FieldAbstractIntegratedPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total22 of 95597%4 of 5492%4685200041
integrateDynamics(FieldAbsoluteDate)1311990%1787%1523101
propagate(FieldAbsoluteDate)51979%1375%131501
secondary(FieldSpacecraftState)25496%1375%1311001
secondaryDerivative(FieldSpacecraftState)25496%1375%1311001
propagate(FieldAbsoluteDate, FieldAbsoluteDate)83100%8100%0501601
convert(FieldODEStateAndDerivative)76100%4100%0301601
createInitialState(FieldSpacecraftState)65100%4100%0301001
updateAdditionalStatesAndDerivatives(FieldSpacecraftState, FieldODEStateAndDerivative)64100%4100%0301201
getManagedAdditionalStates()41100%2100%020601
convert(FieldSpacecraftState)41100%n/a010601
FieldAbstractIntegratedPropagator(Field, FieldODEIntegrator, PropagationType)33100%n/a010901
isAdditionalStateManaged(String)27100%6100%040701
addAdditionalDerivativesProvider(FieldAdditionalDerivativesProvider)26100%2100%020601
setAttitudeProvider(AttitudeProvider)24100%n/a010501
createODE(FieldODEIntegrator)24100%2100%020501
setOrbitType(OrbitType)21100%n/a010401
setPositionAngleType(PositionAngleType)21100%n/a010401
setMu(CalculusFieldElement)21100%n/a010401
initMapper(Field)18100%n/a010301
setUpUserEventDetectors()18100%2100%020401
getEphemerisGenerator()13100%n/a010301
setUpEventDetector(FieldODEIntegrator, FieldEventDetector)8100%n/a010201
addEventDetector(FieldEventDetector)6100%n/a010201
setResetAtEnd(boolean)4100%n/a010201
getIntegratorName()4100%n/a010101
getOrbitType()4100%n/a010101
getPositionAngleType()4100%n/a010101
getMu()4100%n/a010101
getAdditionalDerivativesProviders()4100%n/a010101
getEventsDetectors()4100%n/a010101
clearEventsDetectors()4100%n/a010201
getResetAtEnd()3100%n/a010101
initializeAttitudeProviderForDerivatives()3100%n/a010101
isMeanOrbit()3100%n/a010101
getPropagationType()3100%n/a010101
getCalls()3100%n/a010101
getInitialIntegrationState()3100%n/a010101
getIntegrator()3100%n/a010101
getBasicDimension()2100%n/a010101
beforeIntegration(FieldSpacecraftState, FieldAbsoluteDate)100%n/a010101
afterIntegration()100%n/a010101