Adaptive Control of Free-Flying Space Robot with Position/Attitude Control System

1999 ◽  
Vol 22 (3) ◽  
pp. 488-490 ◽  
Author(s):  
Kei Senda ◽  
Hideyuki Nagoaka ◽  
Yoshisada Murotsu
Keyword(s):  
Adaptive Control ◽  
Control System ◽  
Attitude Control ◽  
Space Robot ◽  
Attitude Control System

Adaptive control of free-flying space robot with position/attitude control system

1997 ◽  
Author(s):  
Kei Senda ◽  
Hideyuki Nagaoka ◽  
Yoshisada Murotsu ◽  
Kei Senda ◽  
Hideyuki Nagaoka ◽  
...  
Keyword(s):  
Adaptive Control ◽  
Control System ◽  
Attitude Control ◽  
Space Robot ◽  
Attitude Control System

Adaptive control applied to Space Station attitude control system

1992 ◽  
Author(s):  
QUANG LAM ◽  
RICHARD CHIPMAN ◽  
TSAY-HSIN HU ◽  
ERIC HOLMES ◽  
JOHN SUNKEL
Keyword(s):  
Adaptive Control ◽  
Control System ◽  
Attitude Control ◽  
Space Station ◽  
Attitude Control System

scholarly journals Design of Attitude Control System for UAV Based on Feedback Linearization and Adaptive Control

2014 ◽  
Vol 2014 ◽  
pp. 1-8 ◽  
Author(s):  
Wenya Zhou ◽  
Kuilong Yin ◽  
Rui Wang ◽  
Yue-E Wang
Keyword(s):  
Adaptive Control ◽  
Control System ◽  
Attitude Control ◽  
Feedback Linearization ◽  
Control Law ◽  
Attitude Control System ◽  
Model Uncertainties ◽  
Performance Indexes ◽  
Attitude Dynamic ◽  
Adaptive Control Law

Attitude dynamic model of unmanned aerial vehicles (UAVs) is multi-input multioutput (MIMO), strong coupling, and nonlinear. Model uncertainties and external gust disturbances should be considered during designing the attitude control system for UAVs. In this paper, feedback linearization and model reference adaptive control (MRAC) are integrated to design the attitude control system for a fixed wing UAV. First of all, the complicated attitude dynamic model is decoupled into three single-input single-output (SISO) channels by input-output feedback linearization. Secondly, the reference models are determined, respectively, according to the performance indexes of each channel. Subsequently, the adaptive control law is obtained using MRAC theory. In order to demonstrate the performance of attitude control system, the adaptive control law and the proportional-integral-derivative (PID) control law are, respectively, used in the coupling nonlinear simulation model. Simulation results indicate that the system performance indexes including maximum overshoot, settling time (2% error range), and rise time obtained by MRAC are better than those by PID. Moreover, MRAC system has stronger robustness with respect to the model uncertainties and gust disturbance.

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.

Double Fail-Safe Attitude Control System for Artificial Meteor Microsatellite ALE-1

2021 ◽  
Vol 19 (1) ◽  
pp. 9-16
Author(s):  
Shinya FUJITA ◽  
Yuji SATO ◽  
Toshinori KUWAHARA ◽  
Yuji SAKAMOTO ◽  
Yoshihiko SHIBUYA ◽  
...  
Keyword(s):  
Control System ◽  
Attitude Control ◽  
Attitude Control System ◽  
Fail Safe

Flight performance of the LES-8/9 three-axis attitude control system

1980 ◽  
Author(s):  
F. FLOYD ◽  
C. MUCH ◽  
N. SMITH ◽  
J. VERNAU ◽  
J. WOODS
Keyword(s):  
Control System ◽  
Attitude Control ◽  
Flight Performance ◽  
Attitude Control System

Design of attitude control system for ASRTU microsatellite

2020 ◽  
Vol 28 (10) ◽  
pp. 2192-2202
Author(s):  
Feng WANG ◽  
◽  
Shi-bo NIU ◽  
Cheng-fei YUE ◽  
Fan WU ◽  
...  
Keyword(s):  
Control System ◽  
Attitude Control ◽  
Attitude Control System
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