Rugged

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total64 of 1,40295%9 of 4278%124812277327
directLocation(AbsoluteDate, Vector3D, Vector3D)2519888%3770%3644501
directLocation(String, double)2423990%21083%2734701
isInRange(AbsoluteDate)50%n/a111111
inverseLocationDerivatives(String, GeodeticPoint, int, int, DSGenerator)419197%2250%2323701
getAlgorithm()30%n/a111111
getRefractionCorrection()30%n/a111111
inverseLocation(String, GeodeticPoint, int, int)183100%4100%0303701
distanceBetweenLOSderivatives(LineSensor, AbsoluteDate, double, SpacecraftToObservedBody, LineSensor, AbsoluteDate, double, DSGenerator)164100%n/a0103001
distanceBetweenLOS(LineSensor, AbsoluteDate, double, SpacecraftToObservedBody, LineSensor, AbsoluteDate, double)135100%n/a0102601
Rugged(IntersectionAlgorithm, ExtendedEllipsoid, boolean, boolean, AtmosphericRefraction, SpacecraftToObservedBody, Collection, String)52100%2100%0201401
getPlaneCrossing(String, int, int)40100%2466%240801
dateLocation(String, GeodeticPoint, int, int)28100%2100%020701
getLineSensor(String)21100%2100%020401
dateLocation(String, double, double, int, int)18100%n/a010301
inverseLocation(String, double, double, int, int)18100%n/a010301
setPlaneCrossing(SensorMeanPlaneCrossing)9100%n/a010201
getScToInertial(AbsoluteDate)5100%n/a010101
getInertialToBody(AbsoluteDate)5100%n/a010101
getBodyToInertial(AbsoluteDate)5100%n/a010101
getLineSensors()4100%n/a010101
getMinDate()4100%n/a010101
getMaxDate()4100%n/a010101
getName()3100%n/a010101
isLightTimeCorrected()3100%n/a010101
isAberrationOfLightCorrected()3100%n/a010101
getEllipsoid()3100%n/a010101
getScToBody()3100%n/a010101