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固体冲压发动机+BTT导弹一体化设计问题讨论 被引量:3

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摘要 介绍了固体冲压发动机的主要性能,分析了BTT控制的起因、优点以及要解决的问题,最后通过讨论导弹总体设计和发动机设计的相互制约和相互影响,研究了固体冲压发动机+BTT控制的空空导弹一体化设计问题。
出处 《航空兵器》 2002年第6期17-20,共4页 Aero Weaponry
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参考文献9

二级参考文献17

  • 1刘同仁.用参数最优化方法计算最优飞行轨迹[J].航空学报,1994,15(11):1298-1305. 被引量:13
  • 2王志刚,严辉,陈士橹.轨迹/飞行器总体参数的一体化优化方法研究[J].飞行力学,1997,15(2):19-26. 被引量:6
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共引文献78

同被引文献13

  • 1刘同仁.用参数最优化方法计算最优飞行轨迹[J].航空学报,1994,15(11):1298-1305. 被引量:13
  • 2王志刚,严辉,陈士橹.轨迹/飞行器总体参数的一体化优化方法研究[J].飞行力学,1997,15(2):19-26. 被引量:6
  • 3Mracek Curtis P,Ridgely D Brett.Missile longitudinal autopilots:connections between optimal control and classical topologies[C]// AIAA Guidance,Navigation,and Control Conference and Exhibit.San Francisco:AIAA,2005:6381
  • 4Lee C H,Chung M J.Gain-scheduled state feedback control design technique for flight vehicles[J].IEEE Transactions on Aerospace and Electronic Systems,2001,37(4):173-182
  • 5Unnikrishnan Nishant,Balakrishnan S N.Dynamic reoptimization of a missile autopilot controller in presence of unmodeled dynamics[C]// AIAA Guidance,Navigation,and Control Conference and Exhibit.San Francisco:AIAA,2005:6387
  • 6Chris M M,Zhu J J.Bank-to-turn roll-yaw-pitch autopilot design using dynamic nonlinear inversion and PD-eigenvalue assignment[C]// Proceeding of the American Control Conference.Chicago:AIAA,2000:1359-1364
  • 7Lee S Y,Lee J I,Ha I J.Nonlinear autopilot for high maneuverability of bank-to-turn missiles[J].IEEE Transactions on Aerospace and Electronic Systems,2001,37(4):1236-1253
  • 8Sastry S.Nonlinear systems:analysis,stability,and control[M].New York:Springer-Verlag,1999:398-402
  • 9张家骅,胡顺楠,顾炎武,曹中俄.整体式固体火箭冲压发动机研制[J].推进技术,1998,19(2):9-13. 被引量:21
  • 10胡朝江,陈士橹.敏捷性管理系统优化设计[J].航空学报,2002,23(1):79-81. 被引量:1

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