NumericalPropagator.Main

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total14 of 33695%3 of 2889%32215308
addMassDerivative(double)121352%1150%121401
init(SpacecraftState, AbsoluteDate)25596%2880%2601001
computeDerivatives(SpacecraftState)77100%6100%0401301
addKeplerContribution(double)68100%4100%0301101
NumericalPropagator.Main(NumericalPropagator, ODEIntegrator)58100%4100%0301101
addNonKeplerianAcceleration(Vector3D)40100%2100%020401
lambda$new$0(ODEIntegrator, EventDetector)6100%n/a010101
lambda$init$1(SpacecraftState, AbsoluteDate, ForceModel)5100%n/a010101