火星观测飞机磁控管相控阵功率传输系统自动跟踪与功率控制实验

A. Nagahama, T. Mitani, N. Shinohara, K. Fukuda, K. Hiraoka, K. Yonemoto
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引用次数: 4

摘要

本研究的目的是为火星观测飞机研制微波功率传输系统。广泛而持续的火星观测对于了解火星的物理特性变得越来越重要。我们提出了一种基于磁控管相控阵的发射系统。在本文中,我们进行了自动跟踪实验,证实了自动跟踪系统的位置检测误差导致接收功率下降。我们还演示了发射功率控制,并证实了功率控制为地面实验飞机提供了近似均匀的直流电压。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Auto tracking and power control experiments of a magnetron-based phased array power transmitting system for a Mars observation airplane
The objective of the present study is to develop a microwave power transmitting system for a Mars observation airplane. A wide-ranging continual Mars observation is becoming important for understanding physical properties of Mars. We suggested a transmitting system with a magnetron-based phased array. In this paper, we conducted auto tracking experiments and confirmed position detection error of the auto tracking system caused declines of received power. We also demonstrated transmitting power control and confirmed that the power control provided approximately uniform DC voltage for a ground experiment airplane.
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