双飞轮单轴联合姿态控制和能量存储演示

2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720) Pub Date : 2013-07-31 DOI:10.1109/aero.2004.1368077

Barbara H. Kenny, Ralph H. Jansen, P. Kascak, T. Dever, Walter Santiago

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引用次数: 14

摘要

目前，典型卫星的能量存储子系统和姿态控制子系统是分离的。能量储存通常由镍镉电池或NiH电池提供，主动姿态控制由控制力矩陀螺仪(cmg)或反应轮完成。如果将这两个子系统结合使用多个飞轮同时进行动能存储和动量传递，则可以实现整体系统质量节约。几位作者研究了飞轮的控制来实现这一目标，并发表了仿真结果，证明了该方法的可行性和性能。本文首次给出了利用两个飞轮在单轴上实现能量存储和动量控制的实验结果。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Demonstration of single axis combined attitude control and energy storage using two flywheels

The energy storage and attitude control subsystems of the typical satellite are presently distinct and separate. Energy storage is conventionally provided by batteries, either NiCd or NiH, and active attitude control is accomplished with control moment gyros (CMGs) or reaction wheels. An overall system mass savings can be realized if these two subsystems are combined using multiple flywheels for simultaneous kinetic energy storage and momentum transfer. Several authors have studied the control of the flywheels to accomplish this and have published simulation results showing the feasibility and performance. This paper presents the first experimental results showing combined energy storage and momentum control about a single axis using two flywheels.

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2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720)

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