AbstractIntegratedPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total19 of 72397%3 of 4293%3563163035
propagate(AbsoluteDate, boolean)1416392%1990%1623801
propagate(AbsoluteDate)51979%1375%131501
createInitialState(SpacecraftState)44100%2100%020701
createODE(ODEIntegrator, ODEState)43100%2100%020801
getCompleteState(double, double[])42100%4100%030701
getManagedAdditionalStates()41100%2100%020601
isAdditionalStateManaged(String)27100%6100%040701
propagate(AbsoluteDate, AbsoluteDate)26100%4100%030501
setAttitudeProvider(AttitudeProvider)24100%n/a010501
addAdditionalEquations(AdditionalEquations)23100%2100%020501
setOrbitType(OrbitType)21100%n/a010401
setPositionAngleType(PositionAngle)21100%n/a010401
setMu(double)21100%n/a010401
setMasterMode(OrekitStepHandler)20100%n/a010601
AbstractIntegratedPropagator(ODEIntegrator, boolean)19100%n/a010601
setEphemerisMode(OrekitStepHandler)19100%n/a010601
setUpUserEventDetectors()18100%2100%020401
setEphemerisMode()18100%n/a010601
getGeneratedEphemeris()16100%2100%020301
setUpEventDetector(ODEIntegrator, EventDetector)14100%n/a010501
setSlaveMode()12100%1150%120501
initMapper()11100%n/a010201
addEventDetector(EventDetector)6100%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(SpacecraftState, AbsoluteDate)100%n/a010101
afterIntegration()100%n/a010101