Adaptive control and parameter-dependent anti-windup compensation for inertia-varying quadcopters*
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Louisville, Louisville, KY, USA
Funder
NASA Kentucky
Publisher
Informa UK Limited
Subject
Computer Science Applications,Control and Systems Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/00207179.2022.2138555
Reference28 articles.
1. Chen, J., Wang, J. & Wang, W. (2018). Model reference adaptive control for a class of aircraft with actuator saturation. InChinese control conference(pp. 2705–2710). IEEE.
2. Dhaybi, M. & Daher, N. (2020). Accurate real-time estimation of the inertia tensor of package delivery quadrotors. InAmerican control conference(pp. 1520–1525). IEEE.
3. Do, A., Da Silva Jr., J. G., Sename, O. & Dugard, L. (2011). Control design for LPV systems with input saturation and state constraints: an application to a semi-active suspension. InIEEE conference on decision and control and European control conference(pp. 3416–3421). IEEE.
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Anti-Windup Compensator Design for Guidance and Control of Quadrotors;2024 American Control Conference (ACC);2024-07-10
2. Anti‐windup compensation for model reference adaptive control schemes;International Journal of Robust and Nonlinear Control;2024-06-30
3. Quadcopters Control Using Online Dynamic Mode Decomposition*;IFAC-PapersOnLine;2023
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