OsculatingToSGP4Converter.java
- /* Copyright 2020-2024 Exotrail
- * Licensed to CS GROUP (CS) under one or more
- * contributor license agreements. See the NOTICE file distributed with
- * this work for additional information regarding copyright ownership.
- * CS licenses this file to You 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.
- */
- package org.orekit.propagation.conversion.averaging.converters;
- import org.orekit.annotation.DefaultDataContext;
- import org.orekit.data.DataContext;
- import org.orekit.frames.Frame;
- import org.orekit.orbits.Orbit;
- import org.orekit.propagation.SpacecraftState;
- import org.orekit.propagation.analytical.tle.TLE;
- import org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm;
- import org.orekit.time.UTCScale;
- import org.orekit.propagation.conversion.averaging.SGP4OrbitalState;
- /**
- * Class for osculating-to-averaged conversion according to "SGP4" theory, meant as the set of
- * models associated to Two-Line Elements.
- *
- * @author Romain Serra
- * @see org.orekit.propagation.analytical.tle.TLEPropagator
- * @see SGP4OrbitalState
- * @since 12.1
- */
- public class OsculatingToSGP4Converter
- extends FixedPointOsculatingToAveragedConverter<SGP4OrbitalState> {
- /** First line of arbitrary TLE. Should not impact conversion. */
- private static final String TEMPLATE_LINE_1 = "1 27421U 02021A 02124.48976499 -.00021470 00000-0 -89879-2 0 20";
- /** Second line of arbitrary TLE. Should not impact conversion. */
- private static final String TEMPLATE_LINE_2 = "2 27421 98.7490 199.5121 0001333 133.9522 226.1918 14.26113993 62";
- /** Scale for fixed-point algorithm. */
- private final double scale;
- /** UTC time scale. */
- private final UTCScale utc;
- /** TEME frame. */
- private final Frame teme;
- /**
- * Constructor with default data context.
- */
- @DefaultDataContext
- public OsculatingToSGP4Converter() {
- this(DataContext.getDefault());
- }
- /**
- * Constructor with default parameters for fixed-point algorithm.
- * @param dataContext data context
- */
- public OsculatingToSGP4Converter(final DataContext dataContext) {
- this(DEFAULT_EPSILON, DEFAULT_MAX_ITERATIONS, FixedPointTleGenerationAlgorithm.SCALE_DEFAULT,
- dataContext);
- }
- /**
- * Constructor.
- * @param epsilon convergence threshold
- * @param maxIterations maximum number of iterations
- * @param scale scale
- * @param dataContext data context
- */
- public OsculatingToSGP4Converter(final double epsilon, final int maxIterations,
- final double scale, final DataContext dataContext) {
- super(epsilon, maxIterations);
- this.scale = scale;
- this.utc = dataContext.getTimeScales().getUTC();
- this.teme = dataContext.getFrames().getTEME();
- }
- /** {@inheritDoc} */
- @Override
- public SGP4OrbitalState convertToAveraged(final Orbit osculatingOrbit) {
- final FixedPointTleGenerationAlgorithm fixedPointAlgorithm = new FixedPointTleGenerationAlgorithm(getEpsilon(),
- getMaxIterations(), scale, utc, teme);
- final SpacecraftState osculatingState = new SpacecraftState(osculatingOrbit);
- final TLE templateTLe = new TLE(TEMPLATE_LINE_1, TEMPLATE_LINE_2, utc);
- final TLE tle = fixedPointAlgorithm.generate(osculatingState, templateTLe);
- return SGP4OrbitalState.of(tle, teme);
- }
- }