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风标头的动力学在系统分析中的作用(英文) 被引量:2

Effect of Aerodynamically Stabilized Seeker Dynamics on System Analysis
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摘要 目的 研究风标头的动力学在制导航弹系统分析中的作用. 方法 对风标头的动力学进行分析,由于其时间常数很小,因此其动力学模型可大大简化. 结果与结论 在进行全弹的动力学仿真时,由于与弹体动力学相比风标头的时间常数很小,因此可采用其简化模型计算而不影响仿真的精度. Aim To study the effect of aerodynamically stabilized seeker dynamics on guided bomb system analysis. Methods A thorough analysis of aerodynamically stabilized seeker dynamics was made to show that because of the much smaller time constant, its dynamic model can be greatly simplified. Results and Conclusion In guided bomb guidance/control digital simulation, with the use of the simplified seeker model, simulation time can be reduced without the loss of simulation accuracy.
出处 《Journal of Beijing Institute of Technology》 EI CAS 1999年第4期437-442,共6页 北京理工大学学报(英文版)
关键词 制导航弹 风标头 局部气流 失调角 guided bomb aerodynamically stabilized seeker local air dislocation angle
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同被引文献7

  • 1袁子怀 钱杏芳.有控飞行力学与计算机仿真(第一版)[M].北京:国防工业出版社,2001.1-28,38-82,187-326.
  • 2Garnell P. Guided weapon control system [M]. England: Pergammon Press Ltd., 1980.
  • 3Xia Qun-li. Study of laser-guided bomb dynamics and its trajectory optimization [D]. Beijing: School of Mechano-Electronics Engineering, Bei-jing Institute of Technology, 1999.
  • 4Xia Qun-li, Qi Zai-kang. Aerodynamic Interpolation for Flight Vehicles with Aerodynamic Axial-Asymmetry. [J]. Journal of Beijing Institute of Technology, 1999, 12 (4):430-436.
  • 5Xia Qun-li, Qi Zai-kang. Lin De-fu, The flight range optimization of Extended Range Guided Munitions (ERGM) [J]. Journal of Beijing Institute of Technology, 2002, 12 (4):437-442.
  • 6张求知 李克己.激光制导炸弹的火控原理及应用.电光与控制,2000,4:29-35.
  • 7金光军,王仕成,刘志国.激光制导炸弹仿真建模研究[J].航空兵器,2002,9(6):4-7. 被引量:7

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