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17 package org.orekit.estimation;
18
19 import org.hipparchus.geometry.euclidean.threed.Vector3D;
20 import org.hipparchus.util.FastMath;
21 import org.orekit.bodies.CelestialBody;
22 import org.orekit.bodies.GeodeticPoint;
23 import org.orekit.bodies.OneAxisEllipsoid;
24 import org.orekit.estimation.measurements.GroundStation;
25 import org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider;
26 import org.orekit.frames.TopocentricFrame;
27 import org.orekit.models.earth.displacement.StationDisplacement;
28 import org.orekit.orbits.CartesianOrbit;
29 import org.orekit.orbits.Orbit;
30 import org.orekit.orbits.PositionAngleType;
31 import org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder;
32 import org.orekit.time.TimeScale;
33 import org.orekit.time.UT1Scale;
34 import org.orekit.utils.IERSConventions;
35 import org.orekit.utils.PVCoordinates;
36
37 import java.util.List;
38 import java.util.Map;
39
40 public class EcksteinHechlerContext implements StationDataProvider {
41
42 public IERSConventions conventions;
43 public OneAxisEllipsoid earth;
44 public CelestialBody sun;
45 public CelestialBody moon;
46 public UnnormalizedSphericalHarmonicsProvider gravity;
47 public TimeScale utc;
48 public UT1Scale ut1;
49 public Orbit initialOrbit;
50 public StationDisplacement[] displacements;
51 public List<GroundStation> stations;
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53
54
55 public Map<GroundStation, GroundStation> TARstations;
56
57 public EcksteinHechlerPropagatorBuilder createBuilder(final PositionAngleType angleType, final boolean perfectStart, final double dP) {
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59 final Orbit startOrbit;
60 if (perfectStart) {
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62 startOrbit = initialOrbit;
63 } else {
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65 final Vector3D initialPosition = initialOrbit.getPosition();
66 final Vector3D initialVelocity = initialOrbit.getPVCoordinates().getVelocity();
67 final Vector3D wrongPosition = initialPosition.add(new Vector3D(1000.0, 0, 0));
68 final Vector3D wrongVelocity = initialVelocity.add(new Vector3D(0, 0, 0.01));
69 startOrbit = new CartesianOrbit(new PVCoordinates(wrongPosition, wrongVelocity),
70 initialOrbit.getFrame(),
71 initialOrbit.getDate(),
72 initialOrbit.getMu());
73 }
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75
76 return new EcksteinHechlerPropagatorBuilder(startOrbit, gravity, angleType, dP);
77
78 }
79
80 GroundStation createStation(double latitudeInDegrees, double longitudeInDegrees,
81 double altitude, String name) {
82 final GeodeticPoint gp = new GeodeticPoint(FastMath.toRadians(latitudeInDegrees),
83 FastMath.toRadians(longitudeInDegrees),
84 altitude);
85 return new GroundStation(new TopocentricFrame(earth, gp, name), ut1.getEOPHistory(), displacements);
86 }
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88 @Override
89 public List<GroundStation> getStations() {
90 return stations;
91 }
92
93 }