FieldIntegratedEphemeris

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total31 of 19484%1 of 1090%417534312
basicPropagate(FieldAbsoluteDate)143068%1150%122701
resetIntermediateState(FieldSpacecraftState, boolean)70%n/a111111
propagateOrbit(FieldAbsoluteDate)50%n/a111111
getMass(FieldAbsoluteDate)50%n/a111111
FieldIntegratedEphemeris(FieldAbsoluteDate, FieldAbsoluteDate, FieldAbsoluteDate, FieldStateMapper, PropagationType, FieldDenseOutputModel, Map, List, String[])60100%4100%0301401
getInterpolatedState(FieldAbsoluteDate)43100%4100%030401
resetInitialState(FieldSpacecraftState)7100%n/a010101
getInitialState()7100%n/a010101
getPVCoordinates(FieldAbsoluteDate, Frame)6100%n/a010101
getFrame()4100%n/a010101
getMinDate()3100%n/a010101
getMaxDate()3100%n/a010101