AngularRaDec

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total3 of 29898%0 of 8100%1815914
getReferenceFrame()30%n/a111111
theoreticalEvaluation(int, int, SpacecraftState[])237100%8100%0504301
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite)55100%n/a0101401
getStation()3100%n/a010101