Optimal Path Following for Small Fixed-Wing UAVs Under Wind Disturbances

被引:48
作者
Yang, Jun [1 ,2 ]
Liu, Cunjia [2 ]
Coombes, Matthew [2 ]
Yan, Yunda [2 ]
Chen, Wen-Hua [2 ]
机构
[1] Southeast Univ, Sch Automat, Nanjing 210096, Peoples R China
[2] Loughborough Univ, Dept Aeronaut & Automot Engn, Loughborough LE11 3TU, Leics, England
基金
中国国家自然科学基金; 英国工程与自然科学研究理事会;
关键词
Wind; Unmanned aerial vehicles; Heuristic algorithms; Aerodynamics; Vehicle dynamics; Kinematics; Task analysis; Disturbance observer; optimal control; path following; unmanned aerial vehicle (UAV); UNMANNED AERIAL VEHICLES; MODEL-PREDICTIVE CONTROL; NONLINEAR-SYSTEMS; TRACKING; GUIDANCE; PERFORMANCE; ALGORITHMS; SINGLE;
D O I
10.1109/TCST.2020.2980727
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 article presents a novel path-following algorithm for fixed-wing unmanned aerial vehicles by virtue of a nonlinear optimal control approach and wind disturbance observers. Different from some exiting algorithms, the proposed algorithm formulates the path-following problem into a control problem by introducing auxiliary dynamics for the path parameter. The proposed controller is designed in an optimal and systematic manner where the control action is generated according to a well-defined cost function. This framework does not require any complex geometric coordinate transformation and can be easily tuned to accommodate curved reference paths, making it straightforward to deploy in different flight missions. Moreover, the wind influences on the path-following performance is explicitly compensated by the proposed algorithm based on the wind estimates provided by nonlinear disturbance observers. The closed-loop stability, including the auxiliary dynamics for path parameter and observer dynamics for wind estimation, is also analyzed. The feasibility and effectiveness of the proposed algorithm have been thoroughly validated in simulation studies and realistic flight tests.
引用
收藏
页码:996 / 1008
页数:13
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