KeplerianPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total9 of 31997%2 of 2090%221269011
writeReplace()611995%11191%1722401
resetInitialState(SpacecraftState)33391%1150%120901
fixState(Orbit, Attitude, double, double, Map)53100%2100%0201001
KeplerianPropagator(Orbit, AttitudeProvider, double, double)31100%n/a010901
propagateOrbit(AbsoluteDate)21100%2100%020401
resetIntermediateState(SpacecraftState, boolean)16100%2100%020401
KeplerianPropagator(Orbit)8100%n/a010201
KeplerianPropagator(Orbit, AttitudeProvider)8100%n/a010201
KeplerianPropagator(Orbit, double)7100%n/a010201
KeplerianPropagator(Orbit, AttitudeProvider, double)7100%n/a010201
getMass(AbsoluteDate)7100%n/a010101