From 8f78ad87d477f8b46be8fc510d9b91d958450c56 Mon Sep 17 00:00:00 2001
From: Guylaine Prat <guylaine.prat@c-s.fr>
Date: Thu, 11 Jan 2018 18:11:03 +0100
Subject: [PATCH] Remove useless method
---
.../refiningPleiades/models/OrbitModel.java | 34 -------------------
1 file changed, 34 deletions(-)
diff --git a/src/tutorials/java/fr/cs/examples/refiningPleiades/models/OrbitModel.java b/src/tutorials/java/fr/cs/examples/refiningPleiades/models/OrbitModel.java
index 1ab3b9fc..b207555c 100644
--- a/src/tutorials/java/fr/cs/examples/refiningPleiades/models/OrbitModel.java
+++ b/src/tutorials/java/fr/cs/examples/refiningPleiades/models/OrbitModel.java
@@ -250,40 +250,6 @@ public class OrbitModel {
}
}
- /** Create the orbit propagator.
- */
- public Propagator createPropagator(final BodyShape earth,
- final NormalizedSphericalHarmonicsProvider gravityField,
- final Orbit orbit)
- throws OrekitException {
-
- final AttitudeProvider attitudeProvider = createAttitudeProvider(earth, orbit);
-
- final SpacecraftState state =
- new SpacecraftState(orbit,
- attitudeProvider.getAttitude(orbit, orbit.getDate(), orbit.getFrame()), 1180.0);
-
- // numerical model for improving orbit
- final OrbitType type = OrbitType.CIRCULAR;
- final double[][] tolerances = NumericalPropagator.tolerances(0.1, orbit, type);
- final DormandPrince853Integrator integrator =
- new DormandPrince853Integrator(1.0e-4 * orbit.getKeplerianPeriod(),
- 1.0e-1 * orbit.getKeplerianPeriod(),
- tolerances[0],
- tolerances[1]);
- integrator.setInitialStepSize(1.0e-2 * orbit.getKeplerianPeriod());
-
- final NumericalPropagator numericalPropagator = new NumericalPropagator(integrator);
- numericalPropagator.addForceModel(new HolmesFeatherstoneAttractionModel(earth.getBodyFrame(), gravityField));
- numericalPropagator .addForceModel(new ThirdBodyAttraction(CelestialBodyFactory.getSun()));
- numericalPropagator .addForceModel(new ThirdBodyAttraction(CelestialBodyFactory.getMoon()));
- numericalPropagator.setOrbitType(type);
- numericalPropagator.setInitialState(state);
- numericalPropagator.setAttitudeProvider(attitudeProvider);
-
- return numericalPropagator;
- }
-
/** Generate the orbit.
*/
public List<TimeStampedPVCoordinates> orbitToPV(final Orbit orbit, final BodyShape earth,
--
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