航天器地面供配电设备接口设计技术  

Interface Design Technology for Ground Power Supply Equipment to Aerospacecraft

作　　者：李立[1] 

机构地区：[1]航天东方红卫星有限公司,北京100080

出　　处：《计算机测量与控制》2003年第6期447-450,共4页Computer Measurement &Control

摘　　要：航天器地面供配电设备必须要确保供电控制的可靠和测量的准确。概述了该设备的基本组成和功能 ,对设备和航天器之间的控制信息、状态信息和测量信息的接口设计技术作了较详细地论述 ,并且结合有代表性的示例给出了参考电路图和说明。It is necessary that the equipment for ground power supply to aerospacecraft runs reliably and measurement through umbilical harness must be correct. The main components and functions of the equipment are described briefly,the interface design technology for control, status and measurement messages are explained, and the electrical diagram and its explanation as typical examples are shown.

关 键 词：航天器 地面供配电设备 接口 设计 印制板 计算机 

分 类 号：V55[航空宇航科学与技术—人机与环境工程] TP334.7[自动化与计算机技术—计算机系统结构]