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高超声速飞行器滑翔制导方法综述 被引量:8

A survey of gliding guidance methods for hypersonic vehicles
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摘要 阐明高超声速飞行器滑翔制导的基本问题,分析滑翔制导过程面临的复杂多约束、机动任务要求、参数扰动等研究难点;分别就国内外标准轨迹制导方法和预测-校正制导方法相关研究现状展开综述,指出了这两类方法中存在的问题。在此基础上,提出高超声速飞行器滑翔制导研究中亟待解决的关键问题,并指出未来滑翔制导方法的研究热点。 The basic problem of gliding guidance for hypersonic vehicles was proposed, and the difficulties of complicated multiple constraints, maneuver requirements, and parameter perturbation in the course of gliding guidance were analyzed. The corresponding research status at home and abroad was surveyed, and the problems were also pointed out. On this basis, the key problems required to be solved at present in the research of gliding guidance for hypersonic vehicles were presented, and the research hotspots in the methods of future gliding guidance were also pointed out. 
出处 《国防科技大学学报》 EI CAS CSCD 北大核心 2017年第3期15-22,共8页 Journal of National University of Defense Technology
基金 国家自然科学基金资助项目(11502289)
关键词 高超声速飞行器 滑翔制导 标准轨迹制导 预测-校正制导 综述 hypersonic vehicle gliding guidance standard trajectory guidance predictor corrector guidance survey
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  • 1闫晓东,唐硕.亚轨道飞行器返回轨道设计方法研究[J].宇航学报,2008,29(2):467-471. 被引量:18
  • 2任章,袁国雄.轨道武器战斗舱再入制导技术研究[J].航天控制,2005,23(2):4-7. 被引量:10
  • 3郑立伟,荆武兴,张燕.基于高斯问题的近最优再入预测制导方法研究[J].航天控制,2006,24(1):39-42. 被引量:4
  • 4Shen Zuojun, Lu Ping. On-board entry trajectory planning ex- panded to sub-orbital flight [ R]. AIAA-2003-5736,2003.
  • 5Hahn P V, Frederick R A, Slegers N. Predictive guidance of a projectile for hit-to-kill interception [ J ]. Control Systems Tech- nology, 2009,17 (4) :745 - 755.
  • 6赵汉元.飞行器再入动力学和制导[M].长沙:国防科技大学出版社,1997..
  • 7Harpold J C, Graves C A. Shuttle entry guidance[J]. J of Astronautical Sciences, 1979, 27(3): 239-268.
  • 8Harpold J C, Gavert D E. Space shuttld entry guidance performance results[J]. J of Guidance, Control, and Dynamics, 1983, 6(6): 442-447.
  • 9Zimpfer D, Hattis P, Ruppert J, et al. Space shuttle GN&C development history and evolution[C]. AIAA Space 2011 Conf & Exposition. California, 2011.
  • 10Mease K D, Chen D T, Teufel P, et al. Reduced-Order entry trajectory planning for acceleration guidance[J]. J of Guidance, Control, and Dynamics, 2002, 25(2): 257-266.

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