期刊文献+

导弹伪攻角反馈三回路驾驶仪设计分析 被引量:27

Design and analysis of missile three-loop autopilot with pseudo-angle of attack feedback
下载PDF
导出
摘要 阐述了几种典型过载驾驶仪的结构演变过程,对传统三回路驾驶仪的结构进行了适当改进,提出了采用伪攻角作为反馈信号的三回路驾驶仪新结构。研究了驾驶仪工程指标与闭环极点之间的对应关系以及从状态反馈到输出反馈的变换技术,给出了基于输出反馈极点配置的伪攻角反馈三回路驾驶仪设计方法。研究结果表明,伪攻角反馈三回路驾驶仪消除了传统三回路驾驶仪的静差,并具有与其相似的控制特性以及鲁棒性能。分析结果显示,两种结构的三回路驾驶仪对静不稳定弹都具有较好的稳定控制性。 For several classical acceleration autopilots,the topologies evolvement is presented firstly.To improve the performance of classical three-loop autopilot,a new three-loop autopilot with pseudo-angle of attack feedback is proposed.The relation between engineering index and closed system poles and the transform technology from state feedback into output feedback are discussed,and a general design method for the new three-loop topology autopilot based on the output feedback pole assignment is proposed.It is concluded that the new three-loop autopilot can eliminate the static error of the classical three-loop topology and has some similarities of the control characteristics and robustness.Both of the new and classical three-loop autopilots can stabilize a static unstable missile very well.
出处 《系统工程与电子技术》 EI CSCD 北大核心 2012年第1期129-135,共7页 Systems Engineering and Electronics
关键词 三回路驾驶仪 结构布局 输出反馈 伪攻角反馈 静稳定性 three-loop autopilot topology output feedback pseudo-angle of attack feedback static stability
  • 引文网络
  • 相关文献

参考文献18

  • 1Mracek C P, Ridgely D B. Missile longitudinal autopilots~ comparison of multiple three loop topologies[C]//Proc, of the AIAA Guidance, Navigation, and Control Conference and Exhibit ,2005:917 - 928.
  • 2Buschek H. Design and flight test for a robust autopilot for theIRIS-T air-to-air missile [J]. Control Engineering Practice, 2003,11(1):551 - 558.
  • 3Wise K A. Robust stability analysis of adaptive missile autopi- lots[C]// Proc. of the AIAA Guidance, Navigation, and Con- trol Conference and Ecrhibit, 2008 : 539 - 544.
  • 4Min B M, Sang D, Tahk M J, et al. Missile autopilot design via output redefinition and gain optimization technique[C]// Proc. of the SICE Annual Conference ,2007:2615 - 2619.
  • 5Garnell P. Guided weapon control systems[M]. Beijing.. Beijing Institute of Technology Press, 2003 : 101 - 113,143 - 164.
  • 6Zarchan P. Tactical and strategic missile guidance[M]. 5th ed. Lexington : AIAA Incorporation, 2007: 483 - 539.
  • 7Lin Defu Fan Junfang Qi Zaikang Mou Yu.Analysis and improvement of missile three-loop autopilots[J].Journal of Systems Engineering and Electronics,2009,20(4):844-851. 被引量:10
  • 8Nesline F W, Nesline M L. How autopilot requirements con- strain the aerodynamic design of homing missiles[C]// Proc. of the American Control Conference, 1984 : 716 - 730.
  • 9Wise K A. A trade study on missile autopilot design using opti- mal control theory[C]// Proc. of the AIAA Guidance, Navi- gation, and Control Conference and Exhibit, 2007 : 816 - 838.
  • 10Mracek C P, Ridgely D B. Missile longitudinal autopilots. con- nections between optimal control and classical topologies[C]// Proc. of the AIAA Guidance, Navigation, and Control Con- ference and Ewhibit, 2005 : 698 - 727.

二级参考文献9

共引文献14

同被引文献146

引证文献27

二级引证文献50

;
使用帮助 返回顶部