ThirdBodyAttraction

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 191100%0 of 0n/a0703107
accelerationDerivatives(SpacecraftState, String)52100%n/a010701
addContribution(SpacecraftState, TimeDerivativesEquations)51100%n/a010701
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D, FieldVector3D, FieldRotation, DerivativeStructure)48100%n/a010701
ThirdBodyAttraction(CelestialBody)24100%n/a010401
setParameter(String, double)7100%n/a010301
getParameter(String)6100%n/a010201
getEventsDetectors()3100%n/a010101