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18 package org.orekit.estimation;
19
20 import org.hipparchus.geometry.euclidean.threed.Vector3D;
21 import org.hipparchus.util.FastMath;
22 import org.orekit.bodies.CelestialBody;
23 import org.orekit.bodies.GeodeticPoint;
24 import org.orekit.bodies.OneAxisEllipsoid;
25 import org.orekit.estimation.measurements.GroundStation;
26 import org.orekit.frames.TopocentricFrame;
27 import org.orekit.models.earth.displacement.StationDisplacement;
28 import org.orekit.models.earth.troposphere.TroposphericModelUtils;
29 import org.orekit.orbits.CartesianOrbit;
30 import org.orekit.orbits.Orbit;
31 import org.orekit.orbits.PositionAngleType;
32 import org.orekit.propagation.conversion.KeplerianPropagatorBuilder;
33 import org.orekit.time.TimeScale;
34 import org.orekit.time.UT1Scale;
35 import org.orekit.utils.IERSConventions;
36 import org.orekit.utils.PVCoordinates;
37
38 import java.util.List;
39
40 public class KeplerianContext implements StationDataProvider {
41
42 public IERSConventions conventions;
43 public OneAxisEllipsoid earth;
44 public CelestialBody sun;
45 public CelestialBody moon;
46 public TimeScale utc;
47 public UT1Scale ut1;
48 public Orbit initialOrbit;
49 public StationDisplacement[] displacements;
50 public List<GroundStation> stations;
51
52 public KeplerianPropagatorBuilder createBuilder(final PositionAngleType angleType, final boolean perfectStart, final double dP) {
53
54 final Orbit startOrbit;
55 if (perfectStart) {
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57 startOrbit = initialOrbit;
58 } else {
59
60 final Vector3D initialPosition = initialOrbit.getPosition();
61 final Vector3D initialVelocity = initialOrbit.getPVCoordinates().getVelocity();
62 final Vector3D wrongPosition = initialPosition.add(new Vector3D(1000.0, 0, 0));
63 final Vector3D wrongVelocity = initialVelocity.add(new Vector3D(0, 0, 0.01));
64 startOrbit = new CartesianOrbit(new PVCoordinates(wrongPosition, wrongVelocity),
65 initialOrbit.getFrame(),
66 initialOrbit.getDate(),
67 initialOrbit.getMu());
68 }
69
70
71 final KeplerianPropagatorBuilder propagatorBuilder =
72 new KeplerianPropagatorBuilder(startOrbit, angleType, dP);
73
74
75 return propagatorBuilder;
76
77 }
78
79 GroundStation createStation(double latitudeInDegrees, double longitudeInDegrees,
80 double altitude, String name) {
81 final GeodeticPoint gp = new GeodeticPoint(FastMath.toRadians(latitudeInDegrees),
82 FastMath.toRadians(longitudeInDegrees),
83 altitude);
84 return new GroundStation(new TopocentricFrame(earth, gp, name),
85 TroposphericModelUtils.STANDARD_ATMOSPHERE_PROVIDER,
86 ut1.getEOPHistory(), displacements);
87 }
88
89 @Override
90 public List<GroundStation> getStations() {
91 return stations;
92 }
93
94 }