Differentiation.StateComponentFunction

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 83100%0 of 0n/a0202002
value(double)62100%n/a0101201
Differentiation.StateComponentFunction(int, StateFunction, AttitudeProvider, SpacecraftState, OrbitType, PositionAngle)21100%n/a010801