Flight Controller Design for Small Quad Tilt Wing UAV
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/64/1/64_64_79/_pdf
Reference1 articles.
1. 1) 佐藤昌之，村岡浩治：Quad Tilt Wing 無人航空機の飛行制御，日本航空宇宙学会論文集，61 (2013), pp. 110-118.
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1. Structured μ-Synthesis of Robust Attitude Control Laws for Quad-Tilt-Wing Unmanned Aerial Vehicle;Journal of Guidance, Control, and Dynamics;2020-12
2. H∞ Control-Based Robust CAS Design for QTW-UAV via the Multiple-Model Approach with Particle Swarm Optimization;International Journal of Aerospace Engineering;2019-07-21
3. H∞ Control-based CAS Design of QTW-UAVs Using Particle Swarm Optimization;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2018
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