SP3Parser.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.io.BufferedReader;
import java.io.IOException;
import java.io.Reader;
import java.util.ArrayList;
import java.util.Arrays;
import java.util.Collections;
import java.util.List;
import java.util.Locale;
import java.util.Scanner;
import java.util.function.Function;
import java.util.regex.Pattern;
import org.hipparchus.exception.LocalizedCoreFormats;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.orekit.annotation.DefaultDataContext;
import org.orekit.data.DataContext;
import org.orekit.data.DataSource;
import org.orekit.errors.OrekitException;
import org.orekit.errors.OrekitIllegalArgumentException;
import org.orekit.errors.OrekitMessages;
import org.orekit.files.general.EphemerisFileParser;
import org.orekit.frames.Frame;
import org.orekit.gnss.TimeSystem;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.DateComponents;
import org.orekit.time.DateTimeComponents;
import org.orekit.time.TimeComponents;
import org.orekit.time.TimeScale;
import org.orekit.time.TimeScales;
import org.orekit.utils.CartesianDerivativesFilter;
import org.orekit.utils.Constants;
import org.orekit.utils.IERSConventions;
/** A parser for the SP3 orbit file format. It supports all formats from sp3-a
* to sp3-d.
* <p>
* <b>Note:</b> this parser is thread-safe, so calling {@link #parse} from
* different threads is allowed.
* </p>
* @see <a href="https://files.igs.org/pub/data/format/sp3_docu.txt">SP3-a file format</a>
* @see <a href="https://files.igs.org/pub/data/format/sp3c.txt">SP3-c file format</a>
* @see <a href="https://files.igs.org/pub/data/format/sp3d.pdf">SP3-d file format</a>
* @author Thomas Neidhart
* @author Luc Maisonobe
*/
public class SP3Parser implements EphemerisFileParser<SP3> {
/** String representation of the center of ephemeris coordinate system. **/
public static final String SP3_FRAME_CENTER_STRING = "EARTH";
/** Spaces delimiters. */
private static final String SPACES = "\\s+";
/** Standard gravitational parameter in m³/s². */
private final double mu;
/** Number of data points to use in interpolation. */
private final int interpolationSamples;
/** Mapping from frame identifier in the file to a {@link Frame}. */
private final Function<? super String, ? extends Frame> frameBuilder;
/** Set of time scales. */
private final TimeScales timeScales;
/**
* Create an SP3 parser using default values.
*
* <p>This constructor uses the {@link DataContext#getDefault() default data context}.
*
* @see #SP3Parser(double, int, Function)
*/
@DefaultDataContext
public SP3Parser() {
this(Constants.EIGEN5C_EARTH_MU, 7, SP3Parser::guessFrame);
}
/**
* Create an SP3 parser and specify the extra information needed to create a {@link
* org.orekit.propagation.Propagator Propagator} from the ephemeris data.
*
* <p>This constructor uses the {@link DataContext#getDefault() default data context}.
*
* @param mu is the standard gravitational parameter to use for
* creating {@link org.orekit.orbits.Orbit Orbits} from
* the ephemeris data. See {@link Constants}.
* @param interpolationSamples is the number of samples to use when interpolating.
* @param frameBuilder is a function that can construct a frame from an SP3
* coordinate system string. The coordinate system can be
* any 5 character string e.g. ITR92, IGb08.
* @see #SP3Parser(double, int, Function, TimeScales)
*/
@DefaultDataContext
public SP3Parser(final double mu,
final int interpolationSamples,
final Function<? super String, ? extends Frame> frameBuilder) {
this(mu, interpolationSamples, frameBuilder,
DataContext.getDefault().getTimeScales());
}
/**
* Create an SP3 parser and specify the extra information needed to create a {@link
* org.orekit.propagation.Propagator Propagator} from the ephemeris data.
*
* @param mu is the standard gravitational parameter to use for
* creating {@link org.orekit.orbits.Orbit Orbits} from
* the ephemeris data. See {@link Constants}.
* @param interpolationSamples is the number of samples to use when interpolating.
* @param frameBuilder is a function that can construct a frame from an SP3
* coordinate system string. The coordinate system can be
* @param timeScales the set of time scales used for parsing dates.
* @since 10.1
*/
public SP3Parser(final double mu,
final int interpolationSamples,
final Function<? super String, ? extends Frame> frameBuilder,
final TimeScales timeScales) {
this.mu = mu;
this.interpolationSamples = interpolationSamples;
this.frameBuilder = frameBuilder;
this.timeScales = timeScales;
}
/**
* Default string to {@link Frame} conversion for {@link #SP3Parser()}.
*
* <p>This method uses the {@link DataContext#getDefault() default data context}.
*
* @param name of the frame.
* @return ITRF based on 2010 conventions,
* with tidal effects considered during EOP interpolation.
*/
@DefaultDataContext
private static Frame guessFrame(final String name) {
return DataContext.getDefault().getFrames()
.getITRF(IERSConventions.IERS_2010, false);
}
@Override
public SP3 parse(final DataSource source) {
try (Reader reader = source.getOpener().openReaderOnce();
BufferedReader br = (reader == null) ? null : new BufferedReader(reader)) {
if (br == null) {
throw new OrekitException(OrekitMessages.UNABLE_TO_FIND_FILE, source.getName());
}
// initialize internal data structures
final ParseInfo pi = new ParseInfo(source.getName());
int lineNumber = 0;
Iterable<LineParser> candidateParsers = Collections.singleton(LineParser.HEADER_VERSION);
nextLine:
for (String line = br.readLine(); line != null; line = br.readLine()) {
++lineNumber;
for (final LineParser candidate : candidateParsers) {
if (candidate.canHandle(line)) {
try {
candidate.parse(line, pi);
if (pi.done) {
break nextLine;
}
candidateParsers = candidate.allowedNext();
continue nextLine;
} catch (StringIndexOutOfBoundsException | NumberFormatException e) {
throw new OrekitException(e,
OrekitMessages.UNABLE_TO_PARSE_LINE_IN_FILE,
lineNumber, pi.fileName, line);
}
}
}
// no parsers found for this line
throw new OrekitException(OrekitMessages.UNABLE_TO_PARSE_LINE_IN_FILE,
lineNumber, pi.fileName, line);
}
pi.file.validate(true, pi.fileName);
return pi.file;
} catch (IOException ioe) {
throw new OrekitException(ioe, LocalizedCoreFormats.SIMPLE_MESSAGE, ioe.getLocalizedMessage());
}
}
/** Transient data used for parsing a sp3 file. The data is kept in a
* separate data structure to make the parser thread-safe.
* <p><b>Note</b>: The class intentionally does not provide accessor
* methods, as it is only used internally for parsing a SP3 file.</p>
*/
private class ParseInfo {
/** File name.
* @since 12.0
*/
private final String fileName;
/** Set of time scales for parsing dates. */
private final TimeScales timeScales;
/** The corresponding SP3File object. */
private SP3 file;
/** The latest epoch as read from the SP3 file. */
private AbsoluteDate latestEpoch;
/** The latest position as read from the SP3 file. */
private Vector3D latestPosition;
/** The latest position accuracy as read from the SP3 file.
* @since 12.0
*/
private Vector3D latestPositionAccuracy;
/** The latest clock value as read from the SP3 file. */
private double latestClock;
/** The latest clock value as read from the SP3 file.
* @since 12.0
*/
private double latestClockAccuracy;
/** The latest clock event flag as read from the SP3 file.
* @since 12.0
*/
private boolean latestClockEvent;
/** The latest clock prediction flag as read from the SP3 file.
* @since 12.0
*/
private boolean latestClockPrediction;
/** The latest orbit maneuver event flag as read from the SP3 file.
* @since 12.0
*/
private boolean latestOrbitManeuverEvent;
/** The latest orbit prediction flag as read from the SP3 file.
* @since 12.0
*/
private boolean latestOrbitPrediction;
/** Indicates if the SP3 file has velocity entries. */
private boolean hasVelocityEntries;
/** The timescale used in the SP3 file. */
private TimeScale timeScale;
/** Date and time of the file. */
private DateTimeComponents epoch;
/** The number of satellites as contained in the SP3 file. */
private int maxSatellites;
/** The number of satellites accuracies already seen. */
private int nbAccuracies;
/** End Of File reached indicator. */
private boolean done;
/** Create a new {@link ParseInfo} object.
* @param fileName file name
*/
protected ParseInfo(final String fileName) {
this.fileName = fileName;
this.timeScales = SP3Parser.this.timeScales;
file = new SP3(mu, interpolationSamples, frameBuilder.apply(SP3_FRAME_CENTER_STRING));
latestEpoch = null;
latestPosition = null;
latestClock = 0.0;
hasVelocityEntries = false;
epoch = DateTimeComponents.JULIAN_EPOCH;
timeScale = timeScales.getGPS();
maxSatellites = 0;
nbAccuracies = 0;
done = false;
}
}
/** Parsers for specific lines. */
private enum LineParser {
/** Parser for version, epoch, data used and agency information. */
HEADER_VERSION("^#[a-z].*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
try (Scanner s1 = new Scanner(line);
Scanner s2 = s1.useDelimiter(SPACES);
Scanner scanner = s2.useLocale(Locale.US)) {
scanner.skip("#");
final String v = scanner.next();
pi.file.getHeader().setVersion(v.substring(0, 1).toLowerCase().charAt(0));
pi.hasVelocityEntries = "V".equals(v.substring(1, 2));
pi.file.getHeader().setFilter(pi.hasVelocityEntries ?
CartesianDerivativesFilter.USE_PV :
CartesianDerivativesFilter.USE_P);
final int year = Integer.parseInt(v.substring(2));
final int month = scanner.nextInt();
final int day = scanner.nextInt();
final int hour = scanner.nextInt();
final int minute = scanner.nextInt();
final double second = scanner.nextDouble();
pi.epoch = new DateTimeComponents(year, month, day,
hour, minute, second);
final int numEpochs = scanner.nextInt();
pi.file.getHeader().setNumberOfEpochs(numEpochs);
// data used indicator
final String fullSpec = scanner.next();
final List<DataUsed> dataUsed = new ArrayList<>();
for (final String specifier : fullSpec.split("\\+")) {
dataUsed.add(DataUsed.parse(specifier, pi.fileName, pi.file.getHeader().getVersion()));
}
pi.file.getHeader().setDataUsed(dataUsed);
pi.file.getHeader().setCoordinateSystem(scanner.next());
pi.file.getHeader().setOrbitTypeKey(scanner.next());
pi.file.getHeader().setAgency(scanner.next());
}
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Collections.singleton(HEADER_DATE_TIME_REFERENCE);
}
},
/** Parser for additional date/time references in gps/julian day notation. */
HEADER_DATE_TIME_REFERENCE("^##.*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
try (Scanner s1 = new Scanner(line);
Scanner s2 = s1.useDelimiter(SPACES);
Scanner scanner = s2.useLocale(Locale.US)) {
scanner.skip("##");
// gps week
pi.file.getHeader().setGpsWeek(scanner.nextInt());
// seconds of week
pi.file.getHeader().setSecondsOfWeek(scanner.nextDouble());
// epoch interval
pi.file.getHeader().setEpochInterval(scanner.nextDouble());
// modified julian day
pi.file.getHeader().setModifiedJulianDay(scanner.nextInt());
// day fraction
pi.file.getHeader().setDayFraction(scanner.nextDouble());
}
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Collections.singleton(HEADER_SAT_IDS);
}
},
/** Parser for satellites identifiers. */
HEADER_SAT_IDS("^\\+ .*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
if (pi.maxSatellites == 0) {
// this is the first ids line, it also contains the number of satellites
pi.maxSatellites = Integer.parseInt(line.substring(3, 6).trim());
}
final int lineLength = line.length();
int count = pi.file.getSatelliteCount();
int startIdx = 9;
while (count++ < pi.maxSatellites && (startIdx + 3) <= lineLength) {
final String satId = line.substring(startIdx, startIdx + 3).trim();
if (satId.length() > 0) {
pi.file.addSatellite(satId);
}
startIdx += 3;
}
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Arrays.asList(HEADER_SAT_IDS, HEADER_ACCURACY);
}
},
/** Parser for general accuracy information for each satellite. */
HEADER_ACCURACY("^\\+\\+.*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
final int lineLength = line.length();
int startIdx = 9;
while (pi.nbAccuracies < pi.maxSatellites && (startIdx + 3) <= lineLength) {
final String sub = line.substring(startIdx, startIdx + 3).trim();
if (sub.length() > 0) {
final int exponent = Integer.parseInt(sub);
// the accuracy is calculated as 2**exp (in mm)
pi.file.getHeader().setAccuracy(pi.nbAccuracies++,
SP3Utils.siAccuracy(SP3Utils.POSITION_ACCURACY_UNIT,
SP3Utils.POS_VEL_BASE_ACCURACY,
exponent));
}
startIdx += 3;
}
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Arrays.asList(HEADER_ACCURACY, HEADER_TIME_SYSTEM);
}
},
/** Parser for time system. */
HEADER_TIME_SYSTEM("^%c.*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
if (pi.file.getHeader().getType() == null) {
// this the first custom fields line, the only one really used
pi.file.getHeader().setType(SP3FileType.parse(line.substring(3, 5).trim()));
// now identify the time system in use
final String tsStr = line.substring(9, 12).trim();
final TimeSystem ts;
if (tsStr.equalsIgnoreCase("ccc")) {
ts = TimeSystem.GPS;
} else {
ts = TimeSystem.parseTimeSystem(tsStr);
}
pi.file.getHeader().setTimeSystem(ts);
pi.timeScale = ts.getTimeScale(pi.timeScales);
// now we know the time scale used, we can set the file epoch
pi.file.getHeader().setEpoch(new AbsoluteDate(pi.epoch, pi.timeScale));
}
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Arrays.asList(HEADER_TIME_SYSTEM, HEADER_STANDARD_DEVIATIONS);
}
},
/** Parser for standard deviations of position/velocity/clock components. */
HEADER_STANDARD_DEVIATIONS("^%f.*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
final double posVelBase = Double.parseDouble(line.substring(3, 13).trim());
if (posVelBase != 0.0) {
// (mm or 10⁻⁴ mm/s)
pi.file.getHeader().setPosVelBase(posVelBase);
}
final double clockBase = Double.parseDouble(line.substring(14, 26).trim());
if (clockBase != 0.0) {
// (ps or 10⁻⁴ ps/s)
pi.file.getHeader().setClockBase(clockBase);
}
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Arrays.asList(HEADER_STANDARD_DEVIATIONS, HEADER_CUSTOM_PARAMETERS);
}
},
/** Parser for custom parameters. */
HEADER_CUSTOM_PARAMETERS("^%i.*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
// ignore additional custom parameters
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Arrays.asList(HEADER_CUSTOM_PARAMETERS, HEADER_COMMENTS);
}
},
/** Parser for comments. */
HEADER_COMMENTS("^[%]?/\\*.*|") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
pi.file.getHeader().addComment(line.substring(line.indexOf('*') + 1).trim());
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Arrays.asList(HEADER_COMMENTS, DATA_EPOCH);
}
},
/** Parser for epoch. */
DATA_EPOCH("^\\* .*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
final int year;
final int month;
final int day;
final int hour;
final int minute;
final double second;
try (Scanner s1 = new Scanner(line);
Scanner s2 = s1.useDelimiter(SPACES);
Scanner scanner = s2.useLocale(Locale.US)) {
scanner.skip("\\*");
year = scanner.nextInt();
month = scanner.nextInt();
day = scanner.nextInt();
hour = scanner.nextInt();
minute = scanner.nextInt();
second = scanner.nextDouble();
}
// some SP3 files have weird epochs as in the following three examples, where
// the middle dates are wrong
//
// * 2016 7 6 16 58 0.00000000
// PL51 11872.234459 3316.551981 101.400098 999999.999999
// VL51 8054.606014 -27076.640110 -53372.762255 999999.999999
// * 2016 7 6 16 60 0.00000000
// PL51 11948.228978 2986.113872 -538.901114 999999.999999
// VL51 4605.419303 -27972.588048 -53316.820671 999999.999999
// * 2016 7 6 17 2 0.00000000
// PL51 11982.652569 2645.786926 -1177.549463 999999.999999
// VL51 1128.248622 -28724.293303 -53097.358387 999999.999999
//
// * 2016 7 6 23 58 0.00000000
// PL51 3215.382310 -7958.586164 8812.395707
// VL51 -18058.659942 -45834.335707 -34496.540437
// * 2016 7 7 24 0 0.00000000
// PL51 2989.229334 -8494.421415 8385.068555
// VL51 -19617.027447 -43444.824985 -36706.159070
// * 2016 7 7 0 2 0.00000000
// PL51 2744.983592 -9000.639164 7931.904779
// VL51 -21072.925764 -40899.633288 -38801.567078
//
// * 2021 12 31 0 0 0.00000000
// PL51 6578.459330 5572.231927 -8703.502054
// VL51 -5356.007694 -48869.881161 -35036.676469
// * 2022 1 0 0 2 0.00000000
// PL51 6499.035610 4978.263048 -9110.135595
// VL51 -7881.633197 -50092.564035 -32717.740919
// * 2022 1 0 0 4 0.00000000
// PL51 6389.313975 4370.794537 -9488.314264
// VL51 -10403.797055 -51119.231402 -30295.421935
// In the first case, the date should really be 2016 7 6 17 0 0.00000000,
// i.e as the minutes field overflows, the hours field should be incremented
// In the second case, the date should really be 2016 7 7 0 0 0.00000000,
// i.e. as the hours field overflows, the day field should be kept as is
// we cannot be sure how carry was managed when these bogus files were written
// so we try different options, incrementing or not previous field, and selecting
// the closest one to expected date
// In the third case, there are two different errors: the date is globally
// shifted to the left by one character, and the day is 0 instead of 1
DateComponents dc = day == 0 ?
new DateComponents(new DateComponents(year, month, 1), -1) :
new DateComponents(year, month, day);
final List<AbsoluteDate> candidates = new ArrayList<>();
int h = hour;
int m = minute;
double s = second;
if (s >= 60.0) {
s -= 60;
addCandidate(candidates, dc, h, m, s, pi.timeScale);
m++;
}
if (m > 59) {
m = 0;
addCandidate(candidates, dc, h, m, s, pi.timeScale);
h++;
}
if (h > 23) {
h = 0;
addCandidate(candidates, dc, h, m, s, pi.timeScale);
dc = new DateComponents(dc, 1);
}
addCandidate(candidates, dc, h, m, s, pi.timeScale);
final AbsoluteDate expected = pi.latestEpoch == null ?
pi.file.getHeader().getEpoch() :
pi.latestEpoch.shiftedBy(pi.file.getHeader().getEpochInterval());
pi.latestEpoch = null;
for (final AbsoluteDate candidate : candidates) {
if (FastMath.abs(candidate.durationFrom(expected)) < 0.01 * pi.file.getHeader().getEpochInterval()) {
pi.latestEpoch = candidate;
}
}
if (pi.latestEpoch == null) {
// no date recognized, just parse again the initial fields
// in order to generate again an exception
pi.latestEpoch = new AbsoluteDate(year, month, day, hour, minute, second, pi.timeScale);
}
}
/** Add an epoch candidate to a list.
* @param candidates list of candidates
* @param dc date components
* @param hour hour number from 0 to 23
* @param minute minute number from 0 to 59
* @param second second number from 0.0 to 60.0 (excluded)
* @param timeScale time scale
* @since 11.1.1
*/
private void addCandidate(final List<AbsoluteDate> candidates, final DateComponents dc,
final int hour, final int minute, final double second,
final TimeScale timeScale) {
try {
candidates.add(new AbsoluteDate(dc, new TimeComponents(hour, minute, second), timeScale));
} catch (OrekitIllegalArgumentException oiae) {
// ignored
}
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Collections.singleton(DATA_POSITION);
}
},
/** Parser for position. */
DATA_POSITION("^P.*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
final String satelliteId = line.substring(1, 4).trim();
if (!pi.file.containsSatellite(satelliteId)) {
pi.latestPosition = Vector3D.ZERO;
} else {
final SP3Header header = pi.file.getHeader();
// the position values are in km and have to be converted to m
pi.latestPosition = new Vector3D(SP3Utils.POSITION_UNIT.toSI(Double.parseDouble(line.substring(4, 18).trim())),
SP3Utils.POSITION_UNIT.toSI(Double.parseDouble(line.substring(18, 32).trim())),
SP3Utils.POSITION_UNIT.toSI(Double.parseDouble(line.substring(32, 46).trim())));
// clock (microsec)
pi.latestClock = SP3Utils.CLOCK_UNIT.toSI(line.trim().length() <= 46 ?
SP3Utils.DEFAULT_CLOCK_VALUE :
Double.parseDouble(line.substring(46, 60).trim()));
if (pi.latestPosition.getNorm() > 0) {
if (line.length() < 69 ||
line.substring(61, 63).trim().length() == 0 ||
line.substring(64, 66).trim().length() == 0 ||
line.substring(67, 69).trim().length() == 0) {
pi.latestPositionAccuracy = null;
} else {
pi.latestPositionAccuracy = new Vector3D(SP3Utils.siAccuracy(SP3Utils.POSITION_ACCURACY_UNIT,
header.getPosVelBase(),
Integer.parseInt(line.substring(61, 63).trim())),
SP3Utils.siAccuracy(SP3Utils.POSITION_ACCURACY_UNIT,
header.getPosVelBase(),
Integer.parseInt(line.substring(64, 66).trim())),
SP3Utils.siAccuracy(SP3Utils.POSITION_ACCURACY_UNIT,
header.getPosVelBase(),
Integer.parseInt(line.substring(67, 69).trim())));
}
if (line.length() < 73 || line.substring(70, 73).trim().length() == 0) {
pi.latestClockAccuracy = Double.NaN;
} else {
pi.latestClockAccuracy = SP3Utils.siAccuracy(SP3Utils.CLOCK_ACCURACY_UNIT,
header.getClockBase(),
Integer.parseInt(line.substring(70, 73).trim()));
}
pi.latestClockEvent = line.length() < 75 ? false : line.substring(74, 75).equals("E");
pi.latestClockPrediction = line.length() < 76 ? false : line.substring(75, 76).equals("P");
pi.latestOrbitManeuverEvent = line.length() < 79 ? false : line.substring(78, 79).equals("M");
pi.latestOrbitPrediction = line.length() < 80 ? false : line.substring(79, 80).equals("P");
if (!pi.hasVelocityEntries) {
final SP3Coordinate coord =
new SP3Coordinate(pi.latestEpoch,
pi.latestPosition, pi.latestPositionAccuracy,
Vector3D.ZERO, null,
pi.latestClock, pi.latestClockAccuracy,
0.0, Double.NaN,
pi.latestClockEvent, pi.latestClockPrediction,
pi.latestOrbitManeuverEvent, pi.latestOrbitPrediction);
pi.file.getEphemeris(satelliteId).addCoordinate(coord, header.getEpochInterval());
}
}
}
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Arrays.asList(DATA_EPOCH, DATA_POSITION, DATA_POSITION_CORRELATION, DATA_VELOCITY, EOF);
}
},
/** Parser for position correlation. */
DATA_POSITION_CORRELATION("^EP.*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
// ignored for now
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Arrays.asList(DATA_EPOCH, DATA_POSITION, DATA_VELOCITY, EOF);
}
},
/** Parser for velocity. */
DATA_VELOCITY("^V.*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
final String satelliteId = line.substring(1, 4).trim();
if (pi.file.containsSatellite(satelliteId) && pi.latestPosition.getNorm() > 0) {
final SP3Header header = pi.file.getHeader();
// the velocity values are in dm/s and have to be converted to m/s
final Vector3D velocity = new Vector3D(SP3Utils.VELOCITY_UNIT.toSI(Double.parseDouble(line.substring(4, 18).trim())),
SP3Utils.VELOCITY_UNIT.toSI(Double.parseDouble(line.substring(18, 32).trim())),
SP3Utils.VELOCITY_UNIT.toSI(Double.parseDouble(line.substring(32, 46).trim())));
// clock rate in file is 1e-4 us / s
final double clockRateChange = SP3Utils.CLOCK_RATE_UNIT.toSI(line.trim().length() <= 46 ?
SP3Utils.DEFAULT_CLOCK_RATE_VALUE :
Double.parseDouble(line.substring(46, 60).trim()));
final Vector3D velocityAccuracy;
if (line.length() < 69 ||
line.substring(61, 63).trim().length() == 0 ||
line.substring(64, 66).trim().length() == 0 ||
line.substring(67, 69).trim().length() == 0) {
velocityAccuracy = null;
} else {
velocityAccuracy = new Vector3D(SP3Utils.siAccuracy(SP3Utils.VELOCITY_ACCURACY_UNIT,
header.getPosVelBase(),
Integer.parseInt(line.substring(61, 63).trim())),
SP3Utils.siAccuracy(SP3Utils.VELOCITY_ACCURACY_UNIT,
header.getPosVelBase(),
Integer.parseInt(line.substring(64, 66).trim())),
SP3Utils.siAccuracy(SP3Utils.VELOCITY_ACCURACY_UNIT,
header.getPosVelBase(),
Integer.parseInt(line.substring(67, 69).trim())));
}
final double clockRateAccuracy;
if (line.length() < 73 || line.substring(70, 73).trim().length() == 0) {
clockRateAccuracy = Double.NaN;
} else {
clockRateAccuracy = SP3Utils.siAccuracy(SP3Utils.CLOCK_RATE_ACCURACY_UNIT,
header.getClockBase(),
Integer.parseInt(line.substring(70, 73).trim()));
}
final SP3Coordinate coord =
new SP3Coordinate(pi.latestEpoch,
pi.latestPosition, pi.latestPositionAccuracy,
velocity, velocityAccuracy,
pi.latestClock, pi.latestClockAccuracy,
clockRateChange, clockRateAccuracy,
pi.latestClockEvent, pi.latestClockPrediction,
pi.latestOrbitManeuverEvent, pi.latestOrbitPrediction);
pi.file.getEphemeris(satelliteId).addCoordinate(coord, header.getEpochInterval());
}
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Arrays.asList(DATA_EPOCH, DATA_POSITION, DATA_VELOCITY_CORRELATION, EOF);
}
},
/** Parser for velocity correlation. */
DATA_VELOCITY_CORRELATION("^EV.*") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
// ignored for now
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Arrays.asList(DATA_EPOCH, DATA_POSITION, EOF);
}
},
/** Parser for End Of File marker. */
EOF("^[eE][oO][fF]\\s*$") {
/** {@inheritDoc} */
@Override
public void parse(final String line, final ParseInfo pi) {
pi.done = true;
}
/** {@inheritDoc} */
@Override
public Iterable<LineParser> allowedNext() {
return Collections.singleton(EOF);
}
};
/** Pattern for identifying line. */
private final Pattern pattern;
/** Simple constructor.
* @param lineRegexp regular expression for identifying line
*/
LineParser(final String lineRegexp) {
pattern = Pattern.compile(lineRegexp);
}
/** Parse a line.
* @param line line to parse
* @param pi holder for transient data
*/
public abstract void parse(String line, ParseInfo pi);
/** Get the allowed parsers for next line.
* @return allowed parsers for next line
*/
public abstract Iterable<LineParser> allowedNext();
/** Check if parser can handle line.
* @param line line to parse
* @return true if parser can handle the specified line
*/
public boolean canHandle(final String line) {
return pattern.matcher(line).matches();
}
}
}