TDOA

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 360100%0 of 14100%01205805
theoreticalEvaluation(int, int, SpacecraftState[])209100%10100%0603301
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[])121100%4100%0301701
TDOA(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite)24100%n/a010601
getPrimeStation()3100%n/a010101
getSecondStation()3100%n/a010101