mirror of
https://github.com/rt-bishop/Look4Sat.git
synced 2026-10-02 03:15:37 +00:00
Minor refactoring and classes move
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commit
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16 files changed
+158
-173
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@@ -32,14 +32,14 @@ class DefaultSatelliteRepo(
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}
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override suspend fun importDataFromFile(stream: InputStream) = withContext(ioDispatcher) {
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val entries = Satellite.importTLE(stream).map { tle -> SatEntry(tle) }
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localSource.updateEntries(entries)
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val importedEntries = Satellite.importElements(stream).map { tle -> SatEntry(tle) }
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localSource.updateEntries(importedEntries)
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}
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override suspend fun importDataFromWeb(sources: List<String>) {
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coroutineScope {
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launch(ioDispatcher) {
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val entries = mutableListOf<SatEntry>()
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val importedEntries = mutableListOf<SatEntry>()
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val streams = mutableListOf<InputStream>()
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sources.forEach { source ->
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remoteSource.fetchFileStream(source)?.let { stream ->
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@@ -52,10 +52,10 @@ class DefaultSatelliteRepo(
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}
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}
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streams.forEach { stream ->
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val importedEntries = Satellite.importTLE(stream).map { tle -> SatEntry(tle) }
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entries.addAll(importedEntries)
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val entries = Satellite.importElements(stream).map { tle -> SatEntry(tle) }
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importedEntries.addAll(entries)
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}
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localSource.updateEntries(entries)
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localSource.updateEntries(importedEntries)
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}
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launch(ioDispatcher) {
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val transmitters = remoteSource.fetchTransmitters().filter { it.isAlive }
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@@ -19,7 +19,7 @@ package com.rtbishop.look4sat.domain.predict4kotlin
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import java.util.*
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class PassPredictor(private val satellite: Satellite, private val qth: GroundPos) {
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class PassPredictor(private val satellite: Satellite, private val gsp: StationPosition) {
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private val oneQuarterOrbitMin = (24.0 * 60.0 / satellite.tle.meanmo / 4.0).toInt()
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private val speedOfLight = 2.99792458E8
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@@ -35,7 +35,7 @@ class PassPredictor(private val satellite: Satellite, private val qth: GroundPos
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}
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fun getSatPos(date: Date): SatPos {
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return satellite.getPosition(qth, date)
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return satellite.getPosition(gsp, date)
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}
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fun getPositions(refDate: Date, stepSec: Int, minBefore: Int, orbits: Double): List<SatPos> {
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@@ -58,7 +58,7 @@ class PassPredictor(private val satellite: Satellite, private val qth: GroundPos
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var shouldWindBack = windBack
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var lastAosDate: Date
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var count = 0
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if (satellite.willBeSeen(qth)) {
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if (satellite.willBeSeen(gsp)) {
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if (satellite.tle.isDeepspace) {
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passes.add(nextDeepSpacePass(refDate))
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} else {
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@@ -17,4 +17,4 @@
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*/
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package com.rtbishop.look4sat.domain.predict4kotlin
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data class Position(val lat: Double, val lon: Double)
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data class Position(val latitude: Double, val longitude: Double)
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@@ -0,0 +1,68 @@
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/*
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* Look4Sat. Amateur radio satellite tracker and pass predictor.
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* Copyright (C) 2019-2021 Arty Bishop (bishop.arty@gmail.com)
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*
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* This program is free software: you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation, either version 3 of the License, or
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* (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with this program. If not, see <https://www.gnu.org/licenses/>.
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*/
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package com.rtbishop.look4sat.domain.predict4kotlin
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import kotlin.math.round
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class QthConverter {
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fun qthToPosition(qthString: String): Position? {
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val trimmedQth = qthString.take(6)
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if (!isValidQTH(trimmedQth)) return null
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val lonFirst = (trimmedQth[0].toUpperCase().toInt() - 65) * 20
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val latFirst = (trimmedQth[1].toUpperCase().toInt() - 65) * 10
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val lonSecond = trimmedQth[2].toString().toInt() * 2
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val latSecond = trimmedQth[3].toString().toInt()
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val lonThird = (((trimmedQth[4].toLowerCase().toInt() - 97) / 12.0) + (1.0 / 24.0)) - 180
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val latThird = (((trimmedQth[5].toLowerCase().toInt() - 97) / 24.0) + (1.0 / 48.0)) - 90
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val longitude = (lonFirst + lonSecond + lonThird).roundToDecimals(4)
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val latitude = (latFirst + latSecond + latThird).roundToDecimals(4)
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return Position(latitude, longitude)
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}
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fun positionToQTH(lat: Double, lon: Double): String? {
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if (!isValidPosition(lat, lon)) return null
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val tempLon = if (lon > 180.0) lon - 360 else lon
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val upper = "ABCDEFGHIJKLMNOPQRSTUVWX"
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val lower = "abcdefghijklmnopqrstuvwx"
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val longitude = tempLon + 180
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val latitude = lat + 90
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val lonFirst = upper[(longitude / 20).toInt()]
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val latFirst = upper[(latitude / 10).toInt()]
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val lonSecond = ((longitude / 2) % 10).toInt().toString()
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val latSecond = (latitude % 10).toInt().toString()
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val lonThird = lower[((longitude % 2) * 12).toInt()]
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val latThird = lower[((latitude % 1) * 24).toInt()]
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return "$lonFirst$latFirst$lonSecond$latSecond$lonThird$latThird"
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}
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private fun isValidQTH(qthString: String): Boolean {
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val qthPattern = "[a-xA-X][a-xA-X][0-9][0-9][a-xA-X][a-xA-X]".toRegex()
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return qthString.matches(qthPattern)
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}
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private fun isValidPosition(lat: Double, lon: Double): Boolean {
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return (lat > -90.0 && lat < 90.0) && (lon > -180.0 && lon < 360.0)
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}
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private fun Double.roundToDecimals(decimals: Int): Double {
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var multiplier = 1.0
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repeat(decimals) { multiplier *= 10 }
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return round(this * multiplier) / multiplier
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}
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}
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@@ -22,39 +22,28 @@ import kotlin.math.*
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class SatPos {
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private val earthRadiusKm = 6.378137E3
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private val r0 = 6378.16
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private val earthRadiusKm = 6378.16
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// Radians
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var azimuth = 0.0
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var elevation = 0.0
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var latitude = 0.0
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var longitude = 0.0
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var time = Date()
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var altitude = 0.0
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var range = 0.0
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var rangeRate = 0.0
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var phase = 0.0
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var altitude = 0.0
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var theta = 0.0
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var eclipseDepth = 0.0
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var eclipsed = false
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var aboveHorizon = false
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fun getDate(): Date {
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return Date(time.time)
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}
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var time = Date()
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fun getRangeCircleRadiusKm(): Double {
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return 0.5 * (12756.33 * acos(earthRadiusKm / (earthRadiusKm + altitude)))
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return earthRadiusKm * acos(earthRadiusKm / (earthRadiusKm + altitude))
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}
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fun getRangeCircle(incrementDegrees: Double = 1.0): List<Position> {
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val positions = mutableListOf<Position>()
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val radiusKm = this.getRangeCircleRadiusKm()
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val lat = this.latitude
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val lon = this.longitude
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val beta = radiusKm / r0
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val beta = getRangeCircleRadiusKm() / earthRadiusKm
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var tempAzimuth = 0
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while (tempAzimuth < 360) {
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val azimuth = tempAzimuth / 360.0 * 2.0 * Math.PI
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@@ -76,22 +65,8 @@ class SatPos {
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}
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while (rangelon < 0.0) rangelon += Math.PI * 2.0
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while (rangelon > Math.PI * 2.0) rangelon -= Math.PI * 2.0
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rangelat = (rangelat / (2.0 * Math.PI)) * 360.0
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rangelon = (rangelon / (2.0 * Math.PI)) * 360.0
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// if (rangelong < 180.0) {
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// rangelong = -rangelong;
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// }
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// else if (rangelong > 180.0) {
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// rangelong = 360.0 - rangelong;
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// }
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//
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// if (rangelat < 90.0) {
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// rangelat = -rangelat;
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// }
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// else if (rangelat > 90.0) {
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// rangelat = 180.0 - rangelat;
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// }
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rangelat = Math.toDegrees(rangelat)
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rangelon = Math.toDegrees(rangelon)
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positions.add(Position(rangelat, rangelon))
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tempAzimuth += incrementDegrees.toInt()
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}
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@@ -42,21 +42,21 @@ abstract class Satellite(val tle: TLE) {
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var s4 = 0.0
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val xke = 7.43669161E-2
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fun willBeSeen(pos: GroundPos): Boolean {
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fun willBeSeen(pos: StationPosition): Boolean {
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return if (tle.meanmo < 1e-8) false else {
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var lin = tle.incl
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if (lin >= 90.0) lin = 180.0 - lin
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val sma = 331.25 * exp(ln(1440.0 / tle.meanmo) * (2.0 / 3.0))
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val apogee = sma * (1.0 + tle.eccn) - earthRadius
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acos(earthRadius / (apogee + earthRadius)) + lin * deg2Rad > abs(pos.lat * deg2Rad)
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acos(earthRadius / (apogee + earthRadius)) + lin * deg2Rad > abs(pos.latitude * deg2Rad)
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}
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}
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fun getPredictor(pos: GroundPos): PassPredictor {
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fun getPredictor(pos: StationPosition): PassPredictor {
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return PassPredictor(this, pos)
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}
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fun getPosition(pos: GroundPos, time: Date): SatPos {
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fun getPosition(pos: StationPosition, time: Date): SatPos {
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val satPos = SatPos()
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// Date/time at which the position and velocity were calculated
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val julUTC = calcCurrentDaynum(time) + 2444238.5
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@@ -121,7 +121,7 @@ abstract class Satellite(val tle: TLE) {
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julianUTC: Double,
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positionVector: Vector4,
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velocityVector: Vector4,
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gsPos: GroundPos,
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gsPos: StationPosition,
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squintVector: Vector4,
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satPos: SatPos
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) {
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@@ -144,8 +144,8 @@ abstract class Satellite(val tle: TLE) {
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velocityVector.z - obsVel.z
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)
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magnitude(range)
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val sinLat = sin(deg2Rad * gsPos.lat)
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val cosLat = cos(deg2Rad * gsPos.lat)
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val sinLat = sin(deg2Rad * gsPos.latitude)
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val cosLat = cos(deg2Rad * gsPos.latitude)
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val sinTheta = sin(gsPosTheta.get())
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val cosTheta = cos(gsPosTheta.get())
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val topS = sinLat * cosTheta * range.x + sinLat * sinTheta * range.y - cosLat * range.z
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@@ -163,20 +163,20 @@ abstract class Satellite(val tle: TLE) {
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// Returns the ECI position and velocity of the observer
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private fun calculateUserPosVel(
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time: Double,
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gsPos: GroundPos,
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gsPos: StationPosition,
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gsPosTheta: AtomicReference<Double>,
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obsPos: Vector4,
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obsVel: Vector4
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) {
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val mFactor = 7.292115E-5
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gsPosTheta.set(mod2PI(thetaGJD(time) + deg2Rad * gsPos.lon))
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gsPosTheta.set(mod2PI(thetaGJD(time) + deg2Rad * gsPos.longitude))
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val c =
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invert(sqrt(1.0 + flatFactor * (flatFactor - 2) * sqr(sin(deg2Rad * gsPos.lat))))
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invert(sqrt(1.0 + flatFactor * (flatFactor - 2) * sqr(sin(deg2Rad * gsPos.latitude))))
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val sq = sqr(1.0 - flatFactor) * c
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val achcp = (earthRadius * c + gsPos.alt / 1000.0) * cos(deg2Rad * gsPos.lat)
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val achcp = (earthRadius * c + gsPos.altitude / 1000.0) * cos(deg2Rad * gsPos.latitude)
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obsPos.setXYZ(
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achcp * cos(gsPosTheta.get()), achcp * sin(gsPosTheta.get()),
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(earthRadius * sq + gsPos.alt / 1000.0) * sin(deg2Rad * gsPos.lat)
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(earthRadius * sq + gsPos.altitude / 1000.0) * sin(deg2Rad * gsPos.latitude)
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)
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obsVel.setXYZ(-mFactor * obsPos.y, mFactor * obsPos.x, 0.0)
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magnitude(obsPos)
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@@ -357,9 +357,9 @@ abstract class Satellite(val tle: TLE) {
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}
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}
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fun importTLE(tleStream: InputStream): List<TLE> {
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val importedTles = mutableListOf<TLE>()
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fun importElements(tleStream: InputStream): List<TLE> {
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val currentTLE = arrayOf(String(), String(), String())
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val importedTles = mutableListOf<TLE>()
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var line = 0
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tleStream.bufferedReader().forEachLine {
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if (line != 2) {
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@@ -367,26 +367,31 @@ abstract class Satellite(val tle: TLE) {
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line++
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} else {
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currentTLE[line] = it
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importedTles.add(parseTLE(currentTLE))
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parseElement(currentTLE)?.let { tle -> importedTles.add(tle) }
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line = 0
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}
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}
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return importedTles
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}
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private fun parseTLE(tle: Array<String>): TLE {
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val name: String = tle[0].trim()
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val epoch: Double = tle[1].substring(18, 32).toDouble()
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val meanmo: Double = tle[2].substring(52, 63).toDouble()
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val eccn: Double = 1.0e-07 * tle[2].substring(26, 33).toDouble()
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val incl: Double = tle[2].substring(8, 16).toDouble()
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val raan: Double = tle[2].substring(17, 25).toDouble()
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val argper: Double = tle[2].substring(34, 42).toDouble()
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val meanan: Double = tle[2].substring(43, 51).toDouble()
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val catnum: Int = tle[1].substring(2, 7).trim().toInt()
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val bstar: Double = 1.0e-5 * tle[1].substring(53, 59).toDouble() /
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10.0.pow(tle[1].substring(60, 61).toDouble())
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return TLE(name, epoch, meanmo, eccn, incl, raan, argper, meanan, catnum, bstar)
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private fun parseElement(tle: Array<String>): TLE? {
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if (tle.size != 3) return null
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try {
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val name: String = tle[0].trim()
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val epoch: Double = tle[1].substring(18, 32).toDouble()
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val meanmo: Double = tle[2].substring(52, 63).toDouble()
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val eccn: Double = 1.0e-07 * tle[2].substring(26, 33).toDouble()
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val incl: Double = tle[2].substring(8, 16).toDouble()
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val raan: Double = tle[2].substring(17, 25).toDouble()
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val argper: Double = tle[2].substring(34, 42).toDouble()
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val meanan: Double = tle[2].substring(43, 51).toDouble()
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val catnum: Int = tle[1].substring(2, 7).trim().toInt()
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val bstar: Double = 1.0e-5 * tle[1].substring(53, 59).toDouble() /
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10.0.pow(tle[1].substring(60, 61).toDouble())
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return TLE(name, epoch, meanmo, eccn, incl, raan, argper, meanan, catnum, bstar)
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} catch (exception: Exception) {
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return null
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}
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}
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}
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}
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+6
-1
@@ -17,4 +17,9 @@
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*/
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package com.rtbishop.look4sat.domain.predict4kotlin
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data class GroundPos(val lat: Double, val lon: Double, val alt: Double, val name: String = "base")
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data class StationPosition(
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val latitude: Double,
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val longitude: Double,
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val altitude: Double,
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val name: String = "base"
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)
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@@ -0,0 +1,60 @@
|
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/*
|
||||
* Look4Sat. Amateur radio satellite tracker and pass predictor.
|
||||
* Copyright (C) 2019-2021 Arty Bishop (bishop.arty@gmail.com)
|
||||
*
|
||||
* This program is free software: you can redistribute it and/or modify
|
||||
* it under the terms of the GNU General Public License as published by
|
||||
* the Free Software Foundation, either version 3 of the License, or
|
||||
* (at your option) any later version.
|
||||
*
|
||||
* This program is distributed in the hope that it will be useful,
|
||||
* but WITHOUT ANY WARRANTY; without even the implied warranty of
|
||||
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
|
||||
* GNU General Public License for more details.
|
||||
*
|
||||
* You should have received a copy of the GNU General Public License
|
||||
* along with this program. If not, see <https://www.gnu.org/licenses/>.
|
||||
*/
|
||||
package com.rtbishop.look4sat
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import com.rtbishop.look4sat.domain.predict4kotlin.QthConverter
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import org.junit.Test
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||||
class QthConverterTest {
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private val converter = QthConverter()
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@Test
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fun `Given valid QTH returns correct location`() {
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var result = converter.qthToPosition("io91VL39FX")
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assert(result?.latitude == 51.4792 && result.longitude == -0.2083)
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result = converter.qthToPosition("JN58TD")
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assert(result?.latitude == 48.1458 && result.longitude == 11.6250)
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result = converter.qthToPosition("gf15vc")
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assert(result?.latitude == -34.8958 && result.longitude == -56.2083)
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result = converter.qthToPosition("fm18LW")
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assert(result?.latitude == 38.9375 && result.longitude == -77.0417)
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}
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@Test
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fun `Given invalid QTH returns null`() {
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var result = converter.qthToPosition("ZZ00zz")
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assert(result == null)
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result = converter.qthToPosition("JN58tz")
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assert(result == null)
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}
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@Test
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fun `Given valid location returns correct QTH`() {
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assert(converter.positionToQTH(51.4878, -0.2146) == "IO91vl")
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assert(converter.positionToQTH(48.1466, 11.6083) == "JN58td")
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assert(converter.positionToQTH(-34.91, -56.2116) == "GF15vc")
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assert(converter.positionToQTH(38.92, -77.065) == "FM18lw")
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||||
}
|
||||
|
||||
@Test
|
||||
fun `Given invalid location returns null`() {
|
||||
assert(converter.positionToQTH(91.0542, -170.1142) == null)
|
||||
assert(converter.positionToQTH(89.0542, -240.1142) == null)
|
||||
}
|
||||
}
|
||||
Reference in new issue
Block a user