Ephemeris

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total9 of 34797%1 of 2696%230165117
resetIntermediateState(SpacecraftState, boolean)70%n/a111111
Ephemeris(List, int, double)21588%1150%120301
Ephemeris(List, int, double, AttitudeProvider)111100%6100%0402001
basicPropagate(AbsoluteDate)103100%12100%0701801
isAdditionalStateManaged(String)31100%6100%040601
getManagedAdditionalStates()30100%n/a010501
resetInitialState(SpacecraftState)7100%n/a010101
Ephemeris(List, int)6100%n/a010201
getPVCoordinates(AbsoluteDate, Frame)6100%n/a010101
propagateOrbit(AbsoluteDate)5100%n/a010101
getMass(AbsoluteDate)5100%n/a010101
getInitialState()5100%n/a010101
getMinDate()3100%n/a010101
getMaxDate()3100%n/a010101
getExtrapolationThreshold()3100%n/a010101
getFrame()3100%n/a010101
createHarvester(String, RealMatrix, DoubleArrayDictionary)2100%n/a010101