Differentiation

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 25100%0 of 0n/a030303
differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngle, double, int)11100%n/a010101
differentiate(ParameterFunction, int, double)7100%n/a010101
static {...}7100%n/a010101