Differentiation

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total8 of 3375%0 of 0n/a141414
differentiate(ParameterFunction, ParameterDriver, int, double)80%n/a111111
differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngle, double, int)11100%n/a010101
differentiate(ParameterFunction, int, double)7100%n/a010101
static {...}7100%n/a010101