-
Notifications
You must be signed in to change notification settings - Fork 28
/
helpers.go
109 lines (88 loc) · 2.76 KB
/
helpers.go
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
package satellite
import (
"log"
"math"
"strconv"
"strings"
)
// Constants
const TWOPI float64 = math.Pi * 2.0
const DEG2RAD float64 = math.Pi / 180.0
const RAD2DEG float64 = 180.0 / math.Pi
const XPDOTP float64 = 1440.0 / (2.0 * math.Pi)
// Holds latitude and Longitude in either degrees or radians
type LatLong struct {
Latitude, Longitude float64
}
// Holds X, Y, Z position
type Vector3 struct {
X, Y, Z float64
}
// Holds an azimuth, elevation and range
type LookAngles struct {
Az, El, Rg float64
}
// Parses a two line element dataset into a Satellite struct
func ParseTLE(line1, line2 string, gravConst Gravity) (sat Satellite) {
sat.Line1 = line1
sat.Line2 = line2
sat.Error = 0
sat.whichconst = getGravConst(gravConst)
// LINE 1 BEGIN
sat.satnum = parseInt(strings.TrimSpace(line1[2:7]))
sat.epochyr = parseInt(line1[18:20])
sat.epochdays = parseFloat(line1[20:32])
// These three can be negative / positive
sat.ndot = parseFloat(strings.Replace(line1[33:43], " ", "", 2))
sat.nddot = parseFloat(strings.Replace(line1[44:45]+"."+line1[45:50]+"e"+line1[50:52], " ", "", 2))
sat.bstar = parseFloat(strings.Replace(line1[53:54]+"."+line1[54:59]+"e"+line1[59:61], " ", "", 2))
// LINE 1 END
// LINE 2 BEGIN
sat.inclo = parseFloat(strings.Replace(line2[8:16], " ", "", 2))
sat.nodeo = parseFloat(strings.Replace(line2[17:25], " ", "", 2))
sat.ecco = parseFloat("." + line2[26:33])
sat.argpo = parseFloat(strings.Replace(line2[34:42], " ", "", 2))
sat.mo = parseFloat(strings.Replace(line2[43:51], " ", "", 2))
sat.no = parseFloat(strings.Replace(line2[52:63], " ", "", 2))
// LINE 2 END
return
}
// Converts a two line element data set into a Satellite struct and runs sgp4init
func TLEToSat(line1, line2 string, gravConst Gravity) Satellite {
//sat := Satellite{Line1: line1, Line2: line2}
sat := ParseTLE(line1, line2, gravConst)
opsmode := "i"
sat.no = sat.no / XPDOTP
sat.ndot = sat.ndot / (XPDOTP * 1440.0)
sat.nddot = sat.nddot / (XPDOTP * 1440.0 * 1440)
sat.inclo = sat.inclo * DEG2RAD
sat.nodeo = sat.nodeo * DEG2RAD
sat.argpo = sat.argpo * DEG2RAD
sat.mo = sat.mo * DEG2RAD
var year int64 = 0
if sat.epochyr < 57 {
year = sat.epochyr + 2000
} else {
year = sat.epochyr + 1900
}
mon, day, hr, min, sec := days2mdhms(year, sat.epochdays)
sat.jdsatepoch = JDay(int(year), int(mon), int(day), int(hr), int(min), int(sec))
sgp4init(&opsmode, sat.jdsatepoch-2433281.5, &sat)
return sat
}
// Parses a string into a float64 value.
func parseFloat(strIn string) (ret float64) {
ret, err := strconv.ParseFloat(strIn, 64)
if err != nil {
log.Fatal(err)
}
return ret
}
// Parses a string into a int64 value.
func parseInt(strIn string) (ret int64) {
ret, err := strconv.ParseInt(strIn, 10, 0)
if err != nil {
log.Fatal(err)
}
return ret
}