| setUpTriggerDatesJacobiansColumns(AbstractStateTransitionMatrixGenerator) |   | 76% | | 94% | 2 | 18 | 12 | 55 | 0 | 1 |
| beforeIntegration(SpacecraftState, AbsoluteDate) | | 14% | | 16% | 3 | 4 | 5 | 7 | 0 | 1 |
| setInitialColumn(String, double[]) | | 78% | | 50% | 1 | 2 | 1 | 16 | 0 | 1 |
| removeForceModels() | | 46% | | 50% | 1 | 2 | 4 | 8 | 0 | 1 |
| manageMedianDate(String, String, String) | | 82% | | 50% | 4 | 6 | 3 | 13 | 0 | 1 |
| manageManeuverDuration(String, String, String) | | 82% | | 50% | 4 | 6 | 3 | 13 | 0 | 1 |
| addForceModel(ForceModel) | | 89% | | 100% | 0 | 4 | 2 | 12 | 0 | 1 |
| tolerances(double, AbsolutePVCoordinates) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| manageTriggerDate(String, Maneuver, ResettableManeuverTriggers, String, boolean, double, boolean) | | 100% | | 100% | 0 | 10 | 0 | 29 | 0 | 1 |
| setUpRegularParametersJacobiansColumns(AbstractStateTransitionMatrixGenerator, List) | | 100% | | 100% | 0 | 12 | 0 | 26 | 0 | 1 |
| setUpStmGenerator() | | 100% | | 100% | 0 | 7 | 0 | 21 | 0 | 1 |
| clearMatricesComputation() | | 100% | | 90% | 1 | 6 | 0 | 15 | 0 | 1 |
| getJacobiansColumnsNames() | | 100% | | 100% | 0 | 6 | 0 | 10 | 0 | 1 |
| NumericalPropagator(ODEIntegrator, AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| resetInitialState(SpacecraftState) | | 100% | | 100% | 0 | 3 | 0 | 5 | 0 | 1 |
| setUpStmAndJacobianGenerators() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| hasNewtonianAttraction() | | 100% | | 100% | 0 | 3 | 0 | 2 | 0 | 1 |
| setMu(double) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getMainStateEquations(ODEIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| tolerances(double, double, Orbit, OrbitType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| initializeAttitudeProviderForDerivatives() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| createHarvester(String, RealMatrix, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| NumericalPropagator(ODEIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getSolver(RealMatrix) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| tolerances(double, Orbit, OrbitType) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getLocalDetector(EventDetector, SwitchEventHandler) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$clearMatricesComputation$0(AdditionalDerivativesProvider) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setIgnoreCentralAttraction(boolean) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| superSetMu(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getAllForceModels() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setOrbitType(OrbitType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setPositionAngleType(PositionAngleType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setInitialState(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| lambda$setUpTriggerDatesJacobiansColumns$1(EventDetector) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOrbitType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |