飞马航空电子系统设计

D.A. Steffy
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引用次数: 1

摘要

飞马座空射空间助推器在1990年4月5日成功地完成了它的首次飞行。数字航空电子设备和计算机技术的许多最新进展简化了飞行器及其测试。单串Pegasus航空电子设备包括多个基于微控制器的远程单元,用于控制执行器、发射推进器和烟火,并在VMEBUS飞行计算机中心的串行数字星型网络中收集遥测数据。飞行、飞机和测试软件是用C语言编写的,还有少量的FORTH和汇编语言。一系列的实验室、模拟、移动试验台、发动机静态发射和自备飞行试验验证了该航空电子系统已经为自由飞行做好了准备。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Pegasus avionics system design
The Pegasus air-launched space booster successfully completed its maiden flight on April 5, 1990. Many recent advances in digital avionics and computer technology simplified the vehicle and its testing. The single-string Pegasus avionics comprise multiple microcontroller-based remote units for controlling actuators, firing thrusters and pyrotechnics, and gathering telemetry arranged in a serial digital star network centered on the VMEBUS flight computer. Flight, aircraft, and test software is in C, with small amounts of FORTH and assembly language. A series of laboratory, simulation, mobile test bed, motor static firing, and captive flight tests verified that the avionics system was ready for free flight.<>
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