FieldNumericalPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total26 of 40093%6 of 2475%831881219
addForceModel(ForceModel)114781%1583%1431201
resetInitialState(FieldSpacecraftState)41173%1150%121501
removeForceModels()40%n/a112211
getOrbitType()30%n/a111111
getNewtonianAttractionForceModel()22090%2250%231401
getForceModels()21487%1150%120101
tolerances(RealFieldElement, FieldOrbit, OrbitType)184100%6100%0403001
FieldNumericalPropagator(Field, FieldODEIntegrator)27100%n/a010901
hasNewtonianAttraction()18100%1375%130201
createMapper(FieldAbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame)11100%n/a010101
setMu(double)7100%n/a010201
getPVCoordinates(FieldAbsoluteDate, Frame)6100%n/a010101
getMainStateEquations(FieldODEIntegrator)6100%n/a010101
superSetMu(double)4100%n/a010201
getAllForceModels()4100%n/a010101
setOrbitType(OrbitType)4100%n/a010201
setPositionAngleType(PositionAngle)4100%n/a010201
setInitialState(FieldSpacecraftState)4100%n/a010201
getPositionAngleType()3100%n/a010101