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远程机动飞行器能量管控制导方法 被引量:1

Research of Energy Management and Control Strategy for Long Range Maneuvering Vehicle
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摘要 针对远程机动飞行器速度散差大幅增加、导致轨道环境显著恶化的问题,提出一种具备较强工程实用性的新型能量管控制导方法,这种方法能够实时根据飞行器能量状态给出较优的飞行轨迹方案,进而确保飞行器能以理想的终端速度和当地弹道倾角命中目标。大量仿真结果验证表明,提出的远程机动飞行器能量管控策略是合理、有效的。 In order to solve the problem of considerable velocity variability and serious flight mechanical environment for long range maneuvering vehicle,a energy management and control method which has a helpful engineering practical value is proposed.According to the proposed method,the optimal fly trajectory scheme satisfying the constraint of the given terminal velocity and trajectory obliquity can be determined based on energy state of the vehicle.The rationality and effectiveness of energy management and control strategy is demonstrated by the simulation results.
作者 童伟 贾平会 张宁 郭珂 李强 Tong Wei;Jia Ping-hui;Zhang Ning;Guo Ke;Li Qiang(Beijing Institute of Space Long March Vehicle,Beijing,100076)
出处 《导弹与航天运载技术》 CSCD 北大核心 2021年第4期88-92,共5页 Missiles and Space Vehicles
关键词 远程 能量管控 终端速度 long range energy management and control terminal velocity
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  • 1雍恩米,唐国金,陈磊.高超声速无动力远程滑翔飞行器多约束条件下的轨迹快速生成[J].宇航学报,2008,29(1):46-52. 被引量:34
  • 2Harpold J C, Graves C A. Shuttle Entry Guidance [ J ]. The Journal of the Astronautical Sciences, 1979, 37 ( 3 ) : 239 - 268.
  • 3Zumnenmm C, Dukeamm G amd Hanson, J. Automatic method to compute orbital reentry trajectories with heating constraints [ J]. Journal of Guidance, Control and Dynamics, 2003, 26 (4) : 523 -529.
  • 4Mease K D, Chen D, Teufel P and Schonenberger H. Reduced-order entry trajectory planning for acceleration guidance[ J ]. Journal of Guidance, Control and Dynamics, 2002, 25 (2) : 257 - 266.
  • 5Roenneke A J. Adaptive onboard guidance for entry vehicle [ C ]// Proceedings of the A1AA Guidance, Navigation, and Control Conference, AIAA, Reston, VA, 2001.
  • 6Bollino K, Ross M. Optimal nonlinear feedback guidance for reentry vehicles [ C ]. AIAA Guidance, Navigation, and Control Conference and Exhibit, Keystone, Colorado, Aug. 21 -24, 2006. AIAA - 2006 - 6074.
  • 7Shen Z, Lu P. Onbooard generation of three-dimensional constrained entry trajectories[ J]. Journal of Guidance, Control and Dynamics, 2003, 26( 1 ) : 110 - 121.
  • 8Vinh N X, Busemann A, Culp R D. Hypersonic and Planetary Entry Flight Mechanics, Univ. of Michigan Press, Ann Arbor, M1, 1980:26-27.
  • 9Corporation T P. A Common Aero Vehicle Model, Description and Employment Guide [ EB/OL]. [ 2003 ] http://www, dtic Mil/matris/sbir/sbit041 srch/af031 a. doc.
  • 10沈作军.航天器先进再人制导技术研究综述[C]//中国宇航学会首届学术会议论文集.北京:宇航出版社,2005:103-104.

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