[1] Durham W C. Constrained controller allocation. Journal of Guidance, Control and Dynamics, 1993, 16(4): 717-725.[2] Arun Kishore W C, Sen S, Ray G. Dynamic control allocation for tracking time varying control demand. Journal of Guidance, Control, and Dynamics, 2008, 31(4): 1150-1157.[3] Johannes T, Johansed T. Adaptive control allocation. Automatica, 2008, 44(11): 2754-2765.[4] Luca Z. Dynamic allocation for input redundant control systems. Automatica, 2009, 45(2): 1431-1438.[5] Ning G D, Zhang S G, Fang Z P. Entry control allocation using sliding modes and state observer synthesis for reusable launch vehicl. Journal of Astronautics, 2007, 28(1): 69-76. (in Chinese) 宁国栋, 张曙光, 方振平. 可重复使用航天器基于状态估计的再入飞行滑模控制器设计研究. 宇航学报, 2007, 28(1): 69-76.[6] Ola H. Resolving actuator redundancy-optimal control allocation. Automatica, 2005, 41(1): 137-144.[7] Durham W C, Bordgon K A. Multiple control effectors rate limiting. Journal of Guidance, Control, and Dynamics, 1996, 19(1): 30-37.[8] Buffington J, Chandler P, Pachter M. On-line system identification for aircraft with distributed control effectors. International Journal of Robust and Nonlinear Control, 1995, 9(14): 1033-1049.[9] Bodson M, Frost S A. Control allocation with load balancing. AIAA Guidance, Navigation, and Control Conference, 2009.[10] Bodson M. Evaluation of optimization methods for control allocation. Journal of Guidance, Control, and Dynamics, 2002, 25(4): 703-711.[11] Potra F, Wright S. Interior-point methods. Journal of Computational and Applied Mathematics, 2000, 124(1): 281-302.[12] Peterson J A M, Bodson M. Constrained quadratic programming techniques for control allocation. IEEE Transactions on Control Systems Technology, 2006, 14(1): 91-98.[13] Lu P. Constrained tracking control of nonlinear systems. Systems & Control Letters, 1996, 27(3): 305-314.[14] Fletcher R. Practical methods of optimization. 2rd ed. New York: JohenWiley & Sons, 2000: 76-83.[15] Wang Z G, Luo S B, Wu J J. Research on reusable launch vehicle. Changsha: National University of Defense Technology Press, 2004: 5-45. (in Chinese) 王振国, 罗世彬, 吴建军. 可重复使用运载器研究进展. 长沙: 国防科技大学出版社, 2004: 5-45.[16] Crocker A M, Andrews D G. Go horizontal: a responsible, evolvable, feasible space launch roadmap. AIAA-2004-6004, 2004.[17] Wallace J G, Bradford J, Charania A C, et al. Concept study of an ARES hybrid-OS launch system. AIAA-2006-8057, 2006.[18] Kauffmann J. Future European launch systems in the FLPP overview and objectives. 57th International Astronautical Congress, 2006.[19] Tomatis C, Bouaziz L, Franck T, et al. RLV candidates for European future launchers preparatory programme. Acta Astronautica, 2009, 65(1): 40-46.[20] Sippel M, Manfletti C, Burkhardt H. Long-term/strategic scenario for reusable booster stages. Acta Astronautica, 2006, 58(4): 209-221.[21] Nakano M M, Willms R J. Space shuttle on-orbit flight control system. AIAA-1982-1576, 1982.[22] Singla P. Multi-resolution methods for high fidelity modeling and control allocation in large scale dynamical systems. Ann Arbor: Department of Aerospace Engineering,Texas A&M University, 2006.[23] Burken J J, Lu P, Wu Z, et al, Two reconfiurable flight control design methods: robust servomechanism and control allocation. Journal of Guidance, Control, and Dynamics, 2001, 24(3): 482-493.[24] Wang J, Longoria R G. Coordinated vehicle dynamics control with control distribution. Proceedings of the 2006 American Control Conference, 2006: 5348-5353.[25] Mercer A M, Mercer P R. Cauchy’s interlace theorem and lower bounds for the spectral radius. Internetional Journal of Mathematics and Mathematical Sciences, 2000, 23(8): 563-566.[26] Xu J T. Research on attitude control and control allocation for reusable boosted vehicle. Harbin: School of Aeronautics, Harbin Institute of Technology, 2010. (in Chinese) 许江涛. 可重复使用助推飞行器姿态控制和控制分配研究. 哈尔滨: 哈尔滨工业大学航天学院, 2010. |