基于自适应模型的推理用于嵌入式诊断和容错系统的冗余管理

M. Nolan, J. Giordano
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引用次数: 5

摘要

在航空航天系统中,安全性、可持续性和任务关键性的考虑通常预示着对内置容错的要求。现有的实现容错的方法通常集中在“蛮力”硬件冗余和作为“点解决方案”开发的广泛、复杂的控制逻辑上,以实现重新配置动作。本文描述了一种创新方法的主要概念和设计实现,该方法将基于自适应模型的诊断推理能力嵌入到容错远程电源控制器(FTRPC)中,为关键用户提供快速故障诊断和重新配置潮流。该方法的一个关键方面是使用系统工程过程来开发可嵌入系统中的推理能力,以完成故障检测、隔离、重新配置和恢复。通过自动化工具集应用的系统工程过程在本质上是通用的,并且可以应用于任何系统,而不是通过密集的工程努力开发的“点解决方案”。整体方法的可扩展性和适用性是该方案的关键技术成果。本文描述了将芯片诊断技术嵌入到最先进的远程电源控制器中的基本概念和实现。该设计最近在马歇尔航天飞行中心(MSFC)主持下的NASA第二阶段SBIR计划下的集成产品开发环境中实施。这种新方法可以通过开发可适应大量动态重新配置状态的确定性基于模型的诊断功能,彻底改变容错系统的健康管理实现。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Use of adaptive model-based reasoning for embedded diagnostics and redundancy management for fault tolerant systems
Safety, sustainability and mission criticality considerations often predicate the requirement for built-in fault tolerance in aerospace systems. Existing approaches to accomplishing fault tolerance typically focus on "brute-force" hardware redundancy and extensive, complex control logic developed as a "point solution" to effect reconfiguration actions. This paper describes the principal concepts and design implementation of an innovative approach for embedding an adaptive model-based diagnostic reasoning capability into a Fault Tolerant Remote Power Controller (FTRPC) to provide rapid fault diagnostics and reconfiguration of powerflow to critical users. A key aspect of this approach is that a systems engineering process was used to develop the reasoning capability that could be embedded in the system to accomplish fault detection, isolation, reconfiguration and recovery. The system engineering process, applied through an automated tool set, is generic in nature and can be applied to any system, as opposed to a "point solution" developed by intensive engineering efforts. The extensibility and applicability of the overall approach is a key technology accomplishment of the program. This paper describes the underlying concepts and implementation of embedding Diagnostician-on-a-Chip technology into a state-of-the-art remote power controller. This design was recently implemented in an Integrated Product Development environment under a NASA Phase II SBIR Program conducted under the auspices of Marshall Space Flight Center (MSFC). This new approach can revolutionize the implementation of health management for fault tolerant systems by developing a deterministic model-based diagnostic capability that is adaptive to a vast number of dynamic reconfiguration states.
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