AdapterPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total49 of 12561%4 of 1060%714143159
basicPropagate(AbsoluteDate)275366%4660%2681801
resetInitialState(SpacecraftState)50%n/a112211
propagateOrbit(AbsoluteDate)50%n/a111111
getMass(AbsoluteDate)50%n/a111111
getEffects()40%n/a111111
getPropagator()30%n/a111111
AdapterPropagator(Propagator)13100%n/a010401
addEffect(AdapterPropagator.DifferentialEffect)6100%n/a010201
getInitialState()4100%n/a010101