DSSTPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total58 of 66891%9 of 4680%144815137625
computeMeanOrbit(SpacecraftState, Collection)1219394%61062%6912701
getSelectedCoefficients()110%20%222211
setAttitudeProvider(AttitudeProvider)81158%1150%122501
getInitialIntegrationState()61267%2100%022501
setInitialState(SpacecraftState)50%n/a112211
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)58100%4100%030901
computeOsculatingState(SpacecraftState, Collection)52100%2100%020801
afterIntegration()46100%8100%0501201
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame)32100%2100%020701
DSSTPropagator(AbstractIntegrator, boolean)24100%n/a010801
DSSTPropagator(AbstractIntegrator)24100%n/a010801
computeMeanState(SpacecraftState, Collection)15100%n/a010201
setSelectedCoefficients(Set)12100%2100%020201
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(AbstractIntegrator)6100%n/a010101
tolerances(double, Orbit)5100%n/a010101