Optimal control of the attitude maneuvering for Razaksat class satellite based on rigid and flexible model.
Chicago Style (17th ed.) CitationOptimal Control of the Attitude Maneuvering for Razaksat Class Satellite Based on Rigid and Flexible Model.
MLA引文Optimal Control of the Attitude Maneuvering for Razaksat Class Satellite Based on Rigid and Flexible Model.
警告:这些引文格式不一定是100%准确.