SP3File.java
/* Copyright 2002-2012 Space Applications Services
* 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.sp3;
import java.util.ArrayList;
import java.util.Collections;
import java.util.LinkedHashMap;
import java.util.List;
import java.util.Locale;
import java.util.Map;
import java.util.function.Function;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.orekit.files.general.EphemerisFile;
import org.orekit.frames.Frame;
import org.orekit.propagation.BoundedPropagator;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.TimeScale;
import org.orekit.utils.CartesianDerivativesFilter;
import org.orekit.utils.TimeStampedPVCoordinates;
/**
* Represents a parsed SP3 orbit file.
* @author Thomas Neidhart
* @author Evan Ward
*/
public class SP3File implements EphemerisFile {
/** String representation of the center of ephemeris coordinate system. **/
public static final String SP3_FRAME_CENTER_STRING = "EARTH";
/** File type indicator. */
public enum SP3FileType {
/** GPS only file. */
GPS,
/** Mixed file. */
MIXED,
/** GLONASS only file. */
GLONASS,
/** LEO only file. */
LEO,
/** Galileo only file. */
GALILEO,
/** COMPASS only file. */
COMPASS,
/** QZSS only file. */
QZSS,
/** undefined file format. */
UNDEFINED
}
/** Orbit type indicator. */
public enum SP3OrbitType {
/** fitted. */
FIT,
/** extrapolated or predicted. */
EXT,
/** broadcast. */
BCT,
/** fitted after applying a Helmert transformation. */
HLM,
/** other type, defined by SP3 file producing agency.
* @since 9.3
*/
OTHER;
/** Parse a string to get the type.
* @param s string to parse
* @return the type corresponding to the string
*/
public static SP3OrbitType parseType(final String s) {
final String normalizedString = s.trim().toUpperCase(Locale.US);
if ("EST".equals(normalizedString)) {
return FIT;
} else if ("BHN".equals(normalizedString)) {
// ESOC navigation team uses BHN for files produced
// by their main parameter estimation program Bahn
return FIT;
} else if ("PRO".equals(normalizedString)) {
// ESOC navigation team uses PRO for files produced
// by their orbit propagation program Propag
return EXT;
} else {
try {
return valueOf(normalizedString);
} catch (IllegalArgumentException iae) {
return OTHER;
}
}
}
}
/** Time system used throughout this SP3 file. */
public enum TimeSystem {
/** Global Positioning System. */
GPS,
/** GLONASS. */
GLO,
/** GALILEO. */
GAL,
/** International Atomic Time. */
TAI,
/** Coordinated Universal Time. */
UTC,
/** Quasi-Zenith System. */
QZS
}
/** File type. */
private SP3FileType type;
/** Time system. */
private TimeSystem timeSystem;
/** Epoch of the file. */
private AbsoluteDate epoch;
/** GPS week. */
private int gpsWeek;
/** Seconds of the current GPS week. */
private double secondsOfWeek;
/** Julian day. */
private int julianDay;
/** Day fraction. */
private double dayFraction;
/** Time-interval between epochs. */
private double epochInterval;
/** Number of epochs. */
private int numberOfEpochs;
/** Coordinate system. */
private String coordinateSystem;
/** Data used indicator. */
private String dataUsed;
/** Orbit type. */
private SP3OrbitType orbitType;
/** Key for orbit type.
* @since 9.3
*/
private String orbitTypeKey;
/** Agency providing the file. */
private String agency;
/** Indicates if data contains velocity or not. */
private CartesianDerivativesFilter filter;
/** Time scale of dates in the ephemeris file. */
private TimeScale timeScale;
/** Time scale, as specified in the file. */
private String timeScaleString;
/** Standard gravitational parameter in m^3 / s^2. */
private final double mu;
/** Number of samples to use when interpolating. */
private final int interpolationSamples;
/** Maps {@link #coordinateSystem} to a {@link Frame}. */
private final Function<? super String, ? extends Frame> frameBuilder;
/** A map containing satellite information. */
private Map<String, SP3Ephemeris> satellites;
/**
* Create a new SP3 file object.
*
* @param mu is the standard gravitational parameter in m^3 / s^2.
* @param interpolationSamples number of samples to use in interpolation.
* @param frameBuilder for constructing a reference frame from the identifier
*/
SP3File(final double mu,
final int interpolationSamples,
final Function<? super String, ? extends Frame> frameBuilder) {
this.mu = mu;
this.interpolationSamples = interpolationSamples;
this.frameBuilder = frameBuilder;
// must be linked has map to preserve order of satellites in the file.
satellites = new LinkedHashMap<>();
}
/**
* Set the derivatives filter.
*
* @param filter that indicates which derivatives of position are available.
*/
void setFilter(final CartesianDerivativesFilter filter) {
this.filter = filter;
}
/**
* Set the time scale.
*
* @param timeScale use to parse dates in this file.
*/
void setTimeScale(final TimeScale timeScale) {
this.timeScale = timeScale;
}
/**
* Set the string used to define the time scale.
*
* @param timeScaleString the time scale identifier used in the file.
*/
void setTimeScaleString(final String timeScaleString) {
this.timeScaleString = timeScaleString;
}
/** Returns the {@link SP3FileType} associated with this SP3 file.
* @return the file type for this SP3 file
*/
public SP3FileType getType() {
return type;
}
/** Set the file type for this SP3 file.
* @param fileType the file type to be set
*/
void setType(final SP3FileType fileType) {
this.type = fileType;
}
/** Returns the {@link TimeSystem} used to time-stamp position entries.
* @return the {@link TimeSystem} of the orbit file
*/
public TimeSystem getTimeSystem() {
return timeSystem;
}
/** Set the time system used in this SP3 file.
* @param system the time system to be set
*/
void setTimeSystem(final TimeSystem system) {
this.timeSystem = system;
}
/** Returns the data used indicator from the SP3 file.
* @return the data used indicator (unparsed)
*/
public String getDataUsed() {
return dataUsed;
}
/** Set the data used indicator for this SP3 file.
* @param data the data used indicator to be set
*/
void setDataUsed(final String data) {
this.dataUsed = data;
}
/** Returns the start epoch of the orbit file.
* @return the start epoch
*/
public AbsoluteDate getEpoch() {
return epoch;
}
/** Set the epoch of the SP3 file.
* @param time the epoch to be set
*/
void setEpoch(final AbsoluteDate time) {
this.epoch = time;
}
/** Returns the GPS week as contained in the SP3 file.
* @return the GPS week of the SP3 file
*/
public int getGpsWeek() {
return gpsWeek;
}
/** Set the GPS week of the SP3 file.
* @param week the GPS week to be set
*/
void setGpsWeek(final int week) {
this.gpsWeek = week;
}
/** Returns the seconds of the GPS week as contained in the SP3 file.
* @return the seconds of the GPS week
*/
public double getSecondsOfWeek() {
return secondsOfWeek;
}
/** Set the seconds of the GPS week for this SP3 file.
* @param seconds the seconds to be set
*/
void setSecondsOfWeek(final double seconds) {
this.secondsOfWeek = seconds;
}
/** Returns the julian day for this SP3 file.
* @return the julian day
*/
public int getJulianDay() {
return julianDay;
}
/** Set the julian day for this SP3 file.
* @param day the julian day to be set
*/
void setJulianDay(final int day) {
this.julianDay = day;
}
/** Returns the day fraction for this SP3 file.
* @return the day fraction
*/
public double getDayFraction() {
return dayFraction;
}
/** Set the day fraction for this SP3 file.
* @param fraction the day fraction to be set
*/
void setDayFraction(final double fraction) {
this.dayFraction = fraction;
}
/** Returns the time interval between epochs (in seconds).
* @return the time interval between epochs
*/
public double getEpochInterval() {
return epochInterval;
}
/** Set the epoch interval for this SP3 file.
* @param interval the interval between orbit entries
*/
void setEpochInterval(final double interval) {
this.epochInterval = interval;
}
/** Returns the number of epochs contained in this orbit file.
* @return the number of epochs
*/
public int getNumberOfEpochs() {
return numberOfEpochs;
}
/** Set the number of epochs as contained in the SP3 file.
* @param epochCount the number of epochs to be set
*/
void setNumberOfEpochs(final int epochCount) {
this.numberOfEpochs = epochCount;
}
/** Returns the coordinate system of the entries in this orbit file.
* @return the coordinate system
*/
public String getCoordinateSystem() {
return coordinateSystem;
}
/** Set the coordinate system used for the orbit entries.
* @param system the coordinate system to be set
*/
void setCoordinateSystem(final String system) {
this.coordinateSystem = system;
}
/** Returns the {@link SP3OrbitType} for this SP3 file.
* @return the orbit type
*/
public SP3OrbitType getOrbitType() {
return orbitType;
}
/** Returns the orbit type key for this SP3 file.
* @return the orbit type key
* @since 9.3
*/
public String getOrbitTypeKey() {
return orbitTypeKey;
}
/** Set the orbit type key for this SP3 file.
* @param oTypeKey the orbit type key to be set
* @since 9.3
*/
void setOrbitTypeKey(final String oTypeKey) {
this.orbitTypeKey = oTypeKey;
this.orbitType = SP3OrbitType.parseType(oTypeKey);
}
/** Returns the agency that prepared this SP3 file.
* @return the agency
*/
public String getAgency() {
return agency;
}
/** Set the agency string for this SP3 file.
* @param agencyStr the agency string to be set
*/
void setAgency(final String agencyStr) {
this.agency = agencyStr;
}
/** Add a new satellite with a given identifier to the list of
* stored satellites.
* @param satId the satellite identifier
*/
public void addSatellite(final String satId) {
// only add satellites which have not been added before
satellites.putIfAbsent(satId, new SP3Ephemeris(satId));
}
@Override
public Map<String, SP3Ephemeris> getSatellites() {
return Collections.unmodifiableMap(satellites);
}
/** Get the number of satellites contained in this orbit file.
* @return the number of satellites
*/
public int getSatelliteCount() {
return satellites.size();
}
/**
* Set the formal accuracy for a satellite.
*
* @param index is the index of the satellite.
* @param accuracy of the satellite, in m.
*/
void setAccuracy(final int index, final double accuracy) {
int n = index;
for (final SP3Ephemeris ephemeris : satellites.values()) {
if (n == 0) {
ephemeris.setAccuracy(accuracy);
return;
}
n--;
}
}
/**
* Get the formal accuracy for a satellite.
*
* @param index is the index of the satellite.
* @return accuracy of the satellite, in m.
*/
double getAccuracy(final int index) {
int n = index;
for (final SP3Ephemeris ephemeris : satellites.values()) {
if (n == 0) {
return ephemeris.getAccuracy();
}
n--;
}
return Double.NaN;
}
/** Tests whether a satellite with the given id is contained in this orbit
* file.
* @param satId the satellite id
* @return {@code true} if the satellite is contained in the file,
* {@code false} otherwise
*/
public boolean containsSatellite(final String satId) {
return satellites.containsKey(satId);
}
/**
* Adds a new P/V coordinate for a given satellite.
*
* @param satId the satellite identifier
* @param coord the P/V coordinate of the satellite
*/
void addSatelliteCoordinate(final String satId, final SP3Coordinate coord) {
satellites.get(satId).coordinates.add(coord);
}
/** An ephemeris for a single satellite in a SP3 file. */
public class SP3Ephemeris implements SatelliteEphemeris, EphemerisSegment {
/** Satellite ID. */
private final String id;
/** Ephemeris Data. */
private final List<SP3Coordinate> coordinates;
/** Accuracy in m. */
private double accuracy;
/**
* Create an ephemeris for a single satellite.
*
* @param id of the satellite.
*/
SP3Ephemeris(final String id) {
this.id = id;
this.coordinates = new ArrayList<>();
}
@Override
public String getId() {
return this.id;
}
@Override
public double getMu() {
return mu;
}
@Override
public String getFrameCenterString() {
return SP3_FRAME_CENTER_STRING;
}
@Override
public String getFrameString() {
return getCoordinateSystem();
}
@Override
public Frame getFrame() {
return frameBuilder.apply(getFrameString());
}
@Override
public String getTimeScaleString() {
return timeScaleString;
}
@Override
public TimeScale getTimeScale() {
return timeScale;
}
@Override
public int getInterpolationSamples() {
return interpolationSamples;
}
@Override
public CartesianDerivativesFilter getAvailableDerivatives() {
return filter;
}
@Override
public List<SP3Coordinate> getCoordinates() {
return Collections.unmodifiableList(this.coordinates);
}
/** Returns a list containing only {@code this}. */
@Override
public List<SP3Ephemeris> getSegments() {
return Collections.singletonList(this);
}
@Override
public AbsoluteDate getStart() {
return coordinates.get(0).getDate();
}
@Override
public AbsoluteDate getStop() {
return coordinates.get(coordinates.size() - 1).getDate();
}
@Override
public BoundedPropagator getPropagator() {
return EphemerisSegment.super.getPropagator();
}
/**
* Set the accuracy for this satellite.
*
* @param accuracy in m.
*/
void setAccuracy(final double accuracy) {
this.accuracy = accuracy;
}
/**
* Get the formal accuracy for this satellite.
*
* <p>The accuracy is limited by the SP3 standard to be a power of 2 in mm.
* The value returned here is in meters.</p>
*
* @return magnitude of one standard deviation, in m.
*/
public double getAccuracy() {
return accuracy;
}
}
/** A single record of position clock and possibly derivatives in an SP3 file. */
public static class SP3Coordinate extends TimeStampedPVCoordinates {
/** Serializable UID. */
private static final long serialVersionUID = 20161116L;
/** Clock correction in s. */
private final double clock;
/** Clock rate in s / s. */
private final double clockRate;
/**
* Create a coordinate with only position.
*
* @param date of validity.
* @param position of the satellite.
* @param clock correction in s.
*/
SP3Coordinate(final AbsoluteDate date,
final Vector3D position,
final double clock) {
this(date, position, Vector3D.ZERO, clock, 0);
}
/**
* Create a coordinate with position and velocity.
*
* @param date of validity.
* @param position of the satellite.
* @param velocity of the satellite.
* @param clock correction in s.
* @param clockRate in s / s.
*/
SP3Coordinate(final AbsoluteDate date,
final Vector3D position,
final Vector3D velocity,
final double clock,
final double clockRate) {
super(date, position, velocity, Vector3D.ZERO);
this.clock = clock;
this.clockRate = clockRate;
}
/**
* Returns the clock correction value.
*
* @return the clock correction in s.
*/
public double getClockCorrection() {
return clock;
}
/**
* Returns the clock rate.
*
* @return the clock rate of change in s/s.
*/
public double getClockRateChange() {
return clockRate;
}
}
}