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运载火箭飞行控制系统双机仿真技术研究
引用本文:张毅成,国文杰. 运载火箭飞行控制系统双机仿真技术研究[J]. 计算机仿真, 2005, 22(3): 56-60
作者姓名:张毅成  国文杰
作者单位:北京控制与电子技术研究所,北京,100038;北京控制与电子技术研究所,北京,100038
摘    要:
运载火箭飞行控制系统的研制要求越来越高,需要有一项新的仿真技术及方法,全面验证飞控计算机软硬件设计的正确性,并能在实验室和火箭发射场环境下进行半实物仿真试验。该文对这项技术及方法进行了研究,提出了双机仿真技术方案:双机仿真系统组成、对飞控计算机软硬件设计要求、双机同步仿真方法、伴随仿真方法。这项技术及方法,已在试验实践中得到了很好的应用,满足了运载火箭飞行控制系统越来越高的研制要求,已成为一项十分有效的试验手段。

关 键 词:飞行控制系统  双机仿真  双机同步仿真  伴随仿真  仿真计算机  飞控计算机
文章编号:1006-9348(2005)03-0056-04
修稿时间:2003-12-09

Double Computers Simulation Technology for Carrier Rocket Flight Control System
ZHANG Yi-cheng,GUO Wen-jie. Double Computers Simulation Technology for Carrier Rocket Flight Control System[J]. Computer Simulation, 2005, 22(3): 56-60
Authors:ZHANG Yi-cheng  GUO Wen-jie
Abstract:
The development of the carrier rocket flight control system are setting much higher requirements, it needs a new method of simulation technology to validate the correctness on the software and hardware design of the flight control computer, and complete the hardware in loop in the laboratory and at the rocketdrome. This paper just studies the technology and method and puts forward the project of double computers simulation: the form of double computers simulation system, the requirements of the software and hardware design of flight control computer, double computers synchronization simulation method, concomitancy simulation method etc. This technology and method have been applied in examination, and it satisfies the higher development requirement of carrier rocket flight control system, it has become an effective examination means.
Keywords:Flight control system  Double computers simulation  Double computers synchronization simulation  Concomitancy simulation  Simulation computer  Flight control computer
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