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17 package org.orekit.estimation;
18
19 import java.util.List;
20 import java.util.Map;
21
22 import org.hipparchus.geometry.euclidean.threed.Vector3D;
23 import org.hipparchus.util.FastMath;
24 import org.orekit.bodies.CelestialBody;
25 import org.orekit.bodies.GeodeticPoint;
26 import org.orekit.bodies.OneAxisEllipsoid;
27 import org.orekit.estimation.measurements.GroundStation;
28 import org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider;
29 import org.orekit.frames.TopocentricFrame;
30 import org.orekit.models.earth.displacement.StationDisplacement;
31 import org.orekit.orbits.CartesianOrbit;
32 import org.orekit.orbits.Orbit;
33 import org.orekit.orbits.PositionAngle;
34 import org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder;
35 import org.orekit.time.TimeScale;
36 import org.orekit.time.UT1Scale;
37 import org.orekit.utils.IERSConventions;
38 import org.orekit.utils.PVCoordinates;
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 PositionAngle angleType, final boolean perfectStart, final double dP) {
58
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.getPVCoordinates().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 }
74
75
76 final EcksteinHechlerPropagatorBuilder propagatorBuilder =
77 new EcksteinHechlerPropagatorBuilder(startOrbit, gravity, angleType, dP);
78
79
80 return propagatorBuilder;
81
82 }
83
84 GroundStation createStation(double latitudeInDegrees, double longitudeInDegrees,
85 double altitude, String name) {
86 final GeodeticPoint gp = new GeodeticPoint(FastMath.toRadians(latitudeInDegrees),
87 FastMath.toRadians(longitudeInDegrees),
88 altitude);
89 return new GroundStation(new TopocentricFrame(earth, gp, name),
90 ut1.getEOPHistory(), displacements);
91 }
92
93 @Override
94 public List<GroundStation> getStations() {
95 return stations;
96 }
97
98 }