AbstractOrbitInterpolator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 113100%0 of 8100%0902205
checkOrbitsConsistency(Collection)75100%6100%0401201
checkFrameIsInertial(Frame)16100%2100%020301
AbstractOrbitInterpolator(int, double, Frame)11100%n/a010401
interpolate(AbsoluteDate, Collection)8100%n/a010201
getOutputInertialFrame()3100%n/a010101