DSSTPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total85 of 82789%11 of 6583%166619181733
removeForceModels()280%20%228811
computeMeanOrbit(SpacecraftState, AttitudeProvider, Collection, double, int)1221194%51372%51014101
addForceModel(DSSTForceModel)114480%1583%1411001
getSelectedCoefficients()110%20%222211
setInitialState(SpacecraftState, PropagationType)51777%1266%131801
setSatelliteRevolution(int)50%n/a112211
getSatelliteRevolution()40%n/a111111
initialIsOsculating()30%n/a111111
getOrbitType()30%n/a111111
getPositionAngleType()30%n/a111111
beforeIntegration(SpacecraftState, AbsoluteDate)84100%6100%0401901
computeOsculatingOrbit(SpacecraftState, List)63100%4100%0301201
computeOsculatingState(SpacecraftState, AttitudeProvider, Collection)59100%2100%0201001
afterIntegration()47100%8100%0501201
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame)32100%2100%020701
DSSTPropagator(ODEIntegrator, PropagationType, AttitudeProvider)24100%n/a010801
setAttitudeProvider(AttitudeProvider)19100%2100%020501
hasNewtonianAttraction()18100%4100%030201
computeMeanState(SpacecraftState, AttitudeProvider, Collection, double, int)18100%n/a010201
resetInitialState(SpacecraftState)15100%2100%020501
getInitialIntegrationState()14100%2100%020301
setSelectedCoefficients(Set)12100%2100%020201
DSSTPropagator(ODEIntegrator, PropagationType)8100%n/a010301
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
DSSTPropagator(ODEIntegrator)5100%n/a010201
setInitialState(SpacecraftState)5100%n/a010201
tolerances(double, Orbit)5100%n/a010101
superSetMu(double)4100%n/a010201
getAllForceModels()4100%n/a010101