COMPARISON OF LOW-EARTH-ORBIT SATELLITE ATTITUDE CONTROLLERS SUBMITTED TO CONTROLLABILITY CONSTRAINTS

被引：39
|
作者：
STEYN, WH
机构：
[1] University of Stellenbosch, Department of Electronic Engineering, Stellenbosch
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1994年 / 17卷 / 04期
关键词：
D O I：
10.2514/3.21269
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A rule-based fuzzy controller is presented and compared with an adaptive MIMO LQR controller in a low-Earth-orbit small satellite attitude control system. The attitude is passively gravity gradient stabilized and actively three-axis magnetorquer controlled. This method insures an Earth-pointing satellite making use of a nondepletable and nonmechanical means of control. A realistic simulation environment, using a nonlinear satellite dynamic model with linear attitude estimators plus sensor measurement noise and external disturbance torques, was used to evaluate the different control techniques.
引用
收藏
页码：795 / 804
页数：10
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