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Power efficiency system for flight application (pesfa) mission

机译：飞行应用（pesfa）任务的能效系统

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The objective of this current research is to describe the design of a high performance micro sensor for small spacecraft that acts as the core of a stand-alone aerospace system. A high performance cascaded micro sensor is designed with micro-electro-mechanical systems (MEMS) and nano-scaled technology, and can be incorporated in conventional methods as well as new spacecraft system designs focused on power efficiency system for flight application (PESFA) mission, referred to herein as the PESFA mission. This research describes the behavior of high performance micro sensor design methodology with dynamic configuration. The results of the computer simulations of these micro sensors are compared for possible improvements and provide high power efficiency at very long lifetimes to be able to operate independent of an energy limitation in flight application such as spacecraft and aerospace systems
机译：当前研究的目的是描述一种小型航天器的高性能微传感器的设计，该传感器充当独立航空航天系统的核心。高性能级联微传感器采用微机电系统（MEMS）和纳米级技术设计而成，可与传统方法以及专注于飞行应用能效系统（PESFA）任务的新航天器系统设计结合使用，这里称为PESFA任务。这项研究描述了具有动态配置的高性能微传感器设计方法的行为。比较了这些微传感器的计算机仿真结果，以求可能的改进，并在非常长的使用寿命内提供高功率效率，从而能够在飞行应用（例如航天器和航空航天系统）中不受能量限制地运行

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