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基于FLNDO的近空间飞行器鲁棒最优预测控制
引用本文:都延丽,吴庆宪,姜长生,周丽.基于FLNDO的近空间飞行器鲁棒最优预测控制[J].宇航学报,2009,30(4).
作者姓名:都延丽  吴庆宪  姜长生  周丽
作者单位:南京航空航天大学自动化学院,南京,210016
基金项目:国家自然科学基金重大项目 
摘    要:针对有强烈干扰和不确定因素影响的近空间高超声速飞行器,提出了一种鲁棒最优广义预测控制律.控制律由最优广义预测控制律(OGPC)和一种新的泛函连接网络干扰观测器(FLNDO)构成.输出的有限时域预测由泰勒级数的展开实现.飞行中的未建模动态以及未知干扰由FLNDO来估计,并且文中也给出了FLNDO和闭环系统的稳定性分析.仿真结果表明对于姿态角和角速率的跟踪问题,设计的控制器达到了满意的控制效果,并且也成功实现了对干扰的抑制以及参数变化的鲁棒性要求.

关 键 词:近空间高超声速飞行器  非线性不确定系统  最优广义预测控制  泛函连接网络  干扰观测器

Based on Functional Link Network Disturbance Observer
DU Yan-li,WU Qing-xian,JIANG Chang-sheng,ZHOU Li.Based on Functional Link Network Disturbance Observer[J].Journal of Astronautics,2009,30(4).
Authors:DU Yan-li  WU Qing-xian  JIANG Chang-sheng  ZHOU Li
Abstract:A robust optimal generalized predictive control ( OGPC) law was presented for a near-space hypersonic ve-hicle (NHV) in the presence of strong disturbances and uncertainties. The control law consisted of the OGPC law and anew functional link network disturbance observer ( FLNDO). The output prediction defined on finite horizon was carried outvia Taylor series expansion. The unmodeled dynamics and unknown disturbances in flight were estimated by the FLNDO.The paper also provided stability analyses of the FLNDO and close-loop system. The simulation results show that the satis-factory performance of the controller for attitude angles tracking,the robustness to parameters variations and the disturbancerejection are successfully accomplished.
Keywords:Near-space hypersonic vehicle  Nonlinear uncertain system  Optimal generalized predictive control  Functional link network  Disturbance observer
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