Tilt-rotor multivariable attitude control with rotor state feedback

被引：2
|
作者：
Panza, S. [1 ]
Guastalla, L.
Roda, B.
Lovera, M. [1 ]
机构：
[1] Politecn Milan, Dept aerospace SCi & Technol, Via La Masa 34, I-20156 Milan, Italy
来源：
IFAC PAPERSONLINE | 2016年 / 49卷 / 17期
关键词：
Attitude control; H-infinity optimization; Aircraft control; Sensitivity functions; HANDLING QUALITIES;
D O I：
10.1016/j.ifacol.2016.09.018
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In this paper, a multi-objective optimization-based methodology for rotorcraft attitude control law design is applied to a tilt-rotor case; the framework allows to enforce requirements of stability, performance, control action moderation, and safety. The structured H-infinity approach is taken into account, and the optimization problem is stated as a mixed-sensitivity problem. Rotor state feedback is used to limit flap motion, and is introduced as an additional loop to a classical attitude control law. (C) 2016, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
引用
收藏
页码：100 / 105
页数：6
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