KeplerianPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total3 of 19598%1 of 887%114047010
resetInitialState(SpacecraftState)33090%1150%120901
fixState(Orbit, Attitude, double, double, Map)53100%2100%0201001
KeplerianPropagator(Orbit, AttitudeProvider, double, double)28100%n/a010901
propagateOrbit(AbsoluteDate)21100%2100%020401
resetIntermediateState(SpacecraftState, boolean)19100%2100%020501
KeplerianPropagator(Orbit)10100%n/a010301
KeplerianPropagator(Orbit, double)9100%n/a010201
KeplerianPropagator(Orbit, AttitudeProvider)8100%n/a010201
KeplerianPropagator(Orbit, AttitudeProvider, double)7100%n/a010201
getMass(AbsoluteDate)7100%n/a010101