AngularRaDec

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total3 of 34299%0 of 8100%1916215
getReferenceFrame()30%n/a111111
theoreticalEvaluation(int, int, SpacecraftState[])258100%8100%0504501
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], int)68100%n/a0101301
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[])10100%n/a010201
getStation()3100%n/a010101