On Structural Parameter Optimization Method for Quad Tilt-Wing UAV Based on Indirect Size Estimation of Domain of Attraction
Sign Up to like & getrecommendations! Published in 2022 at "IEEE Access"
DOI: 10.1109/access.2021.3139156
Abstract: To deal with the flexibility in the electric aircraft design, this study develops a structural parameter optimization method. The quad tilt-wing aircraft exhibits rotary-wing flight and fixed-wing flight modes by tilting its wings. This study… read more here.
Keywords: aircraft; method; tilt wing; quad tilt ... See more keywords
Control Augmentation System Design for Quad-Tilt-Wing Unmanned Aerial Vehicle via Robust Output Regulation Method
Sign Up to like & getrecommendations! Published in 2017 at "IEEE Transactions on Aerospace and Electronic Systems"
DOI: 10.1109/taes.2017.2650618
Abstract: Quad-tilt-wing (QTW) configuration is a promising one for airplanes to achieve vertical take-off and landing (VTOL), which has a pair of tandem wings that can tilt from vertical to horizontal positions. This unique configuration allows… read more here.
Keywords: quad tilt; control; tilt; unmanned aerial ... See more keywords