AbstractIntegratedPropagator.AdaptedStepInterpolator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total6 of 17896%0 of 4100%012232010
restrictStep(SpacecraftState, SpacecraftState)61875%n/a012501
convert(SpacecraftState)61100%2100%020801
convert(ODEStateAndDerivative)48100%2100%0201001
getInterpolatedState(AbsoluteDate)12100%n/a010101
AbstractIntegratedPropagator.AdaptedStepInterpolator(AbstractIntegratedPropagator, ODEStateInterpolator)9100%n/a010301
getPreviousState()6100%n/a010101
getCurrentState()6100%n/a010101
isPreviousStateInterpolated()4100%n/a010101
isCurrentStateInterpolated()4100%n/a010101
isForward()4100%n/a010101