OmmData.java
/* Copyright 2002-2022 CS GROUP
* 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.files.ccsds.ndm.odm.omm;
import org.orekit.errors.OrekitException;
import org.orekit.errors.OrekitMessages;
import org.orekit.files.ccsds.ndm.odm.CartesianCovariance;
import org.orekit.files.ccsds.ndm.odm.KeplerianElements;
import org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey;
import org.orekit.files.ccsds.ndm.odm.SpacecraftParameters;
import org.orekit.files.ccsds.ndm.odm.UserDefined;
import org.orekit.files.ccsds.section.Data;
/**
* Container for Orbit Mean-elements Message data.
* @author Luc Maisonobe
* @since 11.0
*/
public class OmmData implements Data {
/** Keplerian elements block. */
private final KeplerianElements keplerianElementsBlock;
/** Spacecraft parameters block. */
private final SpacecraftParameters spacecraftParameters;
/** TLE block. */
private final OmmTle tleBlock;
/** Covariance matrix logical block being read. */
private final CartesianCovariance covarianceBlock;
/** User defined parameters. */
private final UserDefined userDefinedBlock;
/** Mass. */
private final double mass;
/** Simple constructor.
* @param keplerianElementsBlock Keplerian elements logical block
* @param spacecraftParameters spacecraft parameters logical block (may be null)
* @param tleBlock TLE logical block (may be null)
* @param covarianceBlock covariance matrix logical block (may be null)
* @param userDefinedBlock user-defined logical block
* @param mass mass (always defined, even if there is no {@code spacecraftParameters} block
*/
public OmmData(final KeplerianElements keplerianElementsBlock,
final SpacecraftParameters spacecraftParameters,
final OmmTle tleBlock,
final CartesianCovariance covarianceBlock,
final UserDefined userDefinedBlock,
final double mass) {
this.keplerianElementsBlock = keplerianElementsBlock;
this.spacecraftParameters = spacecraftParameters;
this.tleBlock = tleBlock;
this.covarianceBlock = covarianceBlock;
this.userDefinedBlock = userDefinedBlock;
this.mass = mass;
}
/** {@inheritDoc} */
@Override
public void validate(final double version) {
if (keplerianElementsBlock == null) {
throw new OrekitException(OrekitMessages.UNINITIALIZED_VALUE_FOR_KEY,
KeplerianElementsKey.EPOCH);
}
keplerianElementsBlock.validate(version);
if (spacecraftParameters != null) {
spacecraftParameters.validate(version);
}
if (tleBlock == null) {
// semi-major axis was not checked above, we do it now
keplerianElementsBlock.checkNotNaN(keplerianElementsBlock.getA(),
KeplerianElementsKey.SEMI_MAJOR_AXIS);
} else {
// in OMM with TLE block, only mean motion is allowed, not semi-major axis
keplerianElementsBlock.checkNotNaN(keplerianElementsBlock.getMeanMotion(),
KeplerianElementsKey.MEAN_MOTION);
tleBlock.validate(version);
}
if (covarianceBlock != null) {
covarianceBlock.setEpoch(keplerianElementsBlock.getEpoch());
covarianceBlock.validate(version);
}
if (userDefinedBlock != null) {
userDefinedBlock.validate(version);
}
}
/** Get the Keplerian elements logical block.
* @return Keplerian elements block
*/
public KeplerianElements getKeplerianElementsBlock() {
return keplerianElementsBlock;
}
/** Get the spacecraft parameters logical block.
* @return spacecraft parameters block (may be null)
*/
public SpacecraftParameters getSpacecraftParametersBlock() {
return spacecraftParameters;
}
/** Get the TLE logical block.
* @return TLE block
*/
public OmmTle getTLEBlock() {
return tleBlock;
}
/** Get the covariance matrix logical block.
* @return covariance matrix block (may be null)
*/
public CartesianCovariance getCovarianceBlock() {
return covarianceBlock;
}
/** Get the user defined parameters logical block.
* @return user defined parameters block (may be null)
*/
public UserDefined getUserDefinedBlock() {
return userDefinedBlock;
}
/** Get the mass.
* @return mass
*/
public double getMass() {
return mass;
}
}