This work was supported by the Chinese National Natural Science Foundation (Grant No. 51275239, 11402112), the Aerospace CAST Innovation Foundation, the Cooperative Innovation Foundation of Jiangsu Province (Grant No. 2014003-01), the Postdoctoral Science Foundation (Grant No. 20090461116), the Aviation Science Foundation (Grant No. 20125652055), the Doctor Research Foundation (Grant No. 20123218110003). We also thank the State Key Laboratory of Mechanics and Control of Mechanical Structures of Nanjing University of Aeronautics and Astronautics.
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