SmallManeuverAnalyticalModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total22 of 75897%3 of 4092%431592211
getJacobian(Orbit, PositionAngle, double[][])1537096%31986%21233101
getInertialFrame()40%n/a111111
getInertialDV()0%n/a111111
updateOrbit(Orbit)119100%4100%0301601
SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double)97100%4100%0301601
evaluateJ0Dot()93100%6100%0401501
apply(SpacecraftState)23100%2100%020401
apply(Orbit)13100%2100%020301
SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double)12100%n/a010301
updateMass(double)5100%n/a010101
getDate()4100%n/a010101