@inproceedings{f062dee3641c469cb03c991f7e23872c,
title = "L1 adaptive attitude controller for a tail-sitter MAV in hover flight",
abstract = "Since there exist several practical problems, hover flight control of tail-sitter vertical take-off and landing (VTOL) micro aerial vehicle (MAV) remains a challenging task all the time. This paper proposes a solution to this task, which combines the backstepping control architecture with L1 adaptive control theory. Aerodynamic moments of the wing are included thus the adaptation law is ensured to concentrate on the environmental disturbance. The output dynamic inversion is applied to determine the control surfaces deflection from control moments. These characters enable the controller to be transplanted to other VTOL MAV without retuning. The hover flight tests were conducted on a flying wing tail-sitter MAV, the results showed satisfactory tracking performance and disturbance resistance.",
keywords = "Backstepping control, L1 adaptive control, Micro aerial vehicle, Tail-sitter",
author = "Jin Wang and Bifeng Song and Liguang Wang",
year = "2014",
language = "英语",
series = "29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014",
publisher = "International Council of the Aeronautical Sciences",
booktitle = "29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014",
note = "29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014 ; Conference date: 07-09-2014 Through 12-09-2014",
}