AbstractIntegratedPropagator.ConvertedMainStateEquations

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 142100%1 of 683%1802805
updateStatesFromAdditionalDerivativesIfKnown(SpacecraftState)51100%1583%1401001
init(double, double[], double)37100%n/a010701
computeDerivatives(double, double[])37100%n/a010601
AbstractIntegratedPropagator.ConvertedMainStateEquations(AbstractIntegratedPropagator, AbstractIntegratedPropagator.MainStateEquations)13100%n/a010401
getDimension()4100%n/a010101