scholarly journals Synthesis of an Attitude Control System for Unmanned Underwater Vehicle Using H-infinity Approach

2020 ◽  
Vol 53 (2) ◽  
pp. 14642-14649
Author(s):  
E.A. Gavrilina ◽  
V.N. Chestnov
Author(s):  
Norimitsu Sakagami ◽  
Mizuho Shibata ◽  
Sadao Kawamura ◽  
Toshifumi Inoue ◽  
Hiroyuki Onishi ◽  
...  

2021 ◽  
Vol 54 (2) ◽  
pp. 106-112
Author(s):  
GAVRILINA EKATERINA A. ◽  
◽  
VELTISHEV VADIM V. ◽  

Traditionally, unmanned underwater vehicles are operated at low angles of inclination (pitch and roll). However, there are tasks that require high maneuverability and controllability of the underwater vehicle in the entire range of orientation angles. At the same time, traditional control systems use the Euler angles and have limitations associated with the degeneration of the kinematic equations at a picth angle of ± 90 °, the problem of the non-uniqueness of the Euler angles, and the deterioration of the system performance at large inclinations of the vehicle. Thus, the question of developing a synthesis method for a control system for highly maneuverable unmanned underwater vehicles arises. The paper provides a review and comparative analysis of existing approaches to attitude control, on the basis of which an approach using quaternions is chosen. The law of attitude control based on quaternions was approved during field tests on a hybrid unmanned underwater vehicle "Iznos", developed at Bauman Moscow State Technical University. The results obtained during the tests are given in the article. The quaternion-based approach has better performance in comparison with the traditional control system. In addition, control system based on quaternion approach has a simple structure and can be used to increase the maneuverability of unmanned underwater vehicles with average requirements for positioning accuracy.


2011 ◽  
Vol 110-116 ◽  
pp. 3587-3592 ◽  
Author(s):  
Ban Ying Siang ◽  
Renuganth Varatharajoo

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)


2009 ◽  
Vol 2009 ◽  
pp. 1-9 ◽  
Author(s):  
Ximena Celia Méndez Cubillos ◽  
Luiz Carlos Gadelha de Souza

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.


Author(s):  
Shinya FUJITA ◽  
Yuji SATO ◽  
Toshinori KUWAHARA ◽  
Yuji SAKAMOTO ◽  
Yoshihiko SHIBUYA ◽  
...  

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