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

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 Matlab. 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.

关键词： nonlinear syste extended linearization symbolic language design flight control system

作者: Li Qiu-ju Liao Ni-huan Gong Lu-hong

作者单位: North China Institute of Water Conservancy andHydroelectric PowerZhengzhou,450011, China Zhengzhou Xianghe Group Electrical Installing CO.,LTD Zhengzhou, 450053, China

会议类型: 国际会议

会议名称: 2011 International Conference on Information System and Computational Intelligence(2011 IEEE信息系统与计算智能国际会议 ICISCI 2011)

会议地点: 哈尔滨

会议语种:英文

页码: 254-257

在线出版日期: 2011-01-18（万方平台首次上网日期，不代表论文的发表时间）