Virtual guidance-based finite-time path-following control of underactuated autonomous airship with error constraints and uncertainties

被引:1
|
作者
Wei, Yan [1 ]
Zhou, Pingfang [1 ]
Wang, Yueying [2 ]
Duan, Dengping [1 ]
Chen, Zheng [1 ]
机构
[1] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China
[2] Shanghai Univ, Sch Mechatron Engn & Automat, Shanghai, Peoples R China
基金
中国国家自然科学基金;
关键词
Underactuated autonomous airship; path-following; error constraint; finite-time; neural networks; ADAPTIVE NEURAL-CONTROL; DYNAMIC SURFACE CONTROL; STATION-KEEPING CONTROL; NONLINEAR-SYSTEMS; STRATOSPHERIC AIRSHIP; STABILIZATION;
D O I
10.1177/0954410020969319
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper addresses the finite-time three-dimensional path-following control problem for underactuated autonomous airship with error constraints and uncertainties. First, a five degrees-of-freedom path-following error model in the Serret-Frenet coordinate frame is established. By applying the finite-time stability theory, a virtual guidance-based finite-time adaptive neural backstepping path-following control approach is proposed. Barrier Lyapunov functions (BLFs) are introduced to deal with attitude error constraints. Neural networks (NNs) are presented to compensate for the uncertainties. To prevent the "explosion of complexity" in the design of the backstepping method, a finite-time convergent differentiator (FTCD) is introduced to estimate the time derivatives of virtual control signals. Stability analysis showed that all closed-loop signals are uniformly ultimately bounded, the constrained requirements on the airship attitude errors are never violated, and the path-following errors converge to a small neighborhood of the origin in a finite time. At last, simulation studies are provided to demonstrate the effectiveness of the proposed control approach.
引用
收藏
页码:1246 / 1259
页数:14
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