FieldAbstractIntegratedPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total40 of 80395%7 of 5487%7627177035
propagate(FieldAbsoluteDate, boolean)1716390%11191%1744101
propagate(FieldAbsoluteDate)143068%3562%3521001
propagate(FieldAbsoluteDate, FieldAbsoluteDate)93780%2675%2511001
createInitialState(FieldSpacecraftState)82100%4100%0301001
createODE(FieldODEIntegrator, FieldODEState)43100%2100%020801
getCompleteState(RealFieldElement, RealFieldElement[], RealFieldElement[])43100%4100%030701
getManagedAdditionalStates()41100%2100%020601
isAdditionalStateManaged(String)27100%6100%040701
setAttitudeProvider(AttitudeProvider)24100%n/a010501
FieldAbstractIntegratedPropagator(Field, FieldODEIntegrator, PropagationType)23100%n/a010701
addAdditionalEquations(FieldAdditionalEquations)23100%2100%020501
setOrbitType(OrbitType)21100%n/a010401
setPositionAngleType(PositionAngle)21100%n/a010401
setMu(RealFieldElement)21100%n/a010401
setMasterMode(FieldOrekitStepHandler)20100%n/a010601
initMapper(Field)18100%n/a010301
setUpUserEventDetectors()18100%2100%020401
setEphemerisMode()18100%n/a010601
setUpEventDetector(FieldODEIntegrator, FieldEventDetector)16100%n/a010501
getGeneratedEphemeris()16100%2100%020301
setSlaveMode()12100%1150%120501
addEventDetector(FieldEventDetector)6100%n/a010201
setResetAtEnd(boolean)4100%n/a010201
getOrbitType()4100%n/a010101
getPositionAngleType()4100%n/a010101
getMu()4100%n/a010101
getEventsDetectors()4100%n/a010101
clearEventsDetectors()4100%n/a010201
isMeanOrbit()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