Spacecraft Magnetic Attitude Control Using Approximating Sequence Riccati Equations

被引：18

作者：

Rodriquez-Vazquez, Antonio L. ^{[1
]}

Martin-Prats, Maria A. ^{[1
]}

Bernelli-Zazzera, Franco ^{[2
]}

机构：

[1] Univ Seville, Dept Ingn Elect, Av Descubrimientos S-N, Seville 41092, Spain

[2] Politecn Milan, I-20133 Milan, Italy

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2015年 / 51卷 / 04期

关键词：

CONTROL SYSTEM; SATELLITE;

D O I：

10.1109/TAES.2015.130478

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents the results of a spacecraft attitude control system based on magnetic actuators designed for low Earth orbits. The control system is designed by using a nonlinear control technique based on the approximating sequence of Riccati equations. The behavior of the satellite is discussed under perturbations and model uncertainties. Simulation results are presented when the control system is able to guide the spacecraft to the desired attitude in a variety of different conditions.

引用

页码：3374 / 3385

页数：12

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