NumericalPropagator.Main

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total10 of 18895%2 of 1283%21213106
addMassDerivative(double)101357%1150%121401
NumericalPropagator.Main(NumericalPropagator, AbstractIntegrator)52100%1583%1401001
computeDerivatives(SpacecraftState)44100%2100%020701
addXYZAcceleration(double, double, double)37100%2100%020401
addAcceleration(Vector3D, Frame)22100%n/a010401
addKeplerContribution(double)10100%n/a010201