Differentiation

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total3 of 4393%0 of 0n/a142914
Differentiation()30%n/a112211
differentiate(ParameterFunction, ParameterDriver, int, double)22100%n/a010501
differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngle, double, int)11100%n/a010101
static {...}7100%n/a010101