Sliding mode disturbance observer-based backstepping control for a transport aircraft

被引:5
|
作者
Zhang Chao [1 ,2 ]
Chen ZongJi [1 ,2 ]
Wei Chen [1 ,2 ]
机构
[1] Beihang Univ, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
关键词
backstepping; sliding mode disturbance observer; flight control; heavy cargo airdrop; uncertainty estimation; FLIGHT CONTROL; NONLINEAR-SYSTEMS;
D O I
10.1007/s11432-013-4787-8
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents a novel control method by integrating the sliding mode disturbance observer-based control and the backstepping control technique, and successfully applies it to a flight control system for heavy cargo airdrop operations. The super-twisting second order sliding mode disturbance observer (SOSMDO) is employed to estimate bounded but otherwise arbitrary disturbances, thus ensuring asymptotic convergence of the estimation error to zero in a finite time. Besides, the integrated controller can significantly improve the robustness of the flight control system to modeling uncertainty and external disturbance in the presence of state/control constraints. The closed-loop stability is guaranteed in the sense of Lyapunov. In addition, the proposed approach can considerably reduce design cycles. The performance of the proposed control method is demonstrated in a very low altitude extraction airdrop simulation with a high-fidelity six-degree-of-freedom transport aircraft model.
引用
收藏
页码:1 / 16
页数:16
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