Flight Control Design for Small-Scale Helicopter Using Disturbance-Observer-Based Backstepping-Reference-Cited by-同舟云学术

Flight Control Design for Small-Scale Helicopter Using Disturbance-Observer-Based Backstepping

Published:2015-11 Issue:11 Volume:38 Page:2235-2240
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Lu Hao¹,Liu Cunjia²,Guo Lei³,Chen Wen-Hua²

Affiliation:

1. School of Instrumentation Science and Opto-Electronics Engineering, Beihang University, 100191 Beijing, People’s Republic of China

2. Department of Aeronautical and Automotive Engineering, Loughborough University, Loughborough, England LE11 3TU, United Kingdom

3. National Key Laboratory on Aircraft Control Technology, Beihang University, 100191 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G001196

Reference15 articles.

1. Nonlinear Disturbance Observer-Enhanced Dynamic Inversion Control of Missiles

2. Disturbance attenuation and rejection for systems with nonlinearity via DOBC approach

3. Tracking control of small-scale helicopters using explicit nonlinear MPC augmented with disturbance observers

4. CaiG. “Development of Small-Scale Unmanned-Aerial-Vehicle Helicopter Systems,” Ph.D. Dissertation, Dept. of Electrical and Computer Engineering, National Univ. of Singapore, Singapore, 2009, Chap. 4.

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