期刊文献+

基于自适应幂次切换增益的动能拦截滑模制导律 被引量:1

Adaptive Power Switching Gain based Sliding-Mode Guidance Law for Kinetic Energy Intercept
下载PDF
导出
摘要 抖振问题限制了非线性变结构制导的应用。运用幂函数作为切换增益函数并设计全局鲁棒的滑模,构成自适应趋近律,实现切换线平滑趋近,形成基于自适应幂次切换增益的滑模制导律AP-SMG。给出其存在可达与稳定条件,并对空间目标的非机动和脉冲/连续机动环境作了仿真比较与参数分析。结果表明该制导律在动能拦截中可以有效削弱甚至消除视线角速率和控制律抖振,降低所需控制能量的同时能够保证制导精度,构造简单,无需智能结构辅助,总体性能优于基于常值切换增益的系列制导方法C-SMG。 Chattering restricts the application of nonlinear variable structure guidance law. Through designed an adaptive trending law, consisted of a switching gain with power function and a global robust sliding mode, to smoothly approach switching surfaces, here provided a new sliding-mode method with adaptive power switching gain (AP-SMG). Sliding mode existence, reachability and system stability were analyzed. SIMULINK simulation and parameter analysis were also made under exo-atmosphere intercept conditions with non-maneuvering and impulse/continuous maneuvering target. As a result, chattering of LOS velocity and control law can be effectively decreased even disappeared in kinetic energy intercept. Simultaneously, guidance precision is desired and control energy needed is declined. Without any assisted intelligent structure, the overall performances of APSMG are better than constant switching gain based guidance method (C-SMG).
出处 《宇航学报》 EI CAS CSCD 北大核心 2008年第6期1792-1797,共6页 Journal of Astronautics
基金 国家863项目(2006AA704314) 国家自然科学基金项目(60775022) 国家自然科学基金项目(60674107)
关键词 变结构 自适应 切换增益 制导律 动能拦截 Variable structure Adaptive Switching gain Guidance law Kinetic energy intercept
  • 相关文献

参考文献8

  • 1Slotine J J, Sastry S S. Tracking control of nonlinear systems using sliding surfaces with application to robot manipulator[J]. International Journal of Control, 1983, 38(2) : 465 - 492.
  • 2Hwang C L. Sliding mode control using time-varying switching gain and boundary layer for electro- hydraulic position and differential pressure control[J]. IEE Proceedings Control Theory and Applications, 1996, 143(4) :325- 332.
  • 3Wong L J, Leung F H F, Tam P K S. A chattering elimination algorithm for sliding mode control of uncertain non-linear systems [ J]. 1998, 77(8) : 765- 775.
  • 4Lin F J, Wai R J. Sliding-mode-controlled slider-crank mechanism with fuzzy neural network [J]. IEEE Transactions on Industrial Electronics, 2001, 48(1) : 60 - 70.
  • 5Lu Y S, Chen J S. Design of a global sliding-mode controller for a motor drive with bounded control [J]. International Jounlal of Control, 1995, 62(5) : 1001 - 1019.
  • 6Choi H S, Park Y H, Cho Y S, Lee M H. Global sliding mode control [J]. IEEE Control Systems Magazine, 2001, 21(3) : 27 - 35.
  • 7ZHOU Di, MU Chun-di, et al. Adaptive sliding-mode guidance of a homing missile [J]. Journal of Guidance, Control and Dynamics, 1999, 22(4) : 589 - 594.
  • 8周获.寻的导弹新型导引规律[M].北京:国防工业出版社,2002.

共引文献6

同被引文献10

  • 1Zarchan P.Proportional navigation and weaving targets[J].Journal of Guidance and Control,1995,18(5):969-974.
  • 2Chadwick W R,Zarchan P.Interception of spiraling ballistic missiles[C].Proceedings of the American Control Conference,Washington,1996:4476-4483.
  • 3Zarchan P,Alpert J.Using filter banks to improve interceptor performance against weaving targets[C].AIAA Guidance,Navigation,and Control Conference and Exhibit,Keystone,Colorado,2006.
  • 4Marks G M.Multiple model adaptive estimation (MMAE) based filter banks for interception of maneuvering targets[C].AIAA Guidance,Navigation and Control Conference and Exhibit,Hilton Head,South Carolina,2007.
  • 5Shima T,Shinar J.Time-varying linear pursuit-evasion game models with bounded controls[J].Journal of Guidance,Control,and Dynamics,2002,25(3):425-432.
  • 6Shima T,Shinar J,Weiss H.New interceptor guidance law integrating time-varying and estimation-delay models[J].Journal of Guidance,Control,and Dynamics,2003,26(2):295-303.
  • 7Shima T,Idan M,Golan M O.Sliding-mode control for integrated missile autopilot guidance[J].Journal of Guidance,Control,and Dynamics,2006,29(2):250-260.
  • 8Zarchan P.Tracking and intercepting spiraling ballistic missiles[C].Proceedings of IEEE PLANS Conference,San Diego,CA,2000.
  • 9Gutman S.On optimal guidance for homing missiles[J].Journal of Guidance and Control,1979,2(4):296-300.
  • 10朱隆魁,汤国建,余梦伦.一种大气层内拦截弹自适应滑模制导律研究[J].飞行力学,2008,26(3):64-67. 被引量:2

引证文献1

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