Performance metrics for evaluating spacecraft power control and management (PCM)

C. Madhusudhana, J. Kishore
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引用次数: 6

Abstract

The power subsystem is the most critical system in a spacecraft due to the dependency of nearly every other subsystem for power. The power system configuration depends on various factors such as amount of power required, type of orbit, duration of the mission, constraints on mass volume, and the impact of the system's hardware on the spacecraft design. Power system encompasses power generation, energy storage and power processing. The organization of control and management circuits to carry out these functionalities is termed as Power Control and Management (PCM). Selection of an appropriate PCM is must for achieving the desired mission goal. This makes its choice a most important one for spacecraft Engineers. Different methods are adopted for finding out a suitable PCM. However availability of indices facilitate the evaluation of electrical performance of PCM systems. Hence a set performance metrics which would serve as benchmark has been detailed here. In the end, a typical case has been enumerated to demonstrate the usefulness of these metrics.
评价航天器功率控制与管理(PCM)的性能指标
动力分系统是航天器中最关键的系统,因为几乎所有其他分系统都依赖于动力。动力系统的配置取决于各种因素,如所需的功率、轨道类型、任务持续时间、对质量体积的限制以及系统硬件对航天器设计的影响。电力系统包括发电、储能和电力处理。实现这些功能的控制和管理电路的组织称为电源控制和管理(PCM)。为了实现预期的任务目标,必须选择合适的PCM。这使得它的选择成为航天器工程师最重要的选择。采用不同的方法来寻找合适的PCM。然而,指标的可用性有助于对PCM系统的电气性能进行评价。因此,这里详细介绍了一组可以作为基准的性能指标。最后,列举了一个典型案例来证明这些度量的有用性。
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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