propagate(AbsoluteDate, boolean) | | 92% | | 92% | 1 | 8 | 2 | 37 | 0 | 1 |
propagate(AbsoluteDate) | | 79% | | 75% | 1 | 3 | 1 | 5 | 0 | 1 |
createInitialState(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
getCompleteState(double, double[], double[]) | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
createODE(ODEIntegrator, ODEState) | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
getManagedAdditionalStates() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
isAdditionalStateManaged(String) | | 100% | | 100% | 0 | 4 | 0 | 7 | 0 | 1 |
propagate(AbsoluteDate, AbsoluteDate) | | 100% | | 100% | 0 | 3 | 0 | 5 | 0 | 1 |
setAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
addAdditionalEquations(AdditionalEquations) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
AbstractIntegratedPropagator(ODEIntegrator, boolean) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
setOrbitType(OrbitType) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
setPositionAngleType(PositionAngle) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
setMu(double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
setMasterMode(OrekitStepHandler) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
setEphemerisMode(OrekitStepHandler) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
setUpUserEventDetectors() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
setEphemerisMode() | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
getGeneratedEphemeris() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
setUpEventDetector(ODEIntegrator, EventDetector) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
setSlaveMode() | | 100% | | 50% | 1 | 2 | 0 | 5 | 0 | 1 |
initMapper() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
addEventDetector(EventDetector) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setResetAtEnd(boolean) | | 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 |
getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEventsDetectors() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
clearEventsDetectors() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
isMeanOrbit() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getCalls() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getInitialIntegrationState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getIntegrator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getBasicDimension() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
beforeIntegration(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
afterIntegration() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |