Gain Scheduled Attitude Control of Fixed-Wing UAV With Automatic Controller Tuning-Reference-Cited by-同舟云学术

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Gain Scheduled Attitude Control of Fixed-Wing UAV With Automatic Controller Tuning

Published:2018-07 Issue:4 Volume:26 Page:1192-1203
ISSN:1063-6536
Container-title:IEEE Transactions on Control Systems Technology
language:
Short-container-title:IEEE Trans. Contr. Syst. Technol.

Author:

Poksawat Pakorn,Wang Liuping^ORCID,Mohamed Abdulghani

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Control and Systems Engineering

Link

http://xplorestaging.ieee.org/ielx7/87/8379025/07954051.pdf?arnumber=7954051

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1. Aerobatic Maneuvering Flight Control of Fixed-Wing UAVs: An SE(3) Approach Using Dual Quaternion;IEEE Transactions on Industrial Electronics;2024-11

2. Optimized Fractional-Order Type-2 Fuzzy PID Attitude Controller for Fixed-Wing Aircraft;Journal of Optimization Theory and Applications;2024-09-09

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4. Bio-Inspired Adaptive Fuzzy Control Systems for Precise Low-Altitude Hovering of an Unmanned Aerial Vehicle Under Large Uncertainties;2024 European Control Conference (ECC);2024-06-25

5. Adaptive Attitude Control of a Quadrotor Vehicle in Mixed Wind Field;Proceedings of the 2024 6th International Conference on Control and Computer Vision;2024-06-13

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