FieldNumericalPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total21 of 42195%4 of 2281%532689121
addForceModel(ForceModel)114881%1583%1431201
resetInitialState(FieldSpacecraftState)41173%1150%121501
removeForceModels()40%n/a112211
initializeAttitudeProviderForDerivatives()2981%1150%120301
tolerances(CalculusFieldElement, CalculusFieldElement, FieldOrbit, OrbitType)170100%6100%0402601
FieldNumericalPropagator(Field, FieldODEIntegrator, AttitudeProvider)42100%n/a0101201
tolerances(CalculusFieldElement, FieldOrbit, OrbitType)29100%n/a010501
hasNewtonianAttraction()18100%1375%130201
setMu(CalculusFieldElement)15100%2100%020401
createMapper(FieldAbsoluteDate, CalculusFieldElement, OrbitType, PositionAngleType, AttitudeProvider, Frame)11100%n/a010101
FieldNumericalPropagator(Field, FieldODEIntegrator)8100%n/a010201
getMainStateEquations(FieldODEIntegrator)6100%n/a010101
setIgnoreCentralAttraction(boolean)4100%n/a010201
superSetMu(CalculusFieldElement)4100%n/a010201
getAllForceModels()4100%n/a010101
setOrbitType(OrbitType)4100%n/a010201
setPositionAngleType(PositionAngleType)4100%n/a010201
setInitialState(FieldSpacecraftState)4100%n/a010201
getOrbitType()3100%n/a010101
superGetOrbitType()3100%n/a010101
getPositionAngleType()3100%n/a010101