lambda$setUpTriggerDatesJacobiansColumns$2(String, Maneuver, ManeuverTriggers, List, ParameterDrivenDateIntervalDetector) |   | 69% |   | 91% | 2 | 13 | 12 | 37 | 0 | 1 |
beforeIntegration(SpacecraftState, AbsoluteDate) |   | 14% |   | 16% | 3 | 4 | 5 | 7 | 0 | 1 |
setInitialColumn(String, double[]) |   | 68% |   | 50% | 1 | 2 | 2 | 12 | 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, double, Orbit, OrbitType) |  | 100% |  | 100% | 0 | 4 | 0 | 25 | 0 | 1 |
setUpRegularParametersJacobiansColumns(StateTransitionMatrixGenerator, List) |  | 100% |  | 100% | 0 | 11 | 0 | 25 | 0 | 1 |
manageTriggerDate(String, Maneuver, ManeuverTriggers, String, boolean, double) |  | 100% |  | 100% | 0 | 6 | 0 | 16 | 0 | 1 |
setUpStmGenerator() |  | 100% |  | 100% | 0 | 6 | 0 | 17 | 0 | 1 |
tolerances(double, AbsolutePVCoordinates) |  | 100% | | n/a | 0 | 1 | 0 | 13 | 0 | 1 |
getJacobiansColumnsNames() |  | 100% |  | 100% | 0 | 6 | 0 | 10 | 0 | 1 |
setUpTriggerDatesJacobiansColumns(String) |  | 100% |  | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
NumericalPropagator(ODEIntegrator, AttitudeProvider) |  | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
tolerances(double, Orbit, OrbitType) |  | 100% | | n/a | 0 | 1 | 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 |
resetInitialState(SpacecraftState) |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
initializeAttitudeProviderForDerivatives() |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) |  | 100% | | n/a | 0 | 1 | 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 |
getMainStateEquations(ODEIntegrator) |  | 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 |
getOrbitType() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPositionAngleType() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$setUpTriggerDatesJacobiansColumns$1(EventDetector) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$setUpTriggerDatesJacobiansColumns$0(EventDetector) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
static {...} |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |