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Commit a02642c2 authored by Xavier Gibert's avatar Xavier Gibert
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Bugfix orbit model give correct values of omega and raan

parent e7aadbde
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......@@ -6,6 +6,7 @@ import org.orekit.attitudes.Attitude;
import org.orekit.bodies.CelestialBodyFactory;
import org.orekit.errors.OrekitException;
import org.orekit.frames.Frame;
import org.orekit.orbits.KeplerianOrbit;
import org.orekit.propagation.SpacecraftState;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.TimeScale;
......@@ -230,8 +231,6 @@ public class ModelSimulation {
//TODO
new_state.value_earth_rotation = new Quat();
new_state.value_orbit_w = Math.PI;
new_state.value_orbit_raan = 0;
//XGGDEBUG: correct values
Vector3D spacecraft = scs.getPVCoordinates().getPosition();
......@@ -242,8 +241,9 @@ public class ModelSimulation {
new_state.value_orbit_a = scs.getA();
new_state.value_orbit_e = scs.getE();
new_state.value_orbit_i = scs.getI();
KeplerianOrbit keplerOrb = ((KeplerianOrbit)scs.getOrbit());
new_state.value_orbit_w = keplerOrb.getPerigeeArgument();
new_state.value_orbit_raan = keplerOrb.getRightAscensionOfAscendingNode();
updateStateOrbit(new_state);
}
......
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