Flight Control Design for Small-Scale Helicopter Using Disturbance-Observer-Based Backstepping

被引:52
|
作者
Lu, Hao [1 ]
Liu, Cunjia [2 ]
Guo, Lei [3 ]
Chen, Wen-Hua [2 ]
机构
[1] Beihang Univ, Sch Instrumentat Sci & Optoelect Engn, Beijing 100191, Peoples R China
[2] Univ Loughborough, Dept Aeronaut & Automot Engn, Loughborough LE11 3TU, Leics, England
[3] Beihang Univ, Natl Key Lab Aircraft Control Technol, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
TRACKING CONTROL;
D O I
10.2514/1.G001196
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A study adopts the disturbance-observer-based control scheme to enhance the flight control performance. This method is known as an active anti-disturbance strategy where the lumped disturbances from various sources are estimated by a disturbance observer (DO) and then incorporated into a nominal controller to compensate for their adverse effects. A preliminary study has demonstrated the disturbance rejection ability of this control strategy on a small-scale helicopter. The study proposes a novel disturbance-observer design that extends the scope of the classical one to a partial-state unmeasurable system.
引用
收藏
页码:2235 / 2240
页数:6
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