Luenberger Observer-Based Flight Controller Design Using Robust Control Toolbox™

被引:2
|
作者
Sato, Masayuki [1 ]
Akasaka, Daisuke [2 ]
机构
[1] Japan Aerosp Explorat Agcy, Aeronaut Technol Directorate, Mitaka, Tokyo 1810015, Japan
[2] MathWorks Japan, Minato Ku, 7-F Akasaka Garden City,4-15-1 Akasaka, Tokyo 1070052, Japan
关键词
D O I
10.1109/CCTA48906.2021.9659230
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents a design example of structured H-infinity, control-based flight controller for the lateral-directional motions of JAXA's research airplane MuPAL-alpha using MATLAB (R) Robust Control Toolbox (TM). To be more specific, the design problem of Luenberger observer-based flight controllers is addressed. Even if the controllers' structure is a priori supposed and fixed as Luenberger observer-based controllers, it does not always hold true that the controllers' states faithfully estimate the plants' states. We thus adopt two-step design approach to realize good control performance and good plants' states estimation simultaneously, viz., we first optimize H-infinity control performance of the closed-loop system, and then optimize H-infinity, observer performance under slightly relaxed H-infinity, control performance constraint. In the second process, systune command is used, because multiple design requirements are simultaneously imposed. The control and observer performance are both examined by the Hardware-In-the-Loop Simulation (HILS) tests using the actual MuPAL-alpha.
引用
收藏
页码:1160 / 1165
页数:6
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