[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

弹箭与制导学报 >

2010 , Vol. 30 >Issue 4: 26 - 28

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.04.016

导弹与制导技术

高超声速飞行器再入分数阶PIDμDν姿态控制

  • 秦昌茂 ,
  • 齐乃明
展开
  • 哈尔滨工业大学航天工程系,哈尔滨 150001

秦昌茂(1985-),男,江西人,博士研究生,研究方向:高超声速飞行器制导与控制。

收稿日期: 2009-08-23

  网络出版日期: 2025-05-28

收起

Fractional-order PIDμDν Attitude Controller for Hypersonic Missile in Reentry

  • QIN Changmao ,
  • QI Naiming
Expand
  • Aerospace Engineering Department, Harbin Institute of Technology, Harbin 150001, China

Received date: 2009-08-23

  Online published: 2025-05-28

Fold

摘要

针对高超声速飞行器再入过程中气动环境参数的剧烈变化,文中结合分数阶PIDμDν控制器(FOC)Tustin+CFE数字实现法的10阶近似模型,通过ITAE指标寻优整定FOC参数并应用于某型飞行器的姿态控制。Simulink仿真结果表明,FOC控制器具有比传统PID控制器更好的控制效果,并且在气动参数剧烈变化的情况下,FOC控制器具有更强的鲁棒性。

关键词： 分数阶 PIDμDν控制器; 姿态控制; ITAE最优; Tustin+CFE

本文引用格式

秦昌茂 , 齐乃明 . 高超声速飞行器再入分数阶PIDμDν姿态控制[J]. 弹箭与制导学报, 2010 , 30(4) : 26 -28 . DOI: 10.15892/j.cnki.djzdxb.2010.04.016

Abstract

For hypersonic missile in complex environment of reentry, the fractional-order PIDμDν (FOC) was applied to attitude control of missile and tunes FOC parameters by the ITAE index combining with its ten-order Tustin+CFE digital implementation. The simulation results show that compared with traditional PID controller, FOC has better control effect and stronger robustness when aerodynamic parameters change.

Key words： fractional-order PIDμDν controller; attitude control; ITAE index; Tustin+CFE

[an error occurred while processing this directive]

参考文献

[1]
WANG Q, STENGEL R F. Robust nonlinear control of a hypersonic aircraft[J]. Journal of Guidance, Control and Dynamics, 2000, 23(4): 577- 584.
[2]
ITO D, WARD D, VALASEK J. Robust dynamic inversion controller design and analysis for the X-38[C]// AIAA Guidance, Navigation, and Control Conference. Montreal, Canada: AIAA, 2001: 1- 11.
[3]
XU HJ, IOANNOU PA, MIRMIRANI M. Adaptive sliding mode control design for a hypersonic flight vehicle[J]. Journal of Guidance, Control and Dynamics, 2004, 25(5): 829- 838.
[4]
Serdar Ethem Hamamci. An algorithm for stabilization of fractional order time delay systems using fractional-order PID controllers[J]. IEEE Transactions on Automatic Control, 2007, 52(10): 1964- 1969.
[5]
Podlubny I. Fractional-order systems and PIλDμ controllers[J]. IEEE Transactions on Automatic Control, 1999, 44(1): 208- 214.
[6]
曹军义, 曹秉刚. 分数阶控制器的数字实现及其特性[J]. 控制理论与应用, 2006, 23(5): 791- 794.
[7]
Vinagre B M, Podlubny I, Hernandez A, et al. Some approximations of fractional order operators used in control theory and applications[J]. Fractional Calculus and Applied Analysis, 2000(3): 231- 248.
[8]
CHEN YQ, MOORE K L. Discretization schemes for fractional-order differentiators and integrators[J]. IEEE Trans on Circuits and Systems, 2002, 49(3): 363- 367.
Options
文章导航

/

〈 〉

[an error occurred while processing this directive]