GroundStation.java
/* Copyright 2002-2017 CS Systèmes d'Information
* Licensed to CS Systèmes d'Information (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.estimation.measurements;
import java.util.Map;
import org.hipparchus.Field;
import org.hipparchus.analysis.differentiation.DSFactory;
import org.hipparchus.analysis.differentiation.DerivativeStructure;
import org.hipparchus.geometry.euclidean.threed.FieldRotation;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.orekit.bodies.BodyShape;
import org.orekit.bodies.FieldGeodeticPoint;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.bodies.OneAxisEllipsoid;
import org.orekit.data.BodiesElements;
import org.orekit.data.FundamentalNutationArguments;
import org.orekit.errors.OrekitException;
import org.orekit.errors.OrekitExceptionWrapper;
import org.orekit.errors.OrekitMessages;
import org.orekit.frames.EOPHistory;
import org.orekit.frames.FieldTransform;
import org.orekit.frames.Frame;
import org.orekit.frames.FramesFactory;
import org.orekit.frames.TopocentricFrame;
import org.orekit.frames.Transform;
import org.orekit.models.earth.displacement.StationDisplacement;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.FieldAbsoluteDate;
import org.orekit.time.TimeScalesFactory;
import org.orekit.time.UT1Scale;
import org.orekit.utils.ParameterDriver;
/** Class modeling a ground station that can perform some measurements.
* <p>
* This class adds a position offset parameter to a base {@link TopocentricFrame
* topocentric frame}.
* </p>
* <p>
* Since 9.0, this class also adds parameters for an additional polar motion
* and an additional prime meridian orientation. Since these parameters will
* have the same name for all ground stations, they will be managed consistently
* and allow to estimate Earth orientation precisely (this is needed for precise
* orbit determination). The polar motion and prime meridian orientation will
* be applied <em>after</em> regular Earth orientation parameters, so the value
* of the estimated parameters will be correction to EOP, they will not be the
* complete EOP values by themselves. Basically, this means that for Earth, the
* following transforms are applied in order, between inertial frame and ground
* station frame (for non-Earth based ground stations, different precession nutation
* models and associated planet oritentation parameters would be applied, if available):
* </p>
* <ol>
* <li>precession/nutation, as theoretical model plus celestial pole EOP parameters</li>
* <li>body rotation, as theoretical model plus prime meridian EOP parameters</li>
* <li>polar motion, which is only from EOP parameters (no theoretical models)</li>
* <li>additional body rotation, controlled by {@link #getPrimeMeridianOffsetDriver()} and {@link #getPrimeMeridianDriftDriver()}</li>
* <li>additional polar motion, controlled by {@link #getPolarOffsetXDriver()}, {@link #getPolarDriftXDriver()},
* {@link #getPolarOffsetYDriver()} and {@link #getPolarDriftYDriver()}</li>
* <li>station position offset, controlled by {@link #getEastOffsetDriver()},
* {@link #getNorthOffsetDriver()} and {@link #getZenithOffsetDriver()}</li>
* </ol>
* @author Luc Maisonobe
* @since 8.0
*/
public class GroundStation {
/** Suffix for ground station position offset parameter name. */
public static final String OFFSET_SUFFIX = "-offset";
/** Suffix for ground station intermediate frame name. */
public static final String INTERMEDIATE_SUFFIX = "-intermediate";
/** Offsets scaling factor.
* <p>
* We use a power of 2 (in fact really 1.0 here) to avoid numeric noise introduction
* in the multiplications/divisions sequences.
* </p>
*/
private static final double OFFSET_SCALE = FastMath.scalb(1.0, 0);
/** Provider for Earth frame whose EOP parameters can be estimated. */
private final EstimatedEarthFrameProvider estimatedEarthFrameProvider;
/** Earth frame whose EOP parameters can be estimated. */
private final Frame estimatedEarthFrame;
/** Base frame associated with the station. */
private final TopocentricFrame baseFrame;
/** Fundamental nutation arguments. */
private final FundamentalNutationArguments arguments;
/** Displacement models. */
private final StationDisplacement[] displacements;
/** Driver for position offset along the East axis. */
private final ParameterDriver eastOffsetDriver;
/** Driver for position offset along the North axis. */
private final ParameterDriver northOffsetDriver;
/** Driver for position offset along the zenith axis. */
private final ParameterDriver zenithOffsetDriver;
/** Build a ground station ignoring {@link StationDisplacement station displacements}.
* <p>
* The initial values for the pole and prime meridian parametric linear models
* ({@link #getPrimeMeridianOffsetDriver()}, {@link #getPrimeMeridianDriftDriver()},
* {@link #getPolarOffsetXDriver()}, {@link #getPolarDriftXDriver()},
* {@link #getPolarOffsetXDriver()}, {@link #getPolarDriftXDriver()}) are set to 0.
* The initial values for the station offset model ({@link #getEastOffsetDriver()},
* {@link #getNorthOffsetDriver()}, {@link #getZenithOffsetDriver()}) are set to 0.
* This implies that as long as these values are not changed, the offset frame is
* the same as the {@link #getBaseFrame() base frame}. As soon as some of these models
* are changed, the offset frame moves away from the {@link #getBaseFrame() base frame}.
* </p>
* @param baseFrame base frame associated with the station, without *any* parametric
* model (no station offset, no polar motion, no meridian shift)
* @exception OrekitException if some frame transforms cannot be computed
* or if Earth Orientation Parameters cannot be retrieved from the base frame.
* @see #GroundStation(TopocentricFrame, EOPHistory, StationDisplacement...)
*/
public GroundStation(final TopocentricFrame baseFrame)
throws OrekitException {
this(baseFrame, FramesFactory.findEOP(baseFrame), new StationDisplacement[0]);
}
/** Simple constructor.
* <p>
* The initial values for the pole and prime meridian parametric linear models
* ({@link #getPrimeMeridianOffsetDriver()}, {@link #getPrimeMeridianDriftDriver()},
* {@link #getPolarOffsetXDriver()}, {@link #getPolarDriftXDriver()},
* {@link #getPolarOffsetXDriver()}, {@link #getPolarDriftXDriver()}) are set to 0.
* The initial values for the station offset model ({@link #getEastOffsetDriver()},
* {@link #getNorthOffsetDriver()}, {@link #getZenithOffsetDriver()}) are set to 0.
* This implies that as long as these values are not changed, the offset frame is
* the same as the {@link #getBaseFrame() base frame}. As soon as some of these models
* are changed, the offset frame moves away from the {@link #getBaseFrame() base frame}.
* </p>
* @param baseFrame base frame associated with the station, without *any* parametric
* model (no station offset, no polar motion, no meridian shift)
* @param eopHistory EOP history associated with Earth frames
* @param displacements ground station displacement model (tides, ocean loading,
* atmospheric loading, thermal effects...)
* @exception OrekitException if some frame transforms cannot be computed
* or if the ground station is not defined on a {@link OneAxisEllipsoid ellipsoid}.
* @since 9.1
*/
public GroundStation(final TopocentricFrame baseFrame, final EOPHistory eopHistory,
final StationDisplacement... displacements)
throws OrekitException {
this.baseFrame = baseFrame;
if (eopHistory == null) {
throw new OrekitException(OrekitMessages.NO_EARTH_ORIENTATION_PARAMETERS);
}
final UT1Scale baseUT1 = TimeScalesFactory.getUT1(eopHistory);
this.estimatedEarthFrameProvider = new EstimatedEarthFrameProvider(baseUT1);
this.estimatedEarthFrame = new Frame(baseFrame.getParent(), estimatedEarthFrameProvider,
baseFrame.getParent() + "-estimated");
if (displacements.length == 0) {
arguments = null;
} else {
arguments = eopHistory.getConventions().getNutationArguments(estimatedEarthFrameProvider.getEstimatedUT1());
}
this.displacements = displacements.clone();
this.eastOffsetDriver = new ParameterDriver(baseFrame.getName() + OFFSET_SUFFIX + "-East",
0.0, OFFSET_SCALE,
Double.NEGATIVE_INFINITY, Double.POSITIVE_INFINITY);
this.northOffsetDriver = new ParameterDriver(baseFrame.getName() + OFFSET_SUFFIX + "-North",
0.0, OFFSET_SCALE,
Double.NEGATIVE_INFINITY, Double.POSITIVE_INFINITY);
this.zenithOffsetDriver = new ParameterDriver(baseFrame.getName() + OFFSET_SUFFIX + "-Zenith",
0.0, OFFSET_SCALE,
Double.NEGATIVE_INFINITY, Double.POSITIVE_INFINITY);
}
/** Get the displacement models.
* @return displacement models (empty if no model has been set up)
* @since 9.1
*/
public StationDisplacement[] getDisplacements() {
return displacements.clone();
}
/** Get a driver allowing to change station position along East axis.
* @return driver for station position offset along East axis
*/
public ParameterDriver getEastOffsetDriver() {
return eastOffsetDriver;
}
/** Get a driver allowing to change station position along North axis.
* @return driver for station position offset along North axis
*/
public ParameterDriver getNorthOffsetDriver() {
return northOffsetDriver;
}
/** Get a driver allowing to change station position along Zenith axis.
* @return driver for station position offset along Zenith axis
*/
public ParameterDriver getZenithOffsetDriver() {
return zenithOffsetDriver;
}
/** Get a driver allowing to add a prime meridian rotation.
* <p>
* The parameter is an angle in radians. In order to convert this
* value to a DUT1 in seconds, the value must be divided by
* {@code ave = 7.292115146706979e-5} (which is the nominal Angular Velocity
* of Earth from the TIRF model).
* </p>
* @return driver for prime meridian rotation
*/
public ParameterDriver getPrimeMeridianOffsetDriver() {
return estimatedEarthFrameProvider.getPrimeMeridianOffsetDriver();
}
/** Get a driver allowing to add a prime meridian rotation rate.
* <p>
* The parameter is an angle rate in radians per second. In order to convert this
* value to a LOD in seconds, the value must be multiplied by -86400 and divided by
* {@code ave = 7.292115146706979e-5} (which is the nominal Angular Velocity
* of Earth from the TIRF model).
* </p>
* @return driver for prime meridian rotation rate
*/
public ParameterDriver getPrimeMeridianDriftDriver() {
return estimatedEarthFrameProvider.getPrimeMeridianDriftDriver();
}
/** Get a driver allowing to add a polar offset along X.
* <p>
* The parameter is an angle in radians
* </p>
* @return driver for polar offset along X
*/
public ParameterDriver getPolarOffsetXDriver() {
return estimatedEarthFrameProvider.getPolarOffsetXDriver();
}
/** Get a driver allowing to add a polar drift along X.
* <p>
* The parameter is an angle rate in radians per second
* </p>
* @return driver for polar drift along X
*/
public ParameterDriver getPolarDriftXDriver() {
return estimatedEarthFrameProvider.getPolarDriftXDriver();
}
/** Get a driver allowing to add a polar offset along Y.
* <p>
* The parameter is an angle in radians
* </p>
* @return driver for polar offset along Y
*/
public ParameterDriver getPolarOffsetYDriver() {
return estimatedEarthFrameProvider.getPolarOffsetYDriver();
}
/** Get a driver allowing to add a polar drift along Y.
* <p>
* The parameter is an angle rate in radians per second
* </p>
* @return driver for polar drift along Y
*/
public ParameterDriver getPolarDriftYDriver() {
return estimatedEarthFrameProvider.getPolarDriftYDriver();
}
/** Get the base frame associated with the station.
* <p>
* The base frame corresponds to a null position offset, null
* polar motion, null meridian shift
* </p>
* @return base frame associated with the station
*/
public TopocentricFrame getBaseFrame() {
return baseFrame;
}
/** Get the estimated Earth frame, including the estimated linear models for pole and prime meridian.
* <p>
* This frame is bound to the {@link #getPrimeMeridianOffsetDriver() driver for prime meridian offset},
* {@link #getPrimeMeridianDriftDriver() driver prime meridian drift},
* {@link #getPolarOffsetXDriver() driver for polar offset along X},
* {@link #getPolarDriftXDriver() driver for polar drift along X},
* {@link #getPolarOffsetYDriver() driver for polar offset along Y},
* {@link #getPolarDriftYDriver() driver for polar drift along Y}, so its orientation changes when
* the {@link ParameterDriver#setValue(double) setValue} methods of the drivers are called.
* </p>
* @return estimated Earth frame
* @since 9.1
*/
public Frame getEstimatedEarthFrame() {
return estimatedEarthFrame;
}
/** Get the estimated UT1 scale, including the estimated linear models for prime meridian.
* <p>
* This time scale is bound to the {@link #getPrimeMeridianOffsetDriver() driver for prime meridian offset},
* and {@link #getPrimeMeridianDriftDriver() driver prime meridian drift}, so its offset from UTC changes when
* the {@link ParameterDriver#setValue(double) setValue} methods of the drivers are called.
* </p>
* @return estimated Earth frame
* @since 9.1
*/
public UT1Scale getEstimatedUT1() {
return estimatedEarthFrameProvider.getEstimatedUT1();
}
/** Get the geodetic point at the center of the offset frame.
* @return geodetic point at the center of the offset frame
* @exception OrekitException if frames transforms cannot be computed
* @deprecated as of 9.1, replaced by {@link #getOffsetGeodeticPoint(AbsoluteDate)}
*/
@Deprecated
public GeodeticPoint getOffsetGeodeticPoint()
throws OrekitException {
return getOffsetGeodeticPoint(null);
}
/** Get the station displacement.
* @param date current date
* @param position raw position of the station in Earth frame
* before displacement is applied
* @return station displacement
* @exception OrekitException if displacement cannot be computed
* @since 9.1
*/
private Vector3D computeDisplacement(final AbsoluteDate date, final Vector3D position)
throws OrekitException {
try {
Vector3D displacement = Vector3D.ZERO;
if (arguments != null) {
final BodiesElements elements = arguments.evaluateAll(date);
for (final StationDisplacement sd : displacements) {
// we consider all displacements apply to the same initial position,
// i.e. they apply simultaneously, not according to some order
displacement = displacement.add(sd.displacement(elements, estimatedEarthFrame, position));
}
}
return displacement;
} catch (OrekitExceptionWrapper oew) {
throw oew.getException();
}
}
/** Get the geodetic point at the center of the offset frame.
* @param date current date (may be null if displacements are ignored)
* @return geodetic point at the center of the offset frame
* @exception OrekitException if frames transforms cannot be computed
* @since 9.1
*/
public GeodeticPoint getOffsetGeodeticPoint(final AbsoluteDate date)
throws OrekitException {
// take station offset into account
final double x = parametricModel(eastOffsetDriver);
final double y = parametricModel(northOffsetDriver);
final double z = parametricModel(zenithOffsetDriver);
final BodyShape baseShape = baseFrame.getParentShape();
final Transform baseToBody = baseFrame.getTransformTo(baseShape.getBodyFrame(), date);
Vector3D origin = baseToBody.transformPosition(new Vector3D(x, y, z));
if (date != null) {
origin = origin.add(computeDisplacement(date, origin));
}
return baseShape.transform(origin, baseShape.getBodyFrame(), null);
}
/** Get the transform between offset frame and inertial frame.
* <p>
* The offset frame takes the <em>current</em> position offset,
* polar motion and the meridian shift into account. The frame
* returned is disconnected from later changes in the parameters.
* When the {@link ParameterDriver parameters} managing these
* offsets are changed, the method must be called again to retrieve
* a new offset frame.
* </p>
* @param inertial inertial frame to transform to
* @param date date of the transform
* @return offset frame defining vectors
* @exception OrekitException if offset frame cannot be computed for current offset values
*/
public Transform getOffsetToInertial(final Frame inertial, final AbsoluteDate date)
throws OrekitException {
// take Earth offsets into account
final Transform intermediateToBody = estimatedEarthFrameProvider.getTransform(date).getInverse();
// take station offset into account
final double x = parametricModel(eastOffsetDriver);
final double y = parametricModel(northOffsetDriver);
final double z = parametricModel(zenithOffsetDriver);
final BodyShape baseShape = baseFrame.getParentShape();
final Transform baseToBody = baseFrame.getTransformTo(baseShape.getBodyFrame(), date);
Vector3D origin = baseToBody.transformPosition(new Vector3D(x, y, z));
origin = origin.add(computeDisplacement(date, origin));
final GeodeticPoint originGP = baseShape.transform(origin, baseShape.getBodyFrame(), date);
final Transform offsetToIntermediate =
new Transform(date,
new Transform(date,
new Rotation(Vector3D.PLUS_I, Vector3D.PLUS_K,
originGP.getEast(), originGP.getZenith()),
Vector3D.ZERO),
new Transform(date, origin));
// combine all transforms together
final Transform bodyToInert = baseFrame.getParent().getTransformTo(inertial, date);
return new Transform(date, offsetToIntermediate, new Transform(date, intermediateToBody, bodyToInert));
}
/** Get the transform between offset frame and inertial frame with derivatives.
* <p>
* As the East and North vector are not well defined at pole, the derivatives
* of these two vectors diverge to infinity as we get closer to the pole.
* So this method should not be used for stations less than 0.0001 degree from
* either poles.
* </p>
* @param inertial inertial frame to transform to
* @param date date of the transform
* @param factory factory for the derivatives
* @param indices indices of the estimated parameters in derivatives computations
* @return offset frame defining vectors with derivatives
* @exception OrekitException if some frame transforms cannot be computed
* @since 9.0
*/
public FieldTransform<DerivativeStructure> getOffsetToInertial(final Frame inertial,
final FieldAbsoluteDate<DerivativeStructure> date,
final DSFactory factory,
final Map<String, Integer> indices)
throws OrekitException {
final Field<DerivativeStructure> field = date.getField();
final FieldVector3D<DerivativeStructure> zero = FieldVector3D.getZero(field);
final FieldVector3D<DerivativeStructure> plusI = FieldVector3D.getPlusI(field);
final FieldVector3D<DerivativeStructure> plusK = FieldVector3D.getPlusK(field);
// take Earth offsets into account
final FieldTransform<DerivativeStructure> intermediateToBody =
estimatedEarthFrameProvider.getTransform(date, factory, indices).getInverse();
// take station offset into account
final DerivativeStructure x = parametricModel(factory, eastOffsetDriver, indices);
final DerivativeStructure y = parametricModel(factory, northOffsetDriver, indices);
final DerivativeStructure z = parametricModel(factory, zenithOffsetDriver, indices);
final BodyShape baseShape = baseFrame.getParentShape();
final Transform baseToBody = baseFrame.getTransformTo(baseShape.getBodyFrame(), (AbsoluteDate) null);
FieldVector3D<DerivativeStructure> origin = baseToBody.transformPosition(new FieldVector3D<>(x, y, z));
origin = origin.add(computeDisplacement(date.toAbsoluteDate(), origin.toVector3D()));
final FieldGeodeticPoint<DerivativeStructure> originGP = baseShape.transform(origin, baseShape.getBodyFrame(), date);
final FieldTransform<DerivativeStructure> offsetToIntermediate =
new FieldTransform<>(date,
new FieldTransform<>(date,
new FieldRotation<>(plusI, plusK,
originGP.getEast(), originGP.getZenith()),
zero),
new FieldTransform<>(date, origin));
// combine all transforms together
final FieldTransform<DerivativeStructure> bodyToInert = baseFrame.getParent().getTransformTo(inertial, date);
return new FieldTransform<>(date,
offsetToIntermediate,
new FieldTransform<>(date, intermediateToBody, bodyToInert));
}
/** Evaluate a parametric model.
* @param driver driver managing the parameter
* @return value of the parametric model
*/
private double parametricModel(final ParameterDriver driver) {
return driver.getValue();
}
/** Evaluate a parametric model.
* @param factory factory for the derivatives
* @param driver driver managing the parameter
* @param indices indices of the estimated parameters in derivatives computations
* @return value of the parametric model
*/
private DerivativeStructure parametricModel(final DSFactory factory, final ParameterDriver driver,
final Map<String, Integer> indices) {
final Integer index = indices.get(driver.getName());
return (index == null) ?
factory.constant(driver.getValue()) :
factory.variable(index, driver.getValue());
}
}