Linjie Huang
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Research Subjects
Linjie Huang has a total of 2 co-authors. Here are the top co-authors by number of shared publications:
- Hailong Pei
Key Laboratory of Autonomous Systems and Network Control, Ministry of Education, Guangdong Engineering Technology Research Center of Unmanned Aerial Vehicle Systems, South China University of Technology, Guangzhou 510641, China
1 shared publication - Zihuan Cheng
School of Automation, South China University of Technology, Guangzhou 510640, China
1 shared publication
Latest Publications
- 18 October 2022
- Published by Wiley in Asian Journal of Control
- Vol. 25 (2) , 1619-1638
System identification and improved internal model control for yaw of unmanned helicopter
The sea breeze is a low‐frequency disturbance that severely damages the stability of small unmanned helicopters operating over the sea, especially for the yaw control, which is highly sensitive to disturbance. General internal model control is an appropriate method for dealing with this kind of operation conditions, whereas conventional internal model control cannot eliminate the tracking errors between a nominal model and a real model. In coping with unknown dynamics and low‐frequency gust disturbances for small helicopters, this paper proposes a novel robust controller constructed with system identification and integrator‐based improved general internal model. As a refinement of the conventional frame, the proposed control scheme extends the applicable scope of a controlled plant from a priori known dynamic to an unknown dynamic. Furthermore, under the proposed controller, it is guaranteed that the tracking error between the actual model and the nominal model converges to zero asymptotically. Finally, the effectiveness and advantage of the proposed control scheme are verified through comparative practical flight tests.
- 18 October 2022
- Published by Wiley in Asian Journal of Control
- Vol. 25 (2) , 1619-1638
System identification and improved internal model control for yaw of unmanned helicopter
The sea breeze is a low‐frequency disturbance that severely damages the stability of small unmanned helicopters operating over the sea, especially for the yaw control, which is highly sensitive to disturbance. General internal model control is an appropriate method for dealing with this kind of operation conditions, whereas conventional internal model control cannot eliminate the tracking errors between a nominal model and a real model. In coping with unknown dynamics and low‐frequency gust disturbances for small helicopters, this paper proposes a novel robust controller constructed with system identification and integrator‐based improved general internal model. As a refinement of the conventional frame, the proposed control scheme extends the applicable scope of a controlled plant from a priori known dynamic to an unknown dynamic. Furthermore, under the proposed controller, it is guaranteed that the tracking error between the actual model and the nominal model converges to zero asymptotically. Finally, the effectiveness and advantage of the proposed control scheme are verified through comparative practical flight tests.