作者机构:[1]Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing Institute of Technology, Beijing 100081, China, [2]Lunar Exploration and Space Program Center, China National Space Administration, Beijing 100037, China
相关基金:This work was supported by the National Basic Research Program of China ("973" Program) (Grant No. 2012CB720000), the National Natural Science Foundation qf China (Grant No. 11102021) and Foundation of Science and Technology on Space Intelligent Control Laboratory.