FieldDSSTPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total116 of 92087%13 of 6178%206528193934
removeForceModels()280%20%228811
addForceModel(DSSTForceModel)174572%1583%1431301
computeMeanOrbit(FieldSpacecraftState, AttitudeProvider, Collection, double, int)1225495%51372%51014301
getSelectedCoefficients()110%20%222211
afterIntegration()82071%1375%132801
setAttitudeProvider(AttitudeProvider)81157%1150%122501
setInitialState(FieldSpacecraftState, PropagationType)51777%1266%131801
setInitialState(FieldSpacecraftState)50%n/a112211
setSatelliteRevolution(int)50%n/a112211
getAllForceModels()40%n/a111111
getSatelliteRevolution()40%n/a111111
initialIsOsculating()30%n/a111111
getOrbitType()30%n/a111111
getPositionAngleType()30%n/a111111
beforeIntegration(FieldSpacecraftState, FieldAbsoluteDate)86100%6100%0401901
computeOsculatingOrbit(FieldSpacecraftState, List)71100%4100%0301201
computeOsculatingState(FieldSpacecraftState, AttitudeProvider, Collection)64100%2100%0201001
createMapper(FieldAbsoluteDate, RealFieldElement, OrbitType, PositionAngle, AttitudeProvider, Frame)33100%2100%020701
FieldDSSTPropagator(Field, FieldODEIntegrator, PropagationType, AttitudeProvider)29100%n/a010901
FieldDSSTPropagator(Field, FieldODEIntegrator, AttitudeProvider)29100%n/a010901
computeMeanState(FieldSpacecraftState, AttitudeProvider, Collection, double, int)19100%n/a010201
hasNewtonianAttraction()18100%4100%030201
resetInitialState(FieldSpacecraftState)15100%2100%020501
getInitialIntegrationState()15100%2100%020301
setSelectedCoefficients(Set)12100%2100%020201
FieldDSSTPropagator(Field, FieldODEIntegrator, PropagationType)9100%n/a010301
setInterpolationGridToFixedNumberOfPoints(int)9100%n/a010201
setInterpolationGridToMaxTimeGap(RealFieldElement)9100%n/a010201
FieldDSSTPropagator(Field, FieldODEIntegrator)8100%n/a010301
setMu(RealFieldElement)8100%n/a010201
computeMeanState(FieldSpacecraftState, AttitudeProvider, Collection)8100%n/a010101
getMainStateEquations(FieldODEIntegrator)6100%n/a010101
tolerances(RealFieldElement, FieldOrbit)5100%n/a010101
superSetMu(RealFieldElement)4100%n/a010201