Inner System Design of a Nonlinear Plane Based on Extended Linearization Model

被引:0
作者
Li Qiu-ju [1 ]
Liao Ni-huan [1 ]
Gong Lu-hong [2 ]
机构
[1] N China Inst Water Conservancy & Hydroelect Power, Zhengzhou 450011, Peoples R China
[2] Zhengzhou Xianghe Grp Elect Installing Co Ltd, Zhengzhou 450043, Peoples R China
来源
ADVANCED MATERIALS AND ENGINEERING MATERIALS, PTS 1 AND 2 | 2012年 / 457-458卷
关键词
nonlinear system; extended linearization; symbolic language; flight control system;
D O I
10.4028/www.scientific.net/AMR.457-458.1331
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In order to deal with the control of a rigid spacecraft, a general technique to design advanced controllers for electrical transfer inner system of nonlinear plane was given, based on the generalized extended linearization model and symbolic language of Mat lab. And the system with feedback-control-loop is equal to a linear system basically. Finally the corresponding linear system transfer function is given and the result of simulation has proved the specialties of this control method through the system indentification.
引用
收藏
页码:1331 / +
页数:3
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