DSSTPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total47 of 68793%8 of 4883%124911156525
computeMeanOrbit(SpacecraftState, AttitudeProvider, Collection)1220794%51372%51014201
getSelectedCoefficients()110%20%222211
setAttitudeProvider(AttitudeProvider)81157%1150%122501
setSatelliteRevolution(int)50%n/a112211
removeForceModels()40%n/a112211
getSatelliteRevolution()40%n/a111111
initialIsOsculating()30%n/a111111
beforeIntegration(SpacecraftState, AbsoluteDate)81100%6100%0401901
computeOsculatingOrbit(SpacecraftState, List)63100%4100%0301201
computeOsculatingState(SpacecraftState, AttitudeProvider, Collection)55100%2100%0201001
afterIntegration()46100%8100%0501201
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame)32100%2100%020701
DSSTPropagator(ODEIntegrator, boolean)24100%n/a010801
DSSTPropagator(ODEIntegrator)24100%n/a010801
computeMeanState(SpacecraftState, AttitudeProvider, Collection)16100%n/a010201
getInitialIntegrationState()14100%2100%020301
setSelectedCoefficients(Set)12100%2100%020301
addForceModel(DSSTForceModel)10100%n/a010301
resetInitialState(SpacecraftState)8100%n/a010301
setInitialState(SpacecraftState, boolean)7100%n/a010301
setInterpolationGridToFixedNumberOfPoints(int)7100%n/a010201
setInterpolationGridToMaxTimeGap(double)7100%n/a010201
getMainStateEquations(ODEIntegrator)6100%n/a010101
setInitialState(SpacecraftState)5100%n/a010201
tolerances(double, Orbit)5100%n/a010101