May 19, 2025
 Home  中文
Air & Space Defense  2021, Vol. 4 Issue (1): 65-70    DOI:
UAV Overall and Support Technologies Current Issue | Archive | Adv Search |
Controller Design of the UAV Formation Based on Adaptive Integral Sliding Mode
LIU Chen1, XIE Baodi1, DONG Guobao1, HUO Da1, DUAN Yuxin1,XIA Chuan2
1. Science and Technology on Space System Simulation Laboratory, Beijing Simulation Center, Beijing 100854, China; 2. Beijing Institute of Electronic System Engineering, Beijing 100854, China
Download: PDF (1478 KB)   (1 KB) 
Export: BibTeX | EndNote (RIS)      
Abstract  The controller design problem of a class of UAV (unmanned aerial vehicle) formation systems with bounded disturbance is studied in this paper. Based on adaptive integral sliding mode control frame, a novel adaptive controller is proposed. The adaptive law is introduced to estimate the upper bound of disturbance. The effect of disturbance can be cancelled in the designed protocol. The stability of the closed UAV formation system is analyzed by Lyapnov method. Simulation results validate that the controller proposed in this paper can guarantee the robustness of the closed-loop system, the continuity of the control signal and the signal is relatively small. Hence, the method is prone to apply in practical engineering.
Key wordsUAV      formation control      adaptive      integral sliding mode      consensus     
Received: 27 November 2020      Published: 25 March 2021
ZTFLH:  TP273  
Service
E-mail this article
Add to my bookshelf
Add to citation manager
E-mail Alert
RSS
Articles by authors
Cite this article:   
URL:  
https://www.qk.sjtu.edu.cn/ktfy/EN/     OR     https://www.qk.sjtu.edu.cn/ktfy/EN/Y2021/V4/I1/65
Copyright © 2015 Air & Space Defense, All Rights Reserved.
Powered by Beijing Magtech Co. Ltd