Differentiation

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 86100%0 of 4100%0501303
lambda$differentiate$0(double, OrbitType, PositionAngleType, int, StateFunction, AttitudeProvider, int, SpacecraftState)70100%4100%0301101
differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngleType, double, int)9100%n/a010101
differentiate(ParameterFunction, int, double)7100%n/a010101