FAULT TOLERANT CONTROL FOR DAMAGED AIRCRAFT BASED ON SLIDING MODE CONTROL SCHEME

被引：0
|
作者：
Zhao, Jing [1 ]
Jiang, Bin [1 ]
Shi, Peng [2 ,3 ]
He, Zhen [1 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, 29 Yudao St, Nanjing 210016, Peoples R China
[2] Harbin Engn Univ, Coll Automat, Harbin 150001, Peoples R China
[3] Victoria Univ, Coll Engn & Sci, Melbourne, Vic 8001, Australia
来源：
INTERNATIONAL JOURNAL OF INNOVATIVE COMPUTING INFORMATION AND CONTROL | 2014年 / 10卷 / 01期
基金：
中国国家自然科学基金;
关键词：
Structural damage; Damage-tolerant control; Adaptive sliding mode;
D O I：
暂无
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
In this paper, the problem of structural damage with partial loss vertical tail in aircraft dynamical system is investigated. A linearized aircraft model is introduced firstly, then a damage -tolerant controller based on an adaptive sliding mode control is proposed. Finally, simulations with an aircraft model are conducted to demonstrate the effectiveness and advantages of the proposed design techniques, which can be properly tuned according to structural fault of aircraft.
引用
收藏
页码：293 / 302
页数：10
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