FieldNumericalPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total22 of 39794%3 of 2085%530785220
addForceModel(ForceModel)114781%1583%1431201
resetInitialState(FieldSpacecraftState)41173%1150%121501
removeForceModels()40%n/a112211
getOrbitType()30%n/a111111
tolerances(RealFieldElement, FieldOrbit, OrbitType)184100%6100%0403001
FieldNumericalPropagator(Field, FieldODEIntegrator, AttitudeProvider)39100%n/a0101101
hasNewtonianAttraction()18100%1375%130201
setMu(RealFieldElement)15100%2100%020401
createMapper(FieldAbsoluteDate, RealFieldElement, OrbitType, PositionAngle, AttitudeProvider, Frame)11100%n/a010101
FieldNumericalPropagator(Field, FieldODEIntegrator)8100%n/a010201
getPVCoordinates(FieldAbsoluteDate, Frame)6100%n/a010101
getMainStateEquations(FieldODEIntegrator)6100%n/a010101
setIgnoreCentralAttraction(boolean)4100%n/a010201
superSetMu(RealFieldElement)4100%n/a010201
getAllForceModels()4100%n/a010101
setOrbitType(OrbitType)4100%n/a010201
setPositionAngleType(PositionAngle)4100%n/a010201
setInitialState(FieldSpacecraftState)4100%n/a010201
superGetOrbitType()3100%n/a010101
getPositionAngleType()3100%n/a010101