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Commit 2f1cf585 authored by houmingyang's avatar houmingyang
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change the param for test the Issue 61 bug.

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...@@ -83,15 +83,15 @@ public class InterVisuSatExample { ...@@ -83,15 +83,15 @@ public class InterVisuSatExample {
//// Build of the first satellite with an orbit with 20 degree inclination //// Build of the first satellite with an orbit with 20 degree inclination
// Build of a LEO orbit // Build of a LEO orbit
final KeplerianOrbit firstOrbit = new KeplerianOrbit(7878000, 0, FastMath.toRadians(0), FastMath.toRadians(0), final KeplerianOrbit firstOrbit = new KeplerianOrbit(7838000, 0, FastMath.toRadians(45), FastMath.toRadians(20),
FastMath.toRadians(0), FastMath.toRadians(0), PositionAngleType.MEAN, FramesFactory.getEME2000(), startDate, FastMath.toRadians(0), FastMath.toRadians(0), PositionAngleType.MEAN, FramesFactory.getEME2000(), startDate,
Constants.WGS84_EARTH_MU); Constants.WGS84_EARTH_MU);
final SpacecraftState firstState = new SpacecraftState(firstOrbit); final SpacecraftState firstState = new SpacecraftState(firstOrbit);
//// Build of the first satellite with an orbit with 40 degree inclination and omega of 90 degrees //// Build of the first satellite with an orbit with 40 degree inclination and omega of 90 degrees
// Build of a LEO orbit // Build of a LEO orbit
final KeplerianOrbit secondOrbit = new KeplerianOrbit(7078000, 0, FastMath.toRadians(20), final KeplerianOrbit secondOrbit = new KeplerianOrbit(17878000, 0, FastMath.toRadians(0),
FastMath.toRadians(45), FastMath.toRadians(0), FastMath.toRadians(0), PositionAngleType.MEAN, FastMath.toRadians(120), FastMath.toRadians(0), FastMath.toRadians(0), PositionAngleType.MEAN,
FramesFactory.getEME2000(), FramesFactory.getEME2000(),
startDate, Constants.WGS84_EARTH_MU); startDate, Constants.WGS84_EARTH_MU);
final SpacecraftState secondState = new SpacecraftState(secondOrbit); final SpacecraftState secondState = new SpacecraftState(secondOrbit);
......
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