Differentiation.StateComponentFunction

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total4 of 9395%1 of 250%1301902
value(double)46894%1150%1201101
Differentiation.StateComponentFunction(int, StateFunction, AttitudeProvider, SpacecraftState, OrbitType, PositionAngleType)21100%n/a010801