A high-temperature superconductor energy-momentum control system for small satellites

被引：7
|
作者：
Wilson, TL [1 ]
机构：
[1] NASA, Lyndon B Johnson Space Ctr, Space & Life Sci Directorate, Astromat Res & Explorat Sci Off, Houston, TX 77058 USA
来源：
IEEE TRANSACTIONS ON APPLIED SUPERCONDUCTIVITY | 2003年 / 13卷 / 02期
关键词：
attitude control; energy storage; magnetic bearings; momentum management;
D O I：
10.1109/TASC.2003.813078
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
A method for angular momentum management in flywheel energy storage systems that employ superconducting bearings for spacecraft attitude control is presented. Success with high-temperature superconductor momentum wheels as practical energy storage systems has led to increased interest in their dual function for providing electrical power as well as attitude control of small satellites. The physics of angular momentum management is used to quantify how superconductor magnetic bearing flywheels as electro-mechanical devices serve as both energy storage and angular momentum storage systems within an end-to-end architecture. The result is a compound energy-momentum attitude and electrical power control system for satellites.
引用
收藏
页码：2287 / 2290
页数：4
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