Polytopic LPV System Based Control Design for Multi-propeller airship

被引:0
作者
Chen, L. [1 ]
Duan, D. P. [1 ]
机构
[1] Shanghai Jiao Tong Univ, Inst Aerosp Sci & Technol, Shanghai 200240, Peoples R China
来源
2014 33RD CHINESE CONTROL CONFERENCE (CCC) | 2014年
关键词
Multi-propeller airship; Vectored thrust; Polytopic LPV System; HOSVD; H-infinity State feedback;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
An airship with multi-propeller was proposed in this paper, the nonlinear dynamic model was established and the longitudinal model is transformed into a LPV form by Jacobian linearization method. The discreted LPV system within the interzone of the changing parameters is storied into a tensor, and then HOSVD is used to obtain a finite number of LTI vertex systems, then the robust state-feedback controller was designed in vertex system using linear matrix inequalities(LMIs) approach, and a robust variable gain controller is synthesized via convex decomposition techniques. The velocity tracking of time-varying references based on nonlinear model was carried out with the designed controller; simulation results illustrate the validity of the designed controller.
引用
收藏
页码:4273 / 4276
页数:4
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