n, module.inst)
return riseSetResult(date, riseJD, err)
}
// DownTimeN 落下时间别名(n 变体) / n-parameterised down-time alias.
func (module *Mercury) DownTimeN(date time.Time, lon, lat, height float64, aero bool, n int) (time.Time, error) {
return module.SetTimeN(date, lon, lat, height, aero, n)
}
// SetTimeN 落下时间(n 变体) / n-parameterised set time.
func (module *Mercury) SetTimeN(date time.Time, lon, lat, height float64, aero bool, n int) (time.Time, error) {
var aeroFloat float64
if aero {
aeroFloat = 1
}
date = time.Date(date.Year(), date.Month(), date.Day(), 0, 0, 0, 0, date.Location())
localJD := basic.Date2JD(date)
_, loc := date.Zone()
timezone := float64(loc) / 3600.0
riseJD, err := basic.MercurySetTimeNWithInstance(localJD, lon, lat, timezone, aeroFloat, height, n, module.inst)
return riseSetResult(date, riseJD, err)
}