AbstractIntegratedPropagator.ConvertedMainStateEquations

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 143100%1 of 683%1802805
updateStatesFromAdditionalDerivativesIfKnown(SpacecraftState)51100%1583%1401001
computeDerivatives(double, double[])40100%n/a010601
init(double, double[], double)36100%n/a010701
AbstractIntegratedPropagator.ConvertedMainStateEquations(AbstractIntegratedPropagator, AbstractIntegratedPropagator.MainStateEquations)12100%n/a010401
getDimension()4100%n/a010101