AngularRaDec

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total3 of 31599%0 of 8100%1816114
getReferenceFrame()30%n/a111111
theoreticalEvaluation(int, int, SpacecraftState[])249100%8100%0504501
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite)60100%n/a0101401
getStation()3100%n/a010101