AbstractIntegratedPropagator.AdaptedStepInterpolator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total8 of 16895%1 of 475%112330010
restrictStep(SpacecraftState, SpacecraftState)61875%n/a012501
secondaryDerivative(SpacecraftState)25496%1375%1311001
convertFromOrekit(SpacecraftState)40100%n/a010601
getInterpolatedState(AbsoluteDate)13100%n/a010101
AbstractIntegratedPropagator.AdaptedStepInterpolator(AbstractIntegratedPropagator, ODEStateInterpolator)9100%n/a010301
getPreviousState()7100%n/a010101
getCurrentState()7100%n/a010101
isPreviousStateInterpolated()4100%n/a010101
isCurrentStateInterpolated()4100%n/a010101
isForward()4100%n/a010101