DSSTPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total49 of 1,17995%7 of 11193%89811257242
removeForceModels()280%20%228811
computeMeanOrbit(SpacecraftState, AttitudeProvider, Collection, double, int)1221394%41477%41014101
setInitialState(SpacecraftState, PropagationType)51777%1266%131801
getShortPeriodTerms()40%n/a111111
setUpRegularParametersJacobiansColumns(DSSTStateTransitionMatrixGenerator)122100%18100%01002601
beforeIntegration(SpacecraftState, AbsoluteDate)108100%8100%0502201
setUpStmGenerator()63100%10100%0601801
computeOsculatingState(SpacecraftState, AttitudeProvider, Collection)63100%2100%0201001
computeOsculatingOrbit(SpacecraftState, List)63100%4100%0301201
getJacobiansColumnsNames()57100%10100%0601001
addForceModel(DSSTForceModel)56100%6100%0401001
afterIntegration()47100%8100%0501201
getShortPeriodTermsValue(SpacecraftState)40100%4100%030701
createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame)32100%2100%020701
DSSTPropagator(ODEIntegrator, PropagationType, AttitudeProvider)24100%n/a010801
computeMeanState(SpacecraftState, AttitudeProvider, Collection, double, int)20100%n/a010301
setAttitudeProvider(AttitudeProvider)19100%2100%020501
hasNewtonianAttraction()18100%4100%030201
resetInitialState(SpacecraftState)15100%2100%020501
setUpStmAndJacobianGenerators()14100%2100%020601
getInitialIntegrationState()14100%2100%020301
setSelectedCoefficients(Set)12100%2100%020201
getSelectedCoefficients()11100%2100%020201
DSSTPropagator(ODEIntegrator, PropagationType)8100%n/a010301
createHarvester(String, RealMatrix, DoubleArrayDictionary)8100%n/a010101
setMu(double)7100%n/a010201
setInterpolationGridToFixedNumberOfPoints(int)7100%n/a010201
setInterpolationGridToMaxTimeGap(double)7100%n/a010201
computeMeanState(SpacecraftState, AttitudeProvider, Collection)7100%n/a010101
getMainStateEquations(ODEIntegrator)6100%n/a010101
tolerances(double, double, Orbit)6100%n/a010101
DSSTPropagator(ODEIntegrator)5100%n/a010201
setInitialState(SpacecraftState)5100%n/a010201
setSatelliteRevolution(int)5100%n/a010201
setShortPeriodTerms(List)5100%n/a010201
tolerances(double, Orbit)5100%n/a010101
superSetMu(double)4100%n/a010201
getAllForceModels()4100%n/a010101
getSatelliteRevolution()4100%n/a010101
initialIsOsculating()3100%n/a010101
getOrbitType()3100%n/a010101
getPositionAngleType()3100%n/a010101