期刊文献+

无人机数据链变结构对抗攻击导引方式研究 被引量:4

UAV Data Links Variable Structure Against Attacks Guidance Law Research
下载PDF
导出
摘要 无人机在快速接敌的过程中,传统的导引方法很容易将无人机导引到敌机的火力攻击范围之内。而且传统比例导引法系数的最优解与目标和载机的距离有关,一旦目标机动或存在干扰,跟踪效果都会变差。为此提出了一种基于数据链的无人机变结构对抗攻击导引方式,并进行仿真研究。仿真结果表明,该方法不仅避免把无人机导引到敌机的火力攻击范围之内,而且减小了无人机所需过载,提高了制导精度、速度和鲁棒性,限制了视线角速度。 In the course of UCAV approach to the enemy plane, tradition proportion guidance law is easy to let our plane into the scopes of target fire attack. And the beast coefficient of tradition proportion lead law is related to the target and UCAV's distance, If the target moves with high acceleration or is disturbed, the attack result will become bad. For resolving these questions, a method was given based on data link variable structure adaptive opposed guidance law and make a simulation was made, The simulation result shows that the method not only evades guidance ourplane into targetfire attack scope, but also reduces the overload of the UCAV, improves guiding precision, velocity and robust, restricts the line of sight angle's speed.
出处 《系统仿真学报》 CAS CSCD 北大核心 2008年第13期3507-3509,3513,共4页 Journal of System Simulation
关键词 数据链 无人机 对抗 导引律 变结构 data link UCAV opposed leading law variable structure
  • 相关文献

参考文献3

二级参考文献19

  • 1曾颖超 陆敏峰.战术导弹弹道与姿态动力学[M].西安:西北工业大学出版社,1991.172-194.
  • 2Guelman M. A Qualitative Study of Proportional Navigation[J]. IEEE Transaction on Aerospace and Electronic Systems, 1971, AES-7(4):637-643.
  • 3Becket K. Closed-form Solution of Pure Proportional Navigation[J].IEEE Transitions on Aerospace and Electronic Systems, 1990,AES-26(3): 526-532.
  • 4Ravindra If., BabuI G S, Swamy K N. Switched Biased Proportional Navigation for Homing Guidance Against Highly Maneuvering Targets[J]. Journal of Guidance, Control and Dynamics, 1994, 17(6):1357-1363.
  • 5Yuau P J, Chern J S. Ideal Proportional Navigation[J], Journal of Guidance, Control and Dynamics, 1992, 15(5): 1161 - 1165.
  • 6Shinar J, Guelman M ,Green A. An Optimal Guidance Law for a Planar Pursuit-evasion Game of Kind[J]. Computers and Mathematics with Applications, 1989, 18(1-3): 35-44.
  • 7刑继祥 张春蕊.最优控制应用基础[M].北京:科学出版社,2003..
  • 8吴文海.[D].南京:南京航空航天大学,2003.
  • 9李延杰.防空导弹系统射击指挥[M].北京:北京航空学院出版社,1987..
  • 10张有济.战术导弹飞行力学设计[M].北京:宇航出版社,1996..

共引文献27

同被引文献34

引证文献4

二级引证文献13

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部