Observer-based supersonic cruise missile over-load control system design

被引：0

作者：

Chen Jie ^{[1
]}

Pan Chang-peng ^{[1
]}

Gu Wen-jin ^{[1
]}

机构：

[1] Naval Aeronaut Engn Inst, Dept Control Engn, Yantai 264001, Peoples R China

来源：

Proceedings of the 2007 Chinese Control and Decision Conference | 2007年

关键词：

non-minimum phase; zero dynamic; output-redefinition; integral-type sliding mode; observer;

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：

The pitch channal output tracking of a kind of supersonic cruise missile over-load control system is considered. Output-redefinition approach is adopted to design integral-type sliding mode control law, by which the nonminimum phase problem of original system is resolved, and the tracing of original system output is granteened. The observer is designed to establish missile attacking angle. The simulation results show the effectiveness and robustness.

引用

页码：143 / 146

页数：4

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