DSSTSolarRadiationPressure.java
/* Copyright 2002-2018 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
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*/
package org.orekit.propagation.semianalytical.dsst.forces;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.hipparchus.util.FastMath;
import org.hipparchus.util.MathUtils;
import org.hipparchus.util.Precision;
import org.orekit.errors.OrekitException;
import org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient;
import org.orekit.forces.radiation.RadiationSensitive;
import org.orekit.forces.radiation.SolarRadiationPressure;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.events.EventDetector;
import org.orekit.utils.ExtendedPVCoordinatesProvider;
import org.orekit.utils.PVCoordinatesProvider;
/** Solar radiation pressure contribution to the
* {@link org.orekit.propagation.semianalytical.dsst.DSSTPropagator DSSTPropagator}.
* <p>
* The solar radiation pressure acceleration is computed through the
* acceleration model of
* {@link org.orekit.forces.radiation.SolarRadiationPressure SolarRadiationPressure}.
* </p>
*
* @author Pascal Parraud
*/
public class DSSTSolarRadiationPressure extends AbstractGaussianContribution {
/** Reference distance for the solar radiation pressure (m). */
private static final double D_REF = 149597870000.0;
/** Reference solar radiation pressure at D_REF (N/m²). */
private static final double P_REF = 4.56e-6;
/** Threshold for the choice of the Gauss quadrature order. */
private static final double GAUSS_THRESHOLD = 1.0e-15;
/** Threshold for shadow equation. */
private static final double S_ZERO = 1.0e-6;
/** Prefix for the coefficient keys. */
private static final String PREFIX = "DSST-SRP-";
/** Sun model. */
private final PVCoordinatesProvider sun;
/** Central Body radius. */
private final double ae;
/** Spacecraft model for radiation acceleration computation. */
private final RadiationSensitive spacecraft;
/**
* Simple constructor with default reference values and spherical spacecraft.
* <p>
* When this constructor is used, the reference values are:
* </p>
* <ul>
* <li>d<sub>ref</sub> = 149597870000.0 m</li>
* <li>p<sub>ref</sub> = 4.56 10<sup>-6</sup> N/m²</li>
* </ul>
* <p>
* The spacecraft has a spherical shape.
* </p>
*
* @param cr satellite radiation pressure coefficient (assuming total specular reflection)
* @param area cross sectional area of satellite
* @param sun Sun model
* @param equatorialRadius central body equatorial radius (for shadow computation)
* @deprecated as of 9.2 replaced by {@link #DSSTSolarRadiationPressure(double, double,
* ExtendedPVCoordinatesProvider, double)}
*/
@Deprecated
public DSSTSolarRadiationPressure(final double cr, final double area,
final PVCoordinatesProvider sun,
final double equatorialRadius) {
this(D_REF, P_REF, cr, area, sun, equatorialRadius);
}
/**
* Simple constructor with default reference values and spherical spacecraft.
* <p>
* When this constructor is used, the reference values are:
* </p>
* <ul>
* <li>d<sub>ref</sub> = 149597870000.0 m</li>
* <li>p<sub>ref</sub> = 4.56 10<sup>-6</sup> N/m²</li>
* </ul>
* <p>
* The spacecraft has a spherical shape.
* </p>
*
* @param cr satellite radiation pressure coefficient (assuming total specular reflection)
* @param area cross sectional area of satellite
* @param sun Sun model
* @param equatorialRadius central body equatorial radius (for shadow computation)
* @since 9.2
*/
public DSSTSolarRadiationPressure(final double cr, final double area,
final ExtendedPVCoordinatesProvider sun,
final double equatorialRadius) {
this(D_REF, P_REF, cr, area, sun, equatorialRadius);
}
/**
* Simple constructor with default reference values, but custom spacecraft.
* <p>
* When this constructor is used, the reference values are:
* </p>
* <ul>
* <li>d<sub>ref</sub> = 149597870000.0 m</li>
* <li>p<sub>ref</sub> = 4.56 10<sup>-6</sup> N/m²</li>
* </ul>
*
* @param sun Sun model
* @param equatorialRadius central body equatorial radius (for shadow computation)
* @param spacecraft spacecraft model
* @deprecated as of 9.2 replaced by {{@link #DSSTSolarRadiationPressure(ExtendedPVCoordinatesProvider,
* double, RadiationSensitive)}
*/
public DSSTSolarRadiationPressure(final PVCoordinatesProvider sun,
final double equatorialRadius,
final RadiationSensitive spacecraft) {
this(D_REF, P_REF, sun, equatorialRadius, spacecraft);
}
/**
* Simple constructor with default reference values, but custom spacecraft.
* <p>
* When this constructor is used, the reference values are:
* </p>
* <ul>
* <li>d<sub>ref</sub> = 149597870000.0 m</li>
* <li>p<sub>ref</sub> = 4.56 10<sup>-6</sup> N/m²</li>
* </ul>
*
* @param sun Sun model
* @param equatorialRadius central body equatorial radius (for shadow computation)
* @param spacecraft spacecraft model
* @since 9.2
*/
public DSSTSolarRadiationPressure(final ExtendedPVCoordinatesProvider sun,
final double equatorialRadius,
final RadiationSensitive spacecraft) {
this(D_REF, P_REF, sun, equatorialRadius, spacecraft);
}
/**
* Constructor with customizable reference values but spherical spacecraft.
* <p>
* Note that reference solar radiation pressure <code>pRef</code> in N/m² is linked
* to solar flux SF in W/m² using formula pRef = SF/c where c is the speed of light
* (299792458 m/s). So at 1UA a 1367 W/m² solar flux is a 4.56 10<sup>-6</sup>
* N/m² solar radiation pressure.
* </p>
*
* @param dRef reference distance for the solar radiation pressure (m)
* @param pRef reference solar radiation pressure at dRef (N/m²)
* @param cr satellite radiation pressure coefficient (assuming total specular reflection)
* @param area cross sectional area of satellite
* @param sun Sun model
* @param equatorialRadius central body equatorial radius (for shadow computation)
* @deprecated as of 9.2 replaced by {@link #DSSTSolarRadiationPressure(double, double,
* double, double, ExtendedPVCoordinatesProvider, double)
*/
@Deprecated
public DSSTSolarRadiationPressure(final double dRef, final double pRef,
final double cr, final double area,
final PVCoordinatesProvider sun,
final double equatorialRadius) {
// cR being the DSST SRP coef and assuming a spherical spacecraft,
// the conversion is:
// cR = 1 + (1 - kA) * (1 - kR) * 4 / 9
// with kA arbitrary sets to 0
this(dRef, pRef, sun, equatorialRadius, new IsotropicRadiationSingleCoefficient(area, cr));
}
/**
* Constructor with customizable reference values but spherical spacecraft.
* <p>
* Note that reference solar radiation pressure <code>pRef</code> in N/m² is linked
* to solar flux SF in W/m² using formula pRef = SF/c where c is the speed of light
* (299792458 m/s). So at 1UA a 1367 W/m² solar flux is a 4.56 10<sup>-6</sup>
* N/m² solar radiation pressure.
* </p>
*
* @param dRef reference distance for the solar radiation pressure (m)
* @param pRef reference solar radiation pressure at dRef (N/m²)
* @param cr satellite radiation pressure coefficient (assuming total specular reflection)
* @param area cross sectional area of satellite
* @param sun Sun model
* @param equatorialRadius central body equatorial radius (for shadow computation)
* @since 9.2
*/
public DSSTSolarRadiationPressure(final double dRef, final double pRef,
final double cr, final double area,
final ExtendedPVCoordinatesProvider sun,
final double equatorialRadius) {
// cR being the DSST SRP coef and assuming a spherical spacecraft,
// the conversion is:
// cR = 1 + (1 - kA) * (1 - kR) * 4 / 9
// with kA arbitrary sets to 0
this(dRef, pRef, sun, equatorialRadius, new IsotropicRadiationSingleCoefficient(area, cr));
}
/**
* Complete constructor.
* <p>
* Note that reference solar radiation pressure <code>pRef</code> in N/m² is linked
* to solar flux SF in W/m² using formula pRef = SF/c where c is the speed of light
* (299792458 m/s). So at 1UA a 1367 W/m² solar flux is a 4.56 10<sup>-6</sup>
* N/m² solar radiation pressure.
* </p>
*
* @param dRef reference distance for the solar radiation pressure (m)
* @param pRef reference solar radiation pressure at dRef (N/m²)
* @param sun Sun model
* @param equatorialRadius central body equatorial radius (for shadow computation)
* @param spacecraft spacecraft model
* @deprecated as of 9.2 replaced by {@link #DSSTSolarRadiationPressure(double, double,
* ExtendedPVCoordinatesProvider, double, RadiationSensitive)
*/
@Deprecated
public DSSTSolarRadiationPressure(final double dRef, final double pRef,
final PVCoordinatesProvider sun, final double equatorialRadius,
final RadiationSensitive spacecraft) {
//Call to the constructor from superclass using the numerical SRP model as ForceModel
super(PREFIX, GAUSS_THRESHOLD,
new SolarRadiationPressure(dRef, pRef, sun, equatorialRadius, spacecraft));
this.sun = sun;
this.ae = equatorialRadius;
this.spacecraft = spacecraft;
}
/**
* Complete constructor.
* <p>
* Note that reference solar radiation pressure <code>pRef</code> in N/m² is linked
* to solar flux SF in W/m² using formula pRef = SF/c where c is the speed of light
* (299792458 m/s). So at 1UA a 1367 W/m² solar flux is a 4.56 10<sup>-6</sup>
* N/m² solar radiation pressure.
* </p>
*
* @param dRef reference distance for the solar radiation pressure (m)
* @param pRef reference solar radiation pressure at dRef (N/m²)
* @param sun Sun model
* @param equatorialRadius central body equatorial radius (for shadow computation)
* @param spacecraft spacecraft model
* @since 9.2
*/
public DSSTSolarRadiationPressure(final double dRef, final double pRef,
final ExtendedPVCoordinatesProvider sun,
final double equatorialRadius,
final RadiationSensitive spacecraft) {
//Call to the constructor from superclass using the numerical SRP model as ForceModel
super(PREFIX, GAUSS_THRESHOLD,
new SolarRadiationPressure(dRef, pRef, sun, equatorialRadius, spacecraft));
this.sun = sun;
this.ae = equatorialRadius;
this.spacecraft = spacecraft;
}
/** Get spacecraft shape.
* @return the spacecraft shape.
*/
public RadiationSensitive getSpacecraft() {
return spacecraft;
}
/** {@inheritDoc} */
public EventDetector[] getEventsDetectors() {
return null;
}
/** {@inheritDoc} */
protected double[] getLLimits(final SpacecraftState state) throws OrekitException {
// Default bounds without shadow [-PI, PI]
final double[] ll = {-FastMath.PI + MathUtils.normalizeAngle(state.getLv(), 0),
FastMath.PI + MathUtils.normalizeAngle(state.getLv(), 0)};
// Direction cosines of the Sun in the equinoctial frame
final Vector3D sunDir = sun.getPVCoordinates(state.getDate(), state.getFrame()).getPosition().normalize();
final double alpha = sunDir.dotProduct(f);
final double beta = sunDir.dotProduct(g);
final double gamma = sunDir.dotProduct(w);
// Compute limits only if the perigee is close enough from the central body to be in the shadow
if (FastMath.abs(gamma * a * (1. - ecc)) < ae) {
// Compute the coefficients of the quartic equation in cos(L) 3.5-(2)
final double bet2 = beta * beta;
final double h2 = h * h;
final double k2 = k * k;
final double m = ae / (a * B);
final double m2 = m * m;
final double m4 = m2 * m2;
final double bb = alpha * beta + m2 * h * k;
final double b2 = bb * bb;
final double cc = alpha * alpha - bet2 + m2 * (k2 - h2);
final double dd = 1. - bet2 - m2 * (1. + h2);
final double[] a = new double[5];
a[0] = 4. * b2 + cc * cc;
a[1] = 8. * bb * m2 * h + 4. * cc * m2 * k;
a[2] = -4. * b2 + 4. * m4 * h2 - 2. * cc * dd + 4. * m4 * k2;
a[3] = -8. * bb * m2 * h - 4. * dd * m2 * k;
a[4] = -4. * m4 * h2 + dd * dd;
// Compute the real roots of the quartic equation 3.5-2
final double[] roots = new double[4];
final int nbRoots = realQuarticRoots(a, roots);
if (nbRoots > 0) {
// Check for consistency
boolean entryFound = false;
boolean exitFound = false;
// Eliminate spurious roots
for (int i = 0; i < nbRoots; i++) {
final double cosL = roots[i];
final double sL = FastMath.sqrt((1. - cosL) * (1. + cosL));
// Check both angles: L and -L
for (int j = -1; j <= 1; j += 2) {
final double sinL = j * sL;
final double cPhi = alpha * cosL + beta * sinL;
// Is the angle on the shadow side of the central body (eq. 3.5-3) ?
if (cPhi < 0.) {
final double range = 1. + k * cosL + h * sinL;
final double S = 1. - m2 * range * range - cPhi * cPhi;
// Is the shadow equation 3.5-1 satisfied ?
if (FastMath.abs(S) < S_ZERO) {
// Is this the entry or exit angle ?
final double dSdL = m2 * range * (k * sinL - h * cosL) + cPhi * (alpha * sinL - beta * cosL);
if (dSdL > 0.) {
// Exit from shadow: 3.5-4
exitFound = true;
ll[0] = FastMath.atan2(sinL, cosL);
} else {
// Entry into shadow: 3.5-5
entryFound = true;
ll[1] = FastMath.atan2(sinL, cosL);
}
}
}
}
}
// Must be one entry and one exit or none
if (!(entryFound == exitFound)) {
// entry or exit found but not both ! In this case, consider there is no eclipse...
ll[0] = -FastMath.PI;
ll[1] = FastMath.PI;
}
// Quadrature between L at exit and L at entry so Lexit must be lower than Lentry
if (ll[0] > ll[1]) {
// Keep the angles between [-2PI, 2PI]
if (ll[1] < 0.) {
ll[1] += 2. * FastMath.PI;
} else {
ll[0] -= 2. * FastMath.PI;
}
}
}
}
return ll;
}
/** Get the central body equatorial radius.
* @return central body equatorial radius (m)
*/
public double getEquatorialRadius() {
return ae;
}
/**
* Compute the real roots of a quartic equation.
*
* <pre>
* a[0] * x⁴ + a[1] * x³ + a[2] * x² + a[3] * x + a[4] = 0.
* </pre>
*
* @param a the 5 coefficients
* @param y the real roots
* @return the number of real roots
*/
private int realQuarticRoots(final double[] a, final double[] y) {
/* Treat the degenerate quartic as cubic */
if (Precision.equals(a[0], 0.)) {
final double[] aa = new double[a.length - 1];
System.arraycopy(a, 1, aa, 0, aa.length);
return realCubicRoots(aa, y);
}
// Transform coefficients
final double b = a[1] / a[0];
final double c = a[2] / a[0];
final double d = a[3] / a[0];
final double e = a[4] / a[0];
final double bh = b * 0.5;
// Solve resolvant cubic
final double[] z3 = new double[3];
final int i3 = realCubicRoots(new double[] {1.0, -c, b * d - 4. * e, e * (4. * c - b * b) - d * d}, z3);
if (i3 == 0) {
return 0;
}
// Largest real root of resolvant cubic
final double z = z3[0];
// Compute auxiliary quantities
final double zh = z * 0.5;
final double p = FastMath.max(z + bh * bh - c, 0.);
final double q = FastMath.max(zh * zh - e, 0.);
final double r = bh * z - d;
final double pp = FastMath.sqrt(p);
final double qq = FastMath.copySign(FastMath.sqrt(q), r);
// Solve quadratic factors of quartic equation
final double[] y1 = new double[2];
final int n1 = realQuadraticRoots(new double[] {1.0, bh - pp, zh - qq}, y1);
final double[] y2 = new double[2];
final int n2 = realQuadraticRoots(new double[] {1.0, bh + pp, zh + qq}, y2);
if (n1 == 2) {
if (n2 == 2) {
y[0] = y1[0];
y[1] = y1[1];
y[2] = y2[0];
y[3] = y2[1];
return 4;
} else {
y[0] = y1[0];
y[1] = y1[1];
return 2;
}
} else {
if (n2 == 2) {
y[0] = y2[0];
y[1] = y2[1];
return 2;
} else {
return 0;
}
}
}
/**
* Compute the real roots of a cubic equation.
*
* <pre>
* a[0] * x³ + a[1] * x² + a[2] * x + a[3] = 0.
* </pre>
*
* @param a the 4 coefficients
* @param y the real roots sorted in descending order
* @return the number of real roots
*/
private int realCubicRoots(final double[] a, final double[] y) {
if (Precision.equals(a[0], 0.)) {
// Treat the degenerate cubic as quadratic
final double[] aa = new double[a.length - 1];
System.arraycopy(a, 1, aa, 0, aa.length);
return realQuadraticRoots(aa, y);
}
// Transform coefficients
final double b = -a[1] / (3. * a[0]);
final double c = a[2] / a[0];
final double d = a[3] / a[0];
final double b2 = b * b;
final double p = b2 - c / 3.;
final double q = b * (b2 - c * 0.5) - d * 0.5;
// Compute discriminant
final double disc = p * p * p - q * q;
if (disc < 0.) {
// One real root
final double alpha = q + FastMath.copySign(FastMath.sqrt(-disc), q);
final double cbrtAl = FastMath.cbrt(alpha);
final double cbrtBe = p / cbrtAl;
if (p < 0.) {
y[0] = b + 2. * q / (cbrtAl * cbrtAl + cbrtBe * cbrtBe - p);
} else if (p > 0.) {
y[0] = b + cbrtAl + cbrtBe;
} else {
y[0] = b + cbrtAl;
}
return 1;
} else if (disc > 0.) {
// Three distinct real roots
final double phi = FastMath.atan2(FastMath.sqrt(disc), q) / 3.;
final double sqP = 2.0 * FastMath.sqrt(p);
y[0] = b + sqP * FastMath.cos(phi);
y[1] = b - sqP * FastMath.cos(FastMath.PI / 3. + phi);
y[2] = b - sqP * FastMath.cos(FastMath.PI / 3. - phi);
return 3;
} else {
// One distinct and two equals real roots
final double cbrtQ = FastMath.cbrt(q);
final double root1 = b + 2. * cbrtQ;
final double root2 = b - cbrtQ;
if (q < 0.) {
y[0] = root2;
y[1] = root2;
y[2] = root1;
} else {
y[0] = root1;
y[1] = root2;
y[2] = root2;
}
return 3;
}
}
/**
* Compute the real roots of a quadratic equation.
*
* <pre>
* a[0] * x² + a[1] * x + a[2] = 0.
* </pre>
*
* @param a the 3 coefficients
* @param y the real roots sorted in descending order
* @return the number of real roots
*/
private int realQuadraticRoots(final double[] a, final double[] y) {
if (Precision.equals(a[0], 0.)) {
// Degenerate quadratic
if (Precision.equals(a[1], 0.)) {
// Degenerate linear equation: no real roots
return 0;
}
// Linear equation: one real root
y[0] = -a[2] / a[1];
return 1;
}
// Transform coefficients
final double b = -0.5 * a[1] / a[0];
final double c = a[2] / a[0];
// Compute discriminant
final double d = b * b - c;
if (d < 0.) {
// No real roots
return 0;
} else if (d > 0.) {
// Two distinct real roots
final double y0 = b + FastMath.copySign(FastMath.sqrt(d), b);
final double y1 = c / y0;
y[0] = FastMath.max(y0, y1);
y[1] = FastMath.min(y0, y1);
return 2;
} else {
// Discriminant is zero: two equal real roots
y[0] = b;
y[1] = b;
return 2;
}
}
}