Adaptive Augmentation of an Unmanned Aerial Vehicle's Flight Control System

被引：0
|
作者：
Vlk, Jan [1 ]
Chudy, Peter [1 ]
机构：
[1] Brno Univ Technol, Fac Informat Technol, Brno, Czech Republic
来源：
2018 IEEE/AIAA 37TH DIGITAL AVIONICS SYSTEMS CONFERENCE (DASC) | 2018年
关键词：
adaptive control; aircraft; control hedging; control laws; dynamic model; flight control system; fixed wing; linear quadratic regulator; Lyapunov stability; model reference adaptive control; simulation; state-space model; unmanned aerial vehicle;
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The proposed paper introduces the design of an adaptive augmentation of an Unmanned Aerial Vehicle's (UAV) Flight Control System (FCS). A Linear Quadratic Regulator (LQR) algorithm has been employed as a base-line control strategy and enhanced with an adaptation loop based on a Model Reference Adaptive Control (MRAC) technique.
引用
收藏
页码：633 / 641
页数：9
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