AbstractIntegratedPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total23 of 87097%4 of 5292%4675187041
integrateDynamics(AbsoluteDate, boolean)1412089%1990%1623001
propagate(AbsoluteDate)51979%1375%131501
secondary(SpacecraftState)25096%1375%1311001
secondaryDerivative(SpacecraftState)25096%1375%1311001
propagate(AbsoluteDate, AbsoluteDate)89100%8100%0501801
updateAdditionalStatesAndDerivatives(SpacecraftState, ODEStateAndDerivative)62100%4100%0301201
createInitialState(SpacecraftState)57100%4100%0301001
getManagedAdditionalStates()41100%2100%020601
convert(SpacecraftState)35100%n/a010601
AbstractIntegratedPropagator(ODEIntegrator, PropagationType)32100%n/a010901
isAdditionalStateManaged(String)27100%6100%040701
addAdditionalDerivativesProvider(AdditionalDerivativesProvider)26100%2100%020601
setAttitudeProvider(AttitudeProvider)24100%n/a010501
createODE(ODEIntegrator)24100%2100%020501
setOrbitType(OrbitType)21100%n/a010401
setPositionAngleType(PositionAngleType)21100%n/a010401
setMu(double)21100%n/a010401
setUpUserEventDetectors()18100%2100%020401
convert(ODEStateAndDerivative)17100%n/a010301
getEphemerisGenerator()13100%n/a010301
initMapper()11100%n/a010201
setUpEventDetector(ODEIntegrator, EventDetector)8100%n/a010201
addEventDetector(EventDetector)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
getPropagationType()3100%n/a010101
getCalls()3100%n/a010101
getInitialIntegrationState()3100%n/a010101
getIntegrator()3100%n/a010101
getBasicDimension()2100%n/a010101
setUpStmAndJacobianGenerators()100%n/a010101
beforeIntegration(SpacecraftState, AbsoluteDate)100%n/a010101
afterIntegration()100%n/a010101