飞轮姿态控制与能量传输系统技术进展综述

V. Babuska, S. Beatty, B. deBlonk, J. Fausz
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引用次数: 52

摘要

在过去的十年里,人们对飞轮储能系统在空间应用方面的兴趣有所上升。空军任务概念化学电池的局限性、微处理器和复合材料的进步以及使用飞轮系统进行能量存储和作为姿态控制执行器的前景推动了这种兴趣。主要问题是功率效率、质量和尺寸以及长期稳定性。飞轮作为航天器电池的一对一替代品仅在少数特殊任务中具有竞争力。当飞轮取代两个主要总线子系统中的组件时,潜在的重量和体积优势是有吸引力的。本文的目的是描述用于空间应用的综合动力和姿态控制(IPAC)系统的飞轮技术的最新进展,并描述当前AFRL的工作。本文讨论的主要技术领域是飞轮设计、轴承密封和安全、组合功率分配和姿态控制。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A review of technology developments in flywheel attitude control and energy transmission systems
In the past decade there has been an upswing in the interest of flywheel energy storage systems for space applications. This interest has been driven by limitations of chemical batteries for Air Force mission concepts, advances in microprocessors and composite materials, and the promise of using flywheel systems for energy storage and as attitude control actuators. The primary issues are power efficiency, mass and size, and long-term stability. Flywheels as one-to-one replacements for spacecraft batteries are competitive for only a few special missions. When flywheels replace components in two major bus subsystems, the potential weight and volume benefits are attractive. The objective of this paper is to describe the progression of flywheel technology state-of-the-art for integrated power and attitude control (IPAC) systems in space applications, and describe current AFRL efforts. The main technology areas that are addressed in this paper are flywheel designs, bearings containment and safety, and combined power distribution and attitude control.
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