AngularRaDec

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 326100%0 of 6100%0905406
theoreticalEvaluation(int, int, SpacecraftState[])186100%6100%0402901
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[])95100%n/a0101601
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite)20100%n/a010501
getObservedLineOfSight(Frame)19100%n/a010201
getReferenceFrame()3100%n/a010101
getStation()3100%n/a010101