698 39,., [6].,,,, : 1) ; 2) ,, 14,, [7].,,,,, : 1) :,. 2) :,,, 3) :,,,., [8].,. 1.,,,, ,,,. : 1) :,, 2) :,, 200, s, ) :,.

39 6 Vol. 39, No. 6 2013 6 ACTA AUTOMATICA SINICA June, 2013 1, 2,,,. DOI,,,., 2013, 39(6): 697 702 10.3724/SP.J.1004.2013.00697 Present Situation and Development Tendency of Aerospace Control Techniques BAO Wei-Min 1, 2 Abstract This paper summarizes the current issues and challenges of aerospace control techniques, and generalizes the basic problems and key technologies of launch vehicles and aerospace flights in the next generation. And it analyzes the research progresses of aerospace control at present stage. Moreover, it proposes some suggestions of development of aerospace control in the future. Key words Aerospace craft, control, launching vehicle, dynamics Citation BAO Wei-Min. Present situation and development tendency of aerospace control techniques. Acta Automatica Sinica, 2013, 39(6): 697 702,., [1].,,,, ( ) [2]. [3 4] : (National Aeronautics and Space Administration, NASA) 2002 (Space launch initiative, SLI), ; 2013-01-10 2013-01-14 Manuscript received January 10, 2013; accepted January 14, 2013 Recommended by Academician HUANG Lin 1. 100048 2. 100871 1. China Aerospace Science and Technology Corporation, Beijing 100048 2. College of Engineering, Peking University, Beijing 100871 (Expendable launch vehicle, ELV) (Reusable launch vehicle, RLV) ; 2010 : 2025 ; 2030 30, [5] : (X-37B),,, ;, (Apollo) (Crew exploration vehicle, CEV), 2013 7,,, (MAKS),. (Intermediate experimental vehicle, IXV),, 2012,,

698 39,., [6].,,,, : 1) ; 2) 1 1.1 40,, 14,, [7].,,,,, : 1) :,. 2) :,,, 3) :,,,., [8].,. 1.,,,, 2. 1.2,,,. : 1) :,, 2) :,, 200, 3 000 s, 1 000. 3) :,. 4) :,, RCS (Reaction control system), V,,. 5) :,,,,.,,,,, 3.,,,, 1.,,

6 : 699 1 Fig. 1 Noncoplanar transfer,, 80, 4.,,. 5. 6.,, (Guidance navigation control, GNC) 2 : 1) 2),,. 3), 4),,. 5),. 6)

700 39, 10, 4 ;,,,. 7),,. 8),,.. 3 3.1 60, (Powered explicit guidance, PEG), 70,,, 3.2 20 50,, 20 70,,., 20 90, NASA 1999 X-33 (Advanced guidance and control, AGC), : 1) : (Baseline guidance) (Linear quadratic regulator, LQR) (Evolved acceleration guidance logic for entry, EAGLE). 2) : 3) :,,,,,. 3.3,,,,,,,,, 2., Apollo, : NASA NSEG Draper PredGuid,. 3.4,

6 : 701,,.,, X-37B HTV-2 [10]. 4 2 Fig. 2 Skip entry trajectory.,,,,,. 3 X-43A. 3.5,,, + RCS RCS +, ;., : 1), NASA,,,,,,,,, 3 X-43A Fig. 3 Control structure of X-43A

702 39. 2) HTV-2 : HTV-2, ; :,,,,,, (Integrated product design, IPD). 3),,,. 4),,,,,. 5,,,, References 1 Wang Xiao-Dong. Prospect and review of attitude stabilization and control technology development for missile and launch vehicle. Missiles and Space Vehicles, 2003, (3): 25 30 (.., 2003, (3): 25 30) 2 Wang Ya-Xun. A logic space transportation strategy. Journal of Rocket Propulsion, 2004, 30(1): 58 64 (., 2004, 30(1): 58 64) 3 Jiang Shao-Dong, Han Hong-Shuo. A survey of current RLV concepts in the U.S.. Aerospace China, 2004, (5): 21 25 (,., 2004, (5): 21 25) 4 Jiang Shao-Dong, Han Hong-Shuo. A survey of current RLV concepts in Europe. Aerospace China, 2004, (6): 25 31 (,., 2004, (6): 25 31) 5 He Xia. The hypersonic technology development plan in the U.S.. Modern Military, 2004, (12): 26 28 (., 2004, (12): 26 28) 6 Yang Yong. Study on roadmap of Chinese reusable launch vehicle. Missiles and Space Vehicles, 2006, (4): 1 4 (., 2006, (4): 1 4) 7 Long Le-Hao, Wang Xiao-Jun, Guo Lin-Li. The present situation and prospect of China s space-entering capacity. Engineering Science, 2006, 8(11): 25 32 (,,., 2006, 8(11): 25 32) 8 Lu Ping, Jing Zhong-Liang, Hu Shi-Qiang. Key technologies on advanced guidance and control for sustainable development of manned space flight. Manned Spaceflight, 2011, 17(5): 25 32 (,,.., 2011, 17(5): 25 32) 9 Guo Lin-Li, Shen Lin, Yang Yong, Hu De-Feng. Study on the development strategy for China space transportation system. Missiles and Space Vehicles, 2006, (1): 1 5 (,,,.., 2006, (1): 1 5) 10 Li Su-Xun. Progress in aerodynamics of combination control for vehicles at high speed. Advances in Mechanics, 2009, 39(6): 740 755 (.., 2009, 39(6): 740 755),.,,. E-mail: baoweimin@cashq.ac.cn (BAO Wei-Min Academician of Chinese Academy of Sciences, professor at the China Aerospace Science and Technology Corporation. His research interest covers flight control, aerospace crafts, and launch vehicles.)