Automatic Three-Point Landing of a UAV with H∞-Controlin D-Implementation

被引：5
|
作者：
Sedlmair, Nicolas [1 ]
Theis, Julian [1 ]
Thielecke, Frank [1 ]
机构：
[1] Hamburg Univ Technol, Inst Aircraft Syst Engn, Hamburg, Germany
来源：
IFAC PAPERSONLINE | 2019年 / 52卷 / 12期
关键词：
flight control; robust control applications; multivariable control systems; AUTOLAND CONTROLLER; AUTOPILOT DESIGN; AIRCRAFT;
D O I：
10.1016/j.ifacol.2019.11.262
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A multivariable flight control law for automatic landing of an unmanned aircraft with tailwheel gear configuration is developed in this paper. The control law is obtained using H-infinity-synthesis and implemented in a differential form to facilitate bumpless transfer, i.e. correct initialization when switching control laws, and anti-windup compensation. The controller is evaluated using a validated high-fidelity model of the aircraft and Monte-Carlo simulations. Copyright (C) 2019. The Authors. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码：316 / 321
页数：6
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