Nonlinear Flight Control Design Using Sliding Mode Disturbance Observer-Based Constraint Backstepping

被引:0
作者
Zhang, Chao [1 ]
Chen, Zongji [1 ]
Wei, Chen [1 ]
机构
[1] Beijing Univ, Aeronaut & Astronaut, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
来源
PROCEEDINGS OF THE 10TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA 2012) | 2012年
关键词
flight control; constraint backstepping; sliding mode disturbance observer; heavy cargo airdrop; MAGNITUDE; SYSTEMS;
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
This paper presents a sliding mode disturbance observer-based constraint backstepping control approach (CBS/SMDO) to control a cargo aircraft during heavy cargo airdrop operation. The CBS/SMDO controller is capable of dealing with parametric uncertainties, external disturbances, and unmodeled dynamics in the presence of state/control constraints. The super-twisting second order sliding mode disturbance observer (SOSMDO) is utilized to compensate for the overall uncertainties, avoiding high control gains. The SOSMDO is much simpler than the neural networks-based estimator and could provide asymptotic convergence of the estimation error to zero in finite time. The closed-loop stability is guaranteed in the sense of Lyapunov. The proposed CBS/SMDO controller is applied to the airdrop flight control design on a nonlinear six-degrees-of freedom transport aircraft model in a low attitude tandem extraction airdrop scenario. Simulation results demonstrate the feasibility of the CBS/SMDO method.
引用
收藏
页码:1818 / 1825
页数:8
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