FieldIntegratedEphemeris

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total12 of 30696%1 of 1291%120253014
basicPropagate(FieldAbsoluteDate)123071%1150%122701
getInterpolatedState(FieldAbsoluteDate)82100%4100%030701
updateAdditionalStates(FieldSpacecraftState)77100%4100%0301401
FieldIntegratedEphemeris(FieldAbsoluteDate, FieldAbsoluteDate, FieldAbsoluteDate, FieldStateMapper, PropagationType, FieldDenseOutputModel, FieldArrayDictionary, List, String[], int[])56100%2100%0201501
resetInitialState(FieldSpacecraftState)7100%n/a010101
resetIntermediateState(FieldSpacecraftState, boolean)7100%n/a010101
getInitialState()7100%n/a010101
getPVCoordinates(FieldAbsoluteDate, Frame)6100%n/a010101
propagateOrbit(FieldAbsoluteDate, CalculusFieldElement[])5100%n/a010101
getMass(FieldAbsoluteDate)5100%n/a010101
getFrame()4100%n/a010101
getMinDate()3100%n/a010101
getMaxDate()3100%n/a010101
getParametersDrivers()2100%n/a010101