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Version du 7 juillet 2017 à 06:49
Orbit
To initialize an orbit, we simply have to build it using [PATRIUS] object. For example:
final TimeScale TUC = TimeScalesFactory.getUTC(); final AbsoluteDate date = new AbsoluteDate("2010-01-01T12:00:00.000", TUC); final double sma = Constants.WGS84_EARTH_EQUATORIAL_RADIUS + 250.e3; final double ecc = 0.; final double inc = FastMath.toRadians(51.6); final double raan = FastMath.toRadians(0.); final double pa = FastMath.toRadians(0.); final double ano = FastMath.toRadians(0.); final Frame GCRF = FramesFactory.getGCRF(); final KeplerianOrbit iniOrbit = new KeplerianOrbit(sma, ecc, inc, raan, pa, ano, PositionAngle.MEAN, GCRF, date, MU);
