NumericalPropagator.Main

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total12 of 28995%1 of 2095%11814508
addMassDerivative(double)121352%1150%121401
computeDerivatives(SpacecraftState)78100%6100%0401301
addKeplerContribution(double)69100%4100%0301101
NumericalPropagator.Main(NumericalPropagator, ODEIntegrator)58100%6100%0401101
addNonKeplerianAcceleration(Vector3D)40100%2100%020401
init(SpacecraftState, AbsoluteDate)8100%n/a010201
lambda$new$0(ODEIntegrator, EventDetector)6100%n/a010101
lambda$init$1(SpacecraftState, AbsoluteDate, ForceModel)5100%n/a010101