Back-stepping based anti-disturbance flight controller with preview methodology for autonomous aerial refueling

被引:74
作者
Su, Zikang [1 ,2 ,3 ]
Wang, Honglun [1 ,3 ]
Yao, Peng [1 ,3 ]
Huang, Yu [1 ,3 ]
Qin, Yong [1 ,3 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Honors Coll, Beijing 100191, Peoples R China
[3] Beihang Univ, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
Autonomous aerial refueling; Receiver flight control; Back-stepping; Active disturbance rejection control; Preview control; Fuzzy logic control; TRAJECTORY TRACKING CONTROLLER; DESIGN; SYSTEM; PROBE;
D O I
10.1016/j.ast.2016.11.028
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper proposes a novel back-stepping based flight controller for the receiver in Autonomous Aerial Refueling (AAR) by the combination of active disturbance rejection control (ADRC) and preview control methodology. Firstly, the proposed flight control law design is divided into five loops by the back-stepping technique. The 6 DOF model for aircraft is written into several strict-feedback nonlinear forms through tactful transformation, considering that the path dynamics are originally non-affine nonlinear forms and are intractable for controller design. Secondly, the influences of the unknown flow perturbations on a receiver in each loop are viewed as the components of the "total disturbances" which are estimated and compensated by extended state observer (ESO). Thirdly, the preview control methodology is introduced into the position loop design as the system dynamic of the receiver is much slower than drogue. The position loop determines the proper reference path angle by using a fuzzy-logic ADRC controller in which previewing error and current tracking error are both taken into consideration. And a novel adaptive look-ahead distance scheme based on the fuzzy logic control (FLC) is proposed for the selection of the preview point. Finally, extensive simulations and comparisons on the 6 DOF receiver model are carried out to demonstrate the effectiveness of the proposed flight controller. (C) 2016 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:95 / 108
页数:14
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