Design of Nonlinear Backstepping Controller for Flying Wing UAV Maneuvering Flight

Design of Nonlinear Backstepping Controller for Flying Wing UAV Maneuvering Flight

The flying wing unmanned aerial vehicle (UVA) has poor maneuvering capacity, strong nonlinear and coupling capacities. The traditional Backstepping method can improve the system robustness of flying wing UVA, but has the problems of singular value calculation and conservative property. An improved B...

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Bibliographic Details
Main Authors: YANG Leiheng, LI Jiguang, YANG Lu, YUE Yuan
Format: Article
Language:zho
Published: Editorial Department of Advances in Aeronautical Science and Engineering 2020-10-01
Series:Hangkong gongcheng jinzhan
Subjects:
flying wing uva
maneuvering flight
backstepping method
robustness
singular value calculation
Online Access:http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2019143?st=article_issue

Internet

http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2019143?st=article_issue

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