tolerances(double, AbsolutePVCoordinates) | | 0% | | n/a | 1 | 1 | 13 | 13 | 1 | 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 | 10 | 0 | 24 | 0 | 1 |
lambda$setUpTriggerDatesJacobiansColumns$2(String, Maneuver, AbstractManeuverTriggers, List, ParameterDrivenDateIntervalDetector) | | 100% | | 100% | 0 | 9 | 0 | 17 | 0 | 1 |
manageTriggerDate(String, Maneuver, AbstractManeuverTriggers, String, boolean, double) | | 100% | | 100% | 0 | 6 | 0 | 16 | 0 | 1 |
setUpStmGenerator() | | 100% | | 100% | 0 | 6 | 0 | 17 | 0 | 1 |
setUpTriggerDatesJacobiansColumns(String) | | 100% | | 83% | 1 | 4 | 0 | 13 | 0 | 1 |
getJacobiansColumnsNames() | | 100% | | 100% | 0 | 5 | 0 | 9 | 0 | 1 |
NumericalPropagator(ODEIntegrator, AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
tolerances(double, Orbit, OrbitType) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
setUpStmAndJacobianGenerators() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
hasNewtonianAttraction() | | 100% | | 100% | 0 | 3 | 0 | 2 | 0 | 1 |
resetInitialState(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
setMu(double) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
createHarvester(String, RealMatrix, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
NumericalPropagator(ODEIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getPVCoordinates(AbsoluteDate, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMainStateEquations(ODEIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setIgnoreCentralAttraction(boolean) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
superSetMu(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getAllForceModels() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setOrbitType(OrbitType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setPositionAngleType(PositionAngle) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setInitialState(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getOrbitType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$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 |