飞行姿态模拟器建模及输入受限混杂控制

张刘; 金光; 郑亮亮

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飞行姿态模拟器建模及输入受限混杂控制

微纳技术与精密机械 | 更新时间：2020-08-12

- 飞行姿态模拟器建模及输入受限混杂控制
- Modeling and hybrid control of aircraft simulation with input constraints
- 光学精密工程 2009年17卷第7期页码：1561-1569
- 作者机构：
  
  中国科学院长春光学精密机械与物理研究所, 吉林长春 130033
- 作者简介：
- 基金信息：
  
  国家863高科技研究发展计划资助项目(No.2007aa12J123)()
- DOI：
  中图分类号： V448.153
- 收稿日期：2009-02-11，
  
  修回日期：2009-03-24，
  
  网络出版日期：2009-07-25，
  
  纸质出版日期：2009-07-25
- 稿件说明：
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张刘, 金光, 郑亮亮. 飞行姿态模拟器建模及输入受限混杂控制[J]. 光学精密工程, 2009,17(7): 1561-1569

ZHANG Liu, JIN Guang, ZHENG Liang-liang. Modeling and hybrid control of aircraft simulation with input constraints[J]. Editorial Office of Optics and Precision Engineering, 2009,17(7): 1561-1569
张刘, 金光, 郑亮亮. 飞行姿态模拟器建模及输入受限混杂控制[J]. 光学精密工程, 2009,17(7): 1561-1569 DOI：

ZHANG Liu, JIN Guang, ZHENG Liang-liang. Modeling and hybrid control of aircraft simulation with input constraints[J]. Editorial Office of Optics and Precision Engineering, 2009,17(7): 1561-1569 DOI：

摘要

为进行飞行姿态仿真研究

基于dSPACE建立了地面飞行姿态半物理仿真模拟系统

运用混杂不变集原理和无源控制器设计方法对有界高阶耦合非线性系统进行鲁棒控制器设计。使用Lagrange法建立了具有控制约束的非线性Euler-Lagrange (EL)动力学模型;利用EL系统内在特性

基于非线性状态依赖动态脉冲系统的不变集原理的有关结果和混杂能量控制方法

设计了输入受限的非线性混杂控制器

并进行了数学仿真。最后

将所设计的混杂控制器应用于地面飞行姿态模拟器中进行了半物理仿真实验

得到的动态响应时间为20 s

稳态精度优于5%

超调量约为25%

在外加扰动作用时仍能实现稳定调节。结果表明

给出的饱和控制算法可靠性较强

对系统参数误差和外干扰具有鲁棒性。

Abstract

In order to control the flight attitude for an aircraft

a ground semi-physical flight attitude simulation system was established based on a dSPACE system. The invariant set principle and Passivity-based Controller (PBC) design method was used to deal with the aircraft simulation system

for it was a kind of higher order nonlinear control system with strong coupling. A nonlinear Euler-Lagrange (EL) dynamic model with controller constraints for the aircraft simulation system was established by the Largange method. Then

based on the internal characters of EL systems and the recent results on invariant set stability theorems of nonlinear impulsive hybrid systems

a saturation dynamical hybrid controller for the aircraft simulation system was presented

and the mathematic simulation was also given out to verify the effect of the proposed controller. Finally

a semi-physical simulation experiment was undertaken with the proposed controller.Obtained results show that the dynamic response time is about 20 s

steady-state accuracy is less than 5% and the overshoot is about 25%. These data indicate that the designed saturation controller is valid and robust to both the system parameter errors and disturbance.

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Keywords

references

冯纯伯. 非线性控制系统分析与设计[M]. 2版.北京: 电子工业出版社, 1998. FEN CH B. Nonlinear Control Systems Analysis and Design[M]. 2nd ed.Beijing: Electronics Industry Press, 1998. (in Chinese)[2] 胡跃明. 非线性控制系统理论与应用 [M]. 北京:国防工业出版社,2004. HU Y M. Nonlinear Control System Theory and Application[M]. Beijing: National Defense Industry Presss, 2004. (in Chinese)[3] 楚中毅,崔晶,孙立宁,等. 双重驱动2-DOF平面并联机器人系统的研究[J]. 光学精密工程, 2006,14(3):456-461. CHU ZH Y, CUI J, SUN L N, et al.. Research of a novel dual-driven 2-DOF planar parallel robot[J]. Opt. Precision Eng., 2006,14(3):456-461. (in Chinese)[4] ALION A, ORTEGA R. An observer-based set-point controller for robot manipulators with flexible joints[J]. Syst. Contr. Lett., 1993,21:329-335.[5] 岳明, 邓宗全. 基于状态观测器的球形机器人状态反馈控制系统设计[J]. 光学精密工程, 2008,15(6):878-883. YUE M, DENG Z Q. Design of state feedback control system for spherical robot based on state observe [J]. Opt. Precision Eng., 2008,15(6):878-883. (in Chinese)[6] 郭振凯, 顾文锦. 十字梁实验系统的设计与仿真[J]. 计算机仿真, 2003, 20(11):45-47. GUO ZH K, GU W J. Design and simulation of cross beam experiment system[J]. Computer simulation, 2003, 20(11):45-47. (in Chinese)[7] 郭振凯, 顾文锦. 基于离散非线性PID 控制的十字梁实验系统研究[J]. 系统仿真学报,2003,15(9):1322-1324. GUO ZH K, GU W J. Research on cross beam experiment system based on discrete nonlinear PID control[J]. Journal of System Simulation, 2003,15(9):1322-1324. (in Chinese)[8] LORA A, KELLY R, ORTEGA R, et al.. On global output feedback regulation of euler-Lagrange systems with bounded inputs[J]. IEEE Trans. on Automatic Control,1997,42(8):1138-1143.[9] 张刘,段广仁,王子华. 非线性基准系统的输入受限输出反馈动态脉冲混杂全局调节器设计[J]. 吉林大学学报(工学版), 2008,38(3):735-740. ZHANG L, DUAN G R, WANG Z H. Output feedback global regulation for nonlinear benchmark system with input constraints using hybrid dynamic impulse controller[J]. Journal of Jilin University (Engineering and Technology Edition),2008,38(3):735-740. (in Chinese)[10] HADDAD W M, CHELLABOINA V, KABLAR N A. Nonlinear impulsive dynamical systems. Part Ⅰ: stability and dissipativity . Proc. IEEE Conf. Decision and Control, Phoenix, AZ, 1999:4404-4422.[11] VIJAYSEKHAR C, SANJAY P B, WASSIM M H. An invariance principle for nonlinear hybrid and impulsive dynamical systems . Proceeding of the American Control Conference, Chicago, 2000:3116-3122.[12] 厉明, 纪勇, 贾宏光,等. 基于快速仿真原型的飞行器半物理仿真系统[J]. 光学精密工程, 2008,16(10):1949-1955. LI M, JI Y, JIA H G, et al.. Hardware-in-closed-loop simulation system for aircraft based on rapid simulation prototype[J]. Opt. Precision Eng., 2008,16(10):1949-1955. (in Chinese)[13] 杨旭,孙兆伟,朱承元,等. 基于dSPACE的卫星控制实时仿真系统设计[J]. 系统工程与电子技术, 2005,27(2):335-339. YAN X, SUN ZH W, ZHU CH Y, et al.. Design of real-time simulation system for satellite control based on dSPACE system[J]. Systems Engineering and Electronics, 2005,27(2):335-339. (in Chinese)

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