AngularRaDec

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 297100%0 of 6100%0804905
theoreticalEvaluation(int, int, SpacecraftState[])174100%6100%0402801
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[])88100%n/a0101501
getObservedLineOfSight(Frame)19100%n/a010201
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite)13100%n/a010301
getReferenceFrame()3100%n/a010101