forked from nasa/openmct
-
Notifications
You must be signed in to change notification settings - Fork 0
Expand file tree
/
Copy pathUDLTelemetryProvider.js
More file actions
136 lines (118 loc) · 4.72 KB
/
Copy pathUDLTelemetryProvider.js
File metadata and controls
136 lines (118 loc) · 4.72 KB
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
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
/*****************************************************************************
* Open MCT, Copyright (c) 2014-2024, United States Government
* as represented by the Administrator of the National Aeronautics and Space
* Administration. All rights reserved.
*
* Open MCT is licensed under the Apache License, Version 2.0 (the
* "License"); you may not use this file except in compliance with the License.
* You may obtain a copy of the License at
* http://www.apache.org/licenses/LICENSE-2.0.
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS, WITHOUT
* WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied. See the
* License for the specific language governing permissions and limitations
* under the License.
*
* Open MCT includes source code licensed under additional open source
* licenses. See the Open Source Licenses file (LICENSES.md) included with
* this source code distribution or the Licensing information page available
* at runtime from the About dialog for additional information.
*****************************************************************************/
import { EARTH_RADIUS_KM, MU_EARTH, SATELLITES } from './satellites.js';
const EPHEMERIS_PERIOD_MS = 1000;
const CONJUNCTION_PERIOD_MS = 5000;
const MAX_REQUEST_DATUMS = 50000;
const SECONDARY_OBJECTS = [
'COSMOS 2251 DEB',
'FENGYUN 1C DEB',
'SL-16 R/B',
'STARLINK-30452',
'IRIDIUM 33 DEB'
];
function ephemerisDatum(satellite, timestamp) {
const radiusKm = EARTH_RADIUS_KM + satellite.altitudeKm;
const periodSeconds = 2 * Math.PI * Math.sqrt(Math.pow(radiusKm, 3) / MU_EARTH);
const meanMotion = (2 * Math.PI) / periodSeconds;
const theta = meanMotion * (timestamp / 1000) + (satellite.phaseDeg * Math.PI) / 180;
const inclination = (satellite.inclinationDeg * Math.PI) / 180;
const latitude = (Math.asin(Math.sin(inclination) * Math.sin(theta)) * 180) / Math.PI;
const earthRotationDeg = ((timestamp / 1000) * 360) / 86164;
const longitude =
(((((Math.atan2(Math.cos(inclination) * Math.sin(theta), Math.cos(theta)) * 180) / Math.PI +
satellite.raanDeg -
earthRotationDeg) %
360) +
540) %
360) -
180;
return {
id: satellite.key,
utc: timestamp,
altitude: satellite.altitudeKm + Math.sin(theta * 3) * 2,
latitude,
longitude,
velocity: Math.sqrt(MU_EARTH / radiusKm)
};
}
function conjunctionDatum(timestamp) {
const slot = Math.floor(timestamp / CONJUNCTION_PERIOD_MS);
const wave = Math.abs(Math.sin(slot / 7));
const pc = wave > 0.92 ? 0.0002 + wave / 2000 : wave / 50000;
return {
id: 'conjunctions',
utc: timestamp,
pc: Number(pc.toPrecision(3)),
missDistance: Number((0.4 + (1 - wave) * 24).toFixed(2)),
secondary: SECONDARY_OBJECTS[slot % SECONDARY_OBJECTS.length]
};
}
export default class UDLTelemetryProvider {
supportsRequest(domainObject) {
return this.#isUDLTelemetry(domainObject);
}
supportsSubscribe(domainObject) {
return this.#isUDLTelemetry(domainObject);
}
request(domainObject, options) {
const period =
domainObject.type === 'udl.conjunctions' ? CONJUNCTION_PERIOD_MS : EPHEMERIS_PERIOD_MS;
const size = Math.min(options.size ?? MAX_REQUEST_DATUMS, MAX_REQUEST_DATUMS);
const start = Math.floor(options.start / period) * period;
const requestedCount = Math.floor((options.end - start) / period) + 1;
const count = Math.min(requestedCount, size);
const data = [];
if (options.strategy === 'latest') {
const alignedEnd = Math.floor(options.end / period) * period;
for (let i = count - 1; i >= 0; i--) {
data.push(this.#datumFor(domainObject, alignedEnd - i * period));
}
} else {
const step = count > 1 ? (options.end - start) / (count - 1) : period;
for (let i = 0; i < count; i++) {
data.push(this.#datumFor(domainObject, start + Math.round(i * step)));
}
}
return Promise.resolve(data);
}
subscribe(domainObject, callback) {
const period =
domainObject.type === 'udl.conjunctions' ? CONJUNCTION_PERIOD_MS : EPHEMERIS_PERIOD_MS;
const interval = setInterval(() => {
callback(this.#datumFor(domainObject, Date.now()));
}, period);
return function unsubscribe() {
clearInterval(interval);
};
}
#datumFor(domainObject, timestamp) {
if (domainObject.type === 'udl.conjunctions') {
return conjunctionDatum(timestamp);
}
const satellite = SATELLITES.find((candidate) => candidate.key === domainObject.identifier.key);
return ephemerisDatum(satellite, timestamp);
}
#isUDLTelemetry(domainObject) {
return domainObject.type === 'udl.ephemeris' || domainObject.type === 'udl.conjunctions';
}
}