Integrated optimum design of structure and H-infinity control system

AIAA Journal ◽  
1996 ◽  
Vol 34 (1) ◽  
pp. 159-165 ◽  
Author(s):  
K. Tsujioka ◽  
I. Kajiwara ◽  
A. Nagamatsu
Keyword(s):  
Control System ◽  
Optimum Design ◽  
H Infinity ◽  
H Infinity Control

scholarly journals Optimal Control for Combined Energy Storage and Attitude Control System (CEACS) in Small Satellites

2011 ◽  
Vol 110-116 ◽  
pp. 3587-3592 ◽  
Author(s):  
Ban Ying Siang ◽  
Renuganth Varatharajoo
Keyword(s):  
Control System ◽  
Energy Storage ◽  
Attitude Control ◽  
Control Methods ◽  
Attitude Control System ◽  
H Infinity ◽  
Small Satellites ◽  
Satellite Attitude Control ◽  
H Infinity Control ◽  
Control Modules

The combined energy storage and attitude control system (CEACS) combines both energy storage and attitude control modules via the flywheel technology. Previously only the conventional control methods were tested for CEACS. In this paper, H2 and H-infinity control methods are implemented in CEACS. The satellite attitude control performances show that both control options can be employed for a good attitude pointing accuracy. (Abstract)

scholarly journals H-infinity Control System Design for a Quad-rotor

2015 ◽  
Vol 21 (1) ◽  
pp. 14-20 ◽  
Author(s):  
Taesam Kang ◽  
Kwang Joon Yoon ◽  
Tae-Hyun Ha ◽  
Gigun Lee
Keyword(s):  
Control System ◽  
System Design ◽  
Control System Design ◽  
H Infinity ◽  
H Infinity Control

scholarly journals Using of H-Infinity Control Method in Attitude Control System of Rigid-Flexible Satellite

2009 ◽  
Vol 2009 ◽  
pp. 1-9 ◽  
Author(s):  
Ximena Celia Méndez Cubillos ◽  
Luiz Carlos Gadelha de Souza
Keyword(s):  
Adaptive Control ◽  
Control System ◽  
Control Systems ◽  
Attitude Control ◽  
Control Method ◽  
Control Design ◽  
Attitude Control System ◽  
H Infinity ◽  
H Infinity Control ◽  
Linear And Nonlinear

The attitude control systems of satellites with rigid and flexible components are demanding more and more better performance resulting in the development of several methods control. For that reason, control design methods presently available, including parameters and states estimation, robust and adaptive control, as well as linear and nonlinear theory, need more investigation to know their capability and limitations. In this paper the investigated technique is H-Infinity method in the performance of the Attitude Control System of a Rigid-Flexible Satellite.

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