实时执行内核和故障管理工具

T. Sadeghi, W. Harris
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引用次数: 0

摘要

为了帮助用户在飞行控制计算机的设计过程中设计和评估实时执行核和冗余管理算法,开发了一个容错飞行控制模拟器工具。为了配合这种模拟,开发了一个实时执行内核的顶层设计,以描述设计实时执行内核时使用的基本技术。对几种类型的冗余管理算法的研究揭示了在先进飞行控制系统背景下对这些算法的实时性要求的差异,其中几种算法已被纳入模拟器。执行内核的设计过程和冗余管理算法为如何开发和设计实时系统提供了基本的理解。使用已开发的容错飞行控制模拟器工具,可以在正式定义飞行控制体系结构之前对容错实时系统软件体系结构进行调查、分析和故障排除。使用这种FTFCS工具和所讨论的设计技术,飞行控制计算机系统的非经常性成本和实际设计时间可能会减少。关于这个主题的未来增强和努力可能包括向模拟器添加处理用户提供的调度技术和冗余管理算法的功能。这将使模拟在本质上更加通用,并将增强其多功能性,以适应更广泛的应用。其他增强功能可能包括修改图形界面,以包括一个平视显示器模型或飞机的三维图形表示,这将模拟飞机在特定飞行员输入命令下的动态运动。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Real time executive kernel and fault management tools
A fault tolerant flight control simulator tool has been developed to aid the user in designing and evaluating real time executive kernels and redundancy management algorithms in the design process of a flight control computer. To compliment this simulation, a top level design of a real time executive kernel has been developed to portray the basic techniques used when designing a real time executive kernel. Investigations into several types of redundancy management algorithms have revealed the differences in the real time requirements for these algorithms in the context of an advanced flight control system, and several of these algorithms have been incorporated into the simulator. The design process of the executive kernel and the redundancy management algorithms offer a basic understanding of how a real time system would be developed and designed. The use of the fault tolerant flight control simulator tool that has been developed allows an investigation, analysis, and trouble shooting of fault tolerant, real time system software architectures to be performed prior to the flight control architecture being formally defined. With the use of this FTFCS tool and the discussed design techniques, the non recurring costs and the actual design time of a flight control computer system could potentially be reduced. Future enhancements and efforts on this topic might include adding to the simulator the capability for processing user supplied scheduling techniques and redundancy management algorithms. This would make the simulation more generic in nature and would enhance its versatility to a greater variety of applications. Other enhancements might include modifying the graphical interface to include a model of a head up display or a three dimensional graphical representation of an aircraft which would mimic the aircraft's dynamic motion under specific pilot input commands.
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