期刊文献+

L_1自适应方法在无人战斗机纵向控制中的应用 被引量:3

Longitudinal Controller for UCAV Based on L_1 Adaptive Control Theory
下载PDF
导出
摘要 无人战斗机在空中飞行时,由于各方面因素导致战斗机模型具有大量的不确定性。本文在进行无人机纵向控制设计时,为了提高控制系统的鲁棒性能,采用一种新型的L1自适应控制方法,将无人战斗机模型的不确定性视为时变参数和干扰。最后对所设计的控制系统进行了仿真,结果表明所设计的控制器可使跟踪误差快速收敛且瞬态性能较好。 When the UCAV do maneuver in the air, due to various factors the UCAV has a great un certainty. To improve the robustness during designing longitudinal controller of UCAV, this paper uses a novel L1 adaptive control theory and treats the UCAV model uncertainty as timevarying parameters and in terference. Finally, the simulation results show that the controller can make the tracking error fast conver gence and has good transient performance.
作者 鲁可 袁锁中
出处 《航空兵器》 2013年第5期36-39,共4页 Aero Weaponry
基金 南京航空航天大学基本科研业务费专项科研项目基金(No.V1083-031)
关键词 无人战斗机 纵向控制器 L1自适应控制 不确定性 瞬态性能 unmanned combat air vehicle longitudinal controller L1 adaptive control uncertainty transient performance
  • 相关文献

参考文献10

  • 1Kulczycki E A, Joshi S S, Hess R A, et al. Towards Con- troller Design for Autonomous Airships Using SLC and LQR Methods [ C ]//AIAA Guidance, Navigation, and Control Conference and Exhibit, 2006. Keystone, Colo- rado, AIAA 2006 - 6778.
  • 2江琼,陈怀民,吴佳楠.H_∞鲁棒控制与PID控制相结合的无人机飞行控制研究[J].宇航学报,2006,27(2):192-195. 被引量:20
  • 3Frye M T, Colgren R D. A QFT Based Control Design for the Wraith UAV [ C ]// AIAA Guidance, Navigation, and Control Conference and Exhibit, 2008. Honolulu, Hawai- i, AIAA 2008 - 6486.
  • 4Sharma M, Farrell J A. Backstepping Flight Control Using On-Line Function Approximation [ C ]// AIAA Guidance, Navigation, and Control Conference and Exhibit, 2003. Austin, Texas, AIAA 2003 - 5713.
  • 5黄显林,王海斌,周建锁,胡恒章.空间飞行器基于模糊逻辑的连续滑模控制[J].宇航学报,1999,20(2):22-27. 被引量:5
  • 6Enomoto K, Yamasaki T, Takano H, et al. A Study on a Velocity Control System Design Using the Dynamic Inver- sion Method [ C ]// AIAA Guidance, Navigation, and Control Conference, 2010. Toronto, Ontario Canada, AIAA 2010 - 8204 : 563 - 568.
  • 7Cao C, Hovakimyan N. Design and Analysis of a Novel L1 Adaptive Controller, Part 1 : Control Signal and Asymptot- ic Stability [ C ]//American Control Conference, Inst. of Electrical and Electronics Engineers, Piscataway, N J, 2006:3397 - 3402.
  • 8Cao C, Hovakimyan N. Design and Analysis of a Novel L1Adaptive Controller, Part 2: Guaranteed Transient Per- formanee [ C ]//American Control Conference, Inst. of E- lectrical and Electronics Engineers, Piscataway, N J, 2006, :3403 - 3408.
  • 9Wang J, Patel V V, Cao C, et al. L1 Adaptive Neural Network Controller for Autonomous Aerial Refueling with Guaranteed Transient Performance [ C ]//AIAA Guid- ance, Navigation, and Control Conference, 2006, Key- stone, Colorado, AIAA 2006 - 6206.
  • 10Lei Y, Cao C, Cliff E, et al. Design of an L1 Adaptive Controller for Air - Breathing Hypersonic Vehicle Model in the Presence of Unmodeled Dynamics [ C ]//Proc. AIAA Guidance, Navigation and Control Conf. 2007.

二级参考文献4

  • 1Hwang G C,Fuzzy Sets Systems,1992年,48卷,279页
  • 2申铁龙.H∞控制理论及应用[M].北京:清华大学出版社,1994
  • 3Bernstein D S.LQG control with an H∞ performance bound:Riccati equation approach[J].IEEE Tran.Auetern.Control,1989,34(4):293-305
  • 4Barmish B R.Stablilization of uncertain systems via linear control[J].IEEE trans Auton.Control.1983 28(8):848-850

共引文献23

同被引文献22

引证文献3

二级引证文献14

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