基于切换多胞模型的变体飞行器增益调参控制

王通; 王青; 江未来; 董朝阳

基于切换多胞模型的变体飞行器增益调参控制

1.
北京航空航天大学自动化科学与电气工程学院, 北京 100191
2. 北京航空航天大学航空科学与工程学院, 北京 100191

基金项目: 国家自然科学基金资助项目（61273083）

详细信息

中图分类号: V249.1
计量
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- 被引次数: 0
出版历程
- 收稿日期: 2013-04-01
- 网络出版日期: 2014-01-20

Gain schedule control of morphing vehicle based on switched polytopic system

1.
School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
2. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 针对一类可变后掠翼的变体飞行器，研究了全包线控制器的设计与综合方法.建立了基于切换多胞系统的变体飞行器模型，所提出的框架利用Lyapunov函数方法分析系统的稳定性，能够从理论上保证变体飞行器在全包线下的飞行稳定.给出了利用小凸包算法从三维飞行包线中选取设计点的方法，并对各设计点处的线性化模型设计了最优控制律.为继承传统增益调参方法的优势，提出了一种特殊的控制器插值方法，保证变体飞行器三维包线下的控制综合过程简便实用.仿真结果表明所提出的控制方法在飞行器快速变形和参数大范围快速变化的情况下仍具有良好的控制性能.
- 变体飞行器 /
- 增益调参 /
- 切换多胞系统 /
- 稳定性分析
Abstract: Considering morphing vehicles with alterable sweep wings, control design and synthesis within full flight envelope was researched. The morphing vehicle model based on switched polytopic systems was established. In this framework, the stability analysis was accomplished by Lyapunov functions. The presented approach can guarantee the flight stability of the morphing vehicle within full flight envelope. A technique using the small convex hull algorithm was provided to select operating points from the 3-D flight envelope. Optimal control laws were also designed for linear models of operating points. To inherit the advantage of traditional methods, a specific interpolation method was proposed to make the control synthesis within the 3-D flight envelope brief and practical. Simulation results show that the proposed approach can guarantee flight performance during the fast reshaping of the morphing vehicles within full flight envelope.
- morphing vehicle /
- gain schedule /
- switched polytopic system /
- stability analysis

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参考文献(10)

[1]	Chakravarthy A, Grant D T, Lind R.Time-varying dynamics of a micro air vehicle with variable-sweep morphing[J].Journal of Guidance, Control, and Dynamics, 2012, 35(3):890-903
[2]	Seigler T M, Neal D A.Analysis of transition stability for morphing aircraft[J].Journal of Guidance, Control, and Dynamics, 2009, 32(6):1947-1953
[3]	乐挺, 王立新, 艾俊强.变体飞机设计的主要关键技术[J].飞行力学, 2009, 27(5):6-10 Yue Ting, Wang Lixin, Ai Junqiang.Key technologies in morphing aircraft design[J].Flight Dynamics, 2009, 27(5):6-10(in Chinese)
[4]	陆宇平, 何真.变体飞行器控制系统综述[J].航空学报, 2009, 30(10):1906-1911 Lu Yuping, He Zhen.A survey of morphing aircraft control systems[J].Acta Aeronautica et Astronautica Sinica, 2009, 30(10): 1906-1911(in Chinese)
[5]	Obradovic B, Subbarao K.Modeling of flight dynamics of morphing wing aircraft[J].Journal of Aircraft, 2011, 48(2):391-402
[6]	Abdulrahi M.Maneuvering control and configuration adaptation of a biologically inspired morphing aircraft[D].Florida:University of Florida, 2007
[7]	Seigler T M.Dynamics and control of morphing aircraft[D].Virginia:Virginia Polytechnic Institute and State University, 2005
[8]	苏铁, 董朝阳, 侯砚泽.变体无人机动力学模型及切换控制研究[J].沈阳航空航天大学学报, 2012, 29(1):1-5 Su Tie, Dong Chaoyang, Hou Yanze.Modeling and switching control of morphing UAV[J].Journal of Shenyang Aerospace University, 2012, 29(1):1-5(in Chinese)
[9]	Hou Yanze, Wang Qing, Dong Chaoyang.Gain scheduled control:switched polytopic system approach[J].Journal of Guidance, Control, and Dynamics, 2011, 34(2):623-629
[10]	Baldelli D H, Lee D, Pena R S, et al.Modeling and control of an aeroelastic morphing vehicle[J].Journal of Guidance, Control and Dynamics, 2008, 31(6):1687-1699