NumericalPropagator.Main

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total12 of 20294%1 of 1493%11413507
addMassDerivative(double)121352%1150%121401
NumericalPropagator.Main(NumericalPropagator, ODEIntegrator)52100%6100%0401001
computeDerivatives(SpacecraftState)38100%2100%020701
addXYZAcceleration(double, double, double)37100%2100%020401
addAcceleration(Vector3D, Frame)22100%n/a010401
init(SpacecraftState, AbsoluteDate)18100%2100%020401
addKeplerContribution(double)10100%n/a010201