coordinate frames transformation

This commit is contained in:
nuknal
2024-08-15 14:01:05 +08:00
parent 7c1240f2db
commit c2480a828b
12 changed files with 19640 additions and 16 deletions

266
pkg/calculator/eop.go Normal file
View File

@@ -0,0 +1,266 @@
package calculator
import (
"bufio"
"bytes"
_ "embed"
"fmt"
"io"
"math"
"os"
"strconv"
"strings"
"time"
"github.com/hebl/gofa"
)
const (
ARC_SECONDS_PER_RADIAN = 206264.80624709636
)
// https://www.iers.org/IERS/EN/DataProducts/EarthOrientationData/eop.html
// https://maia.usno.navy.mil/ser7/finals2000A.all
type EOPEntry struct {
Year int
Month int
Day int
MJD float64
Xp float64 // 弧度 rad
Yp float64 // 弧度 rad
Dut1 float64
}
// https://earth-info.nga.mil/#eopp
type EOPP5Line struct {
Ta float64
A, B float64
C, D, P [2]float64
E, F float64
G, H, Q [2]float64
Tb float64
I, J float64
K, L, R [4]float64
}
type EOPTable struct {
URL string
Local2000A string
EOPs map[float64]*EOPEntry
EOPP5Line EOPP5Line
UseEOPP5Line bool
}
var EOP *EOPTable
func NewEOPTable() *EOPTable {
eop := &EOPTable{
URL: "https://maia.usno.navy.mil/ser7/finals2000A.all",
Local2000A: "data/EOP/finals2000A.all",
EOPs: make(map[float64]*EOPEntry),
UseEOPP5Line: false, // 当天使用 EOPP5Line 预测结果无法通过测试
}
return eop
}
func (eop *EOPTable) Load(eopData []byte, eopp5Line []byte) error {
f, err := os.Open(eop.Local2000A)
if err != nil {
return eop.loadEmbed(eopData, eopp5Line)
}
defer f.Close()
data, err := io.ReadAll(f)
if err != nil {
return eop.loadEmbed(eopData, eopp5Line)
}
return eop.loadEmbed(data, eopp5Line)
}
func (eop *EOPTable) loadEmbed(eopData []byte, eopp5Line []byte) error {
reader := bufio.NewReader(bytes.NewReader(eopData))
for {
line, _, err := reader.ReadLine()
if err == io.EOF {
break
}
if err != nil {
return err
}
var e EOPEntry
if err := e.line2EOPEntry(line); err != nil {
break
}
eop.EOPs[e.MJD] = &e
}
eop.EOPP5Line.parse(eopp5Line)
return nil
}
func (eop EOPTable) Get(mjd float64) (*EOPEntry, bool) {
e, ok := eop.EOPs[mjd]
if !ok && eop.UseEOPP5Line {
xp, yp, dut1 := eop.EOPP5Line.Predict(mjd)
e = &EOPEntry{
MJD: mjd,
Xp: xp / ARC_SECONDS_PER_RADIAN,
Yp: yp / ARC_SECONDS_PER_RADIAN,
Dut1: dut1,
}
ok = true
}
return e, ok
}
func (eop EOPTable) GetByUTCTime(utctime time.Time) (*EOPEntry, bool) {
var djm0, mjd float64
gofa.Cal2jd(int(utctime.Year()), int(utctime.Month()), int(utctime.Day()), &djm0, &mjd)
return eop.Get(mjd)
}
// https://maia.usno.navy.mil/ser7/readme.finals2000A
// The format of the finals2000A.data, finals2000A.daily, and finals2000A.all files is:
// Col.# Format Quantity
// ------- ------ -------------------------------------------------------------
// 1-2 I2 year (to get true calendar year, add 1900 for MJD<=51543 or add 2000 for MJD>=51544)
// 3-4 I2 month number
// 5-6 I2 day of month
// 7 X [blank]
// 8-15 F8.2 fractional Modified Julian Date (MJD UTC)
// 16 X [blank]
// 17 A1 IERS (I) or Prediction (P) flag for Bull. A polar motion values
// 18 X [blank]
// 19-27 F9.6 Bull. A PM-x (sec. of arc)
// 28-36 F9.6 error in PM-x (sec. of arc)
// 37 X [blank]
// 38-46 F9.6 Bull. A PM-y (sec. of arc)
// 47-55 F9.6 error in PM-y (sec. of arc)
// 56-57 2X [blanks]
// 58 A1 IERS (I) or Prediction (P) flag for Bull. A UT1-UTC values
// 59-68 F10.7 Bull. A UT1-UTC (sec. of time)
// 69-78 F10.7 error in UT1-UTC (sec. of time)
// 79 X [blank]
// 80-86 F7.4 Bull. A LOD (msec. of time) -- NOT ALWAYS FILLED
// 87-93 F7.4 error in LOD (msec. of time) -- NOT ALWAYS FILLED
// 94-95 2X [blanks]
// 96 A1 IERS (I) or Prediction (P) flag for Bull. A nutation values
// 97 X [blank]
// 98-106 F9.3 Bull. A dX wrt IAU2000A Nutation (msec. of arc), Free Core Nutation NOT Removed
// 107-115 F9.3 error in dX (msec. of arc)
// 116 X [blank]
// 117-125 F9.3 Bull. A dY wrt IAU2000A Nutation (msec. of arc), Free Core Nutation NOT Removed
// 126-134 F9.3 error in dY (msec. of arc)
// 135-144 F10.6 Bull. B PM-x (sec. of arc)
// 145-154 F10.6 Bull. B PM-y (sec. of arc)
// 155-165 F11.7 Bull. B UT1-UTC (sec. of time)
// 166-175 F10.3 Bull. B dX wrt IAU2000A Nutation (msec. of arc)
// 176-185 F10.3 Bull. B dY wrt IAU2000A Nutation (msec. of arc)
func (e *EOPEntry) line2EOPEntry(line []byte) error {
if len(line) < 68 {
return fmt.Errorf("invalid eop line")
}
e.Year, _ = strconv.Atoi(string(line[0:2]))
e.Month, _ = strconv.Atoi(strings.TrimSpace(string(line[2:4])))
e.Day, _ = strconv.Atoi(strings.TrimSpace(string(line[4:6])))
e.MJD, _ = strconv.ParseFloat(string(line[7:15]), 64)
e.Xp, _ = strconv.ParseFloat(strings.TrimSpace(string(line[18:27])), 64)
e.Yp, _ = strconv.ParseFloat(strings.TrimSpace(string(line[37:46])), 64)
e.Xp = e.Xp / ARC_SECONDS_PER_RADIAN
e.Yp = e.Yp / ARC_SECONDS_PER_RADIAN
e.Dut1, _ = strconv.ParseFloat(strings.TrimSpace(string(line[58:68])), 64)
return nil
}
func (e *EOPP5Line) parse(eopp5Line []byte) error {
e.P[0] = 1.0
e.P[1] = 1.0
for i := 0; i < 4; i++ {
e.R[i] = 1.0
}
reader := bufio.NewReader(bytes.NewReader(eopp5Line))
var lines [][]byte
for {
line, _, err := reader.ReadLine()
if err == io.EOF {
break
}
if err != nil {
return err
}
lines = append(lines, line)
}
if len(lines) < 5 {
return fmt.Errorf("invalid eopp5 lines")
}
e.Ta, _ = strconv.ParseFloat(strings.TrimSpace(string(lines[0][0:10])), 64)
e.A, _ = strconv.ParseFloat(strings.TrimSpace(string(lines[0][10:20])), 64)
e.B, _ = strconv.ParseFloat(strings.TrimSpace(string(lines[0][20:30])), 64)
e.C[0], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[0][30:40])), 64)
e.C[1], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[0][40:50])), 64)
e.D[0], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[0][50:60])), 64)
e.D[1], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[0][60:70])), 64)
e.P[0], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[0][70:76])), 64)
e.P[1], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[1][0:6])), 64)
e.E, _ = strconv.ParseFloat(strings.TrimSpace(string(lines[1][6:16])), 64)
e.F, _ = strconv.ParseFloat(strings.TrimSpace(string(lines[1][16:26])), 64)
e.G[0], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[1][26:36])), 64)
e.G[1], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[1][36:46])), 64)
e.H[0], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[1][46:56])), 64)
e.H[1], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[1][56:66])), 64)
e.Q[0], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[1][66:72])), 64)
e.Q[1], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[1][72:78])), 64)
e.Tb, _ = strconv.ParseFloat(strings.TrimSpace(string(lines[2][0:10])), 64)
e.I, _ = strconv.ParseFloat(strings.TrimSpace(string(lines[2][10:20])), 64)
e.J, _ = strconv.ParseFloat(strings.TrimSpace(string(lines[2][20:30])), 64)
e.K[0], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[2][30:40])), 64)
e.K[1], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[2][40:50])), 64)
e.K[2], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[2][50:60])), 64)
e.K[3], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[2][60:70])), 64)
e.L[0], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[3][0:10])), 64)
e.L[1], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[3][10:20])), 64)
e.L[2], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[3][20:30])), 64)
e.L[3], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[3][30:40])), 64)
e.R[0], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[3][40:49])), 64)
e.R[1], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[3][49:58])), 64)
e.R[2], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[3][58:67])), 64)
e.R[3], _ = strconv.ParseFloat(strings.TrimSpace(string(lines[3][67:76])), 64)
return nil
}
// https://earth-info.nga.mil/php/download.php?file=gnss-eopp
func (e *EOPP5Line) Predict(mjd float64) (xp, yp, dut1 float64) {
xp = e.A + e.B*(mjd-e.Ta) +
e.C[0]*math.Sin(2*math.Pi*(mjd-e.Ta)/e.P[0]) + e.D[0]*math.Cos(2*math.Pi*(mjd-e.Ta)/e.P[0]) +
e.C[1]*math.Sin(2*math.Pi*(mjd-e.Ta)/e.P[1]) + e.D[1]*math.Cos(2*math.Pi*(mjd-e.Ta)/e.P[1])
yp = e.E + e.F*(mjd-e.Ta) +
e.G[0]*math.Sin(2*math.Pi*(mjd-e.Ta)/e.Q[0]) + e.H[0]*math.Cos(2*math.Pi*(mjd-e.Ta)/e.Q[0]) +
e.G[1]*math.Sin(2*math.Pi*(mjd-e.Ta)/e.Q[1]) + e.H[1]*math.Cos(2*math.Pi*(mjd-e.Ta)/e.Q[1])
dut1 = e.I + e.J*(mjd-e.Tb) +
e.K[0]*math.Sin(2*math.Pi*(mjd-e.Tb)/e.R[0]) + e.L[0]*math.Cos(2*math.Pi*(mjd-e.Tb)/e.R[0]) +
e.K[1]*math.Sin(2*math.Pi*(mjd-e.Tb)/e.R[1]) + e.L[1]*math.Cos(2*math.Pi*(mjd-e.Tb)/e.R[1]) +
e.K[2]*math.Sin(2*math.Pi*(mjd-e.Tb)/e.R[2]) + e.L[2]*math.Cos(2*math.Pi*(mjd-e.Tb)/e.R[2]) +
e.K[3]*math.Sin(2*math.Pi*(mjd-e.Tb)/e.R[3]) + e.L[3]*math.Cos(2*math.Pi*(mjd-e.Tb)/e.R[3])
return
}