Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
7154154 | Chinese Journal of Aeronautics | 2017 | 18 Pages |
Abstract
The tilt rotor unmanned aerial vehicle (TRUAV) exhibits special application value due to its unique rotor structure. However, varying dynamics and aerodynamic interference caused by tiltable rotors are great technical challenges and key issues for TRUAV's high-powered flight controls, which have attracted the attention of many researchers. This paper outlines the concept of TRUAV and some typical TRUAV platforms while focusing on control techniques. TRUAV structural features, dynamics modeling, and flight control methods are discussed, and major challenges and corresponding developmental tendencies associated with TRUAV flight control are summarized.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Liu Zhong, He Yuqing, Yang Liying, Han Jianda,