integrateDynamics(FieldAbsoluteDate) |   | 90% |   | 87% | 1 | 5 | 2 | 31 | 0 | 1 |
propagate(FieldAbsoluteDate) |   | 79% |   | 75% | 1 | 3 | 1 | 5 | 0 | 1 |
secondary(FieldSpacecraftState) |   | 96% |   | 75% | 1 | 3 | 1 | 10 | 0 | 1 |
secondaryDerivative(FieldSpacecraftState) |   | 96% |   | 75% | 1 | 3 | 1 | 10 | 0 | 1 |
propagate(FieldAbsoluteDate, FieldAbsoluteDate) |  | 100% |  | 100% | 0 | 5 | 0 | 16 | 0 | 1 |
convert(FieldODEStateAndDerivative) |  | 100% |  | 100% | 0 | 3 | 0 | 16 | 0 | 1 |
createInitialState(FieldSpacecraftState) |  | 100% |  | 100% | 0 | 3 | 0 | 10 | 0 | 1 |
updateAdditionalStatesAndDerivatives(FieldSpacecraftState, FieldODEStateAndDerivative) |  | 100% |  | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
getManagedAdditionalStates() |  | 100% |  | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
convert(FieldSpacecraftState) |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
FieldAbstractIntegratedPropagator(Field, FieldODEIntegrator, PropagationType) |  | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
isAdditionalStateManaged(String) |  | 100% |  | 100% | 0 | 4 | 0 | 7 | 0 | 1 |
addAdditionalDerivativesProvider(FieldAdditionalDerivativesProvider) |  | 100% |  | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
setAttitudeProvider(AttitudeProvider) |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
createODE(FieldODEIntegrator) |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
setOrbitType(OrbitType) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
setPositionAngleType(PositionAngleType) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
setMu(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
initMapper(Field) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
setUpUserEventDetectors() |  | 100% |  | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
getEphemerisGenerator() |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
setUpEventDetector(FieldODEIntegrator, FieldEventDetector) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
addEventDetector(FieldEventDetector) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setResetAtEnd(boolean) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getIntegratorName() |  | 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 |
getMu() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAdditionalDerivativesProviders() |  | 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 |
getResetAtEnd() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
initializeAttitudeProviderForDerivatives() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
isMeanOrbit() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPropagationType() |  | 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(FieldSpacecraftState, FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
afterIntegration() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |