PositionMeasurement

Element	Missed Instructions	Cov.	Missed Branches	Cov.	Missed	Cxty	Missed	Lines	Missed	Methods
Total	0 of 224	100%	0 of 2	100%	0	10	0	20	0	9
static {...}		100%		n/a	0	1	0	1	0	1
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[], boolean)		100%		100%	0	2	0	6	0	1
PositionMeasurement(AbsoluteDate, Vector3D, double[], double, ObservableSatellite)		100%		n/a	0	1	0	2	0	1
PositionMeasurement(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite)		100%		n/a	0	1	0	2	0	1
PositionMeasurement(AbsoluteDate, Vector3D, double, double, ObservableSatellite)		100%		n/a	0	1	0	2	0	1
theoreticalEvaluation(int, int, SpacecraftState[])		100%		n/a	0	1	0	3	0	1
PositionMeasurement(AbsoluteDate, Vector3D, MeasurementQuality, ObservableSatellite)		100%		n/a	0	1	0	2	0	1
getPosition()		100%		n/a	0	1	0	1	0	1
getMeasurementType()		100%		n/a	0	1	0	1	0	1