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首页> 外文期刊>St. Petersburg Polytechnic University Journal: Physics and Mathematics >A model of an ion plasma electrically powered spacecraft propulsion with a remote monitoring and a control system
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A model of an ion plasma electrically powered spacecraft propulsion with a remote monitoring and a control system

机译：具有远程监测和控制系统的离子等离子体电动航天器推进模型

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This paper continues the publication cycle on developing the ion plasma electrically powered spacecraft propulsion (EPSP) of the spacecraft. For monitoring and control of the EPSP operation, a feedback system based on a signal proportional to the EPSP plasma radiation intensity has been proposed to be used. It was assumed that the radiation intensity in the ultraviolet, visible and infrared ranges being proportional to the instantaneous thrust value of the EPSP. Accordingly, the introduction of a signal from the radiation registration detector into the feedback loop should allow to create an onboard closed system for monitoring and control of the EPSP operation. A photodetector based on a dynamic pin-diode integrator was considered for use in this system.
机译：本文继续发布在开发航天器的离子等离子体电动航天器推进（EPSP）上的出版周期。 为了监视和控制EPSP操作，已经提出了一种基于与EPSP等离子体辐射强度成比例的信号的反馈系统。 假设紫外线中的辐射强度，可见光和红外范围与EPSP的瞬时推力值成比例。 因此，将来自辐射登记检测器的信号引入反馈循环应该允许创建用于监视和控制EPSP操作的车载封闭系统。 基于动态引脚二极管积分器的光电探测器被认为用于该系统。

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