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 (8th ed.) CitationOptimal Control of the Attitude Maneuvering for Razaksat Class Satellite Based on Rigid and Flexible Model.
Warning: These citations may not always be 100% accurate.