Ephemeris

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 497100%2 of 3494%2400100023
Ephemeris(List, TimeInterpolator, List, TimeInterpolator, AttitudeProvider)95100%4100%0301901
checkStatesAndCovariancesConsistency(List, List)70100%6100%0401001
basicPropagate(AbsoluteDate)70100%4100%0301701
buildOrbitAndCovarianceSample()37100%2100%020601
checkInputConsistency(List, TimeInterpolator, List, TimeInterpolator)33100%4100%030901
isAdditionalStateManaged(String)31100%6100%040601
getManagedAdditionalStates()30100%n/a010501
getCovariance(AbsoluteDate)25100%2466%240601
Ephemeris(List, int)22100%n/a010401
Ephemeris(List, TimeInterpolator, List, TimeInterpolator)18100%2100%020301
Ephemeris(List, TimeInterpolator, AttitudeProvider)10100%n/a010201
Ephemeris(List, TimeInterpolator)9100%n/a010201
resetInitialState(SpacecraftState)7100%n/a010101
resetIntermediateState(SpacecraftState, boolean)7100%n/a010101
propagateOrbit(AbsoluteDate)5100%n/a010101
getMass(AbsoluteDate)5100%n/a010101
getInitialState()5100%n/a010101
getCovarianceInterpolator()4100%n/a010101
getMinDate()3100%n/a010101
getMaxDate()3100%n/a010101
getFrame()3100%n/a010101
getStateInterpolator()3100%n/a010101
createHarvester(String, RealMatrix, DoubleArrayDictionary)2100%n/a010101