AbstractMeasurement

Element	Missed Instructions	Cov.	Missed Branches	Cov.	Missed	Cxty	Missed	Lines	Missed	Methods
Total	6 of 404	98%	1 of 12	91%	2	29	2	90	1	23
signalTimeOfFlight(TimeStampedFieldPVCoordinates, FieldVector3D, FieldAbsoluteDate)		0%		n/a	1	1	2	2	1	1
getCoordinates(SpacecraftState, int, int)		100%		n/a	0	1	0	16	0	1
signalTimeOfFlight(FieldPVCoordinatesProvider, FieldAbsoluteDate, FieldVector3D, FieldAbsoluteDate, Frame)		100%		75%	1	3	0	10	0	1
AbstractMeasurement(AbsoluteDate, double, double, double, List)		100%		n/a	0	1	0	10	0	1
signalTimeOfFlight(PVCoordinatesProvider, AbsoluteDate, Vector3D, AbsoluteDate, Frame)		100%		100%	0	3	0	10	0	1
AbstractMeasurement(AbsoluteDate, double[], double[], double[], List)		100%		n/a	0	1	0	10	0	1
estimateWithoutDerivatives(int, int, SpacecraftState[])		100%		100%	0	2	0	5	0	1
estimate(int, int, SpacecraftState[])		100%		100%	0	2	0	5	0	1
addModifier(EstimationModifier)		100%		n/a	0	1	0	3	0	1
signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate, Frame)		100%		n/a	0	1	0	2	0	1
signalTimeOfFlight(TimeStampedFieldPVCoordinates, FieldVector3D, FieldAbsoluteDate, Frame)		100%		n/a	0	1	0	2	0	1
addParameterDriver(ParameterDriver)		100%		n/a	0	1	0	2	0	1
signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate)		100%		n/a	0	1	0	2	0	1
getTheoreticalStandardDeviation()		100%		n/a	0	1	0	1	0	1
getBaseWeight()		100%		n/a	0	1	0	1	0	1
getObservedValue()		100%		n/a	0	1	0	1	0	1
getParametersDrivers()		100%		n/a	0	1	0	1	0	1
setEnabled(boolean)		100%		n/a	0	1	0	2	0	1
getDimension()		100%		n/a	0	1	0	1	0	1
getModifiers()		100%		n/a	0	1	0	1	0	1
isEnabled()		100%		n/a	0	1	0	1	0	1
getSatellites()		100%		n/a	0	1	0	1	0	1
getDate()		100%		n/a	0	1	0	1	0	1