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A Dynamic Fault Tree Approach for Time-Dependent Logical Modeling of Autonomous Flight Systems

机译:自主飞行系统时间依赖性逻辑建模的动态故障树方法

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This paper addresses the urgent need for adequate methodologies to use in analyzing autonomous flight systems, including Unmanned Aircraft. These systems are inherently dynamic and require analysis that is explicitly time dependent. Autonomous flight systems are becoming more commonly used, especially for Part 23 aircraft including Business (Corporate) and Regional Jets or Unmanned Aircraft deployed in hazardous environment/situation. Such systems are expected to make their own decisions under uncertain conditions caused by potential system structure changes when entering a new flight phase or switching to a new system configuration due to system degradation or failure(s) [1]. This paper highlights significant modeling errors that can arise in analyzing dynamic scenarios where these time dependencies are ignored. Model-based solutions are provided by incorporating a time-dependent algebraic formalism into Fault Tree Analysis (FTA) and Dependency Diagram (DD) with updated descriptions in SAE ARP4761A and ARP4754B (Note: These are currently under development). A Dynamic Goal Tree (or alternatively, a Dynamic Dependency Diagram) provides an effective implementation of the time-dependent logic for dynamic system analysis analyzing autonomous flight systems which are inherently dynamic since decisions need to be made without human input in a very short time. The safety analysis for autonomous flight systems, including Unmanned Aircraft, can be performed by extending the traditional phased mission analysis, thus the potential system structure changes for different phases in a flight mission can be expressed by a Dynamic Fault Tree (DFT), or alternatively, a Dynamic Goal Tree (DGT), or Dynamic Dependency Diagram (DDD) [2].
机译:本文的地址为适当的方法来使用在分析自主飞行系统,包括无人飞机的迫切需要。这些系统本质上是动态的,需要分析,这是明确的时间依赖性。自主飞行系统越来越常用,尤其是对于部分23架飞机,包括企业(公司)和支线喷气飞机或无人机部署在危险环境/局势。这样的系统被预期进入一个新的飞行阶段或切换到一个新的系统配置由于系统退化或故障(S)[1]时,因潜在的系统结构的变化不确定的条件下,使自己的决定。本文强调,可以在分析动态情境中发生的是这些时间依赖性忽略显著建模误差。基于模型的解决方案是通过将随时间变化的代数形式主义到故障树分析(FTA)和依赖关系图(DD)与SAE ARP4761A和ARP4754B更新说明提供的(注:这是目前正在开发)。动态目标树(或者可替换地,动态依赖关系图)提供了一种有效地执行用于动态系统的分析分析自主飞行系统,因为决定需要在很短的时间而无需人工输入由这是固有的动态依赖于时间的逻辑。对于自主飞行系统,包括无人驾驶飞机的安全性分析,可以通过扩展传统的相控任务分析来进行,因此对于在飞行任务不同相位的电位的系统结构的改变可以通过一个动力故障树(DFT)来表示,或可选地,动态目标树(DGT),或动态依赖关系图(DDD)[2]。

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    《SAE AeroTech Americas》|2019年|1 Electronic text data|共6页
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    John Wang;

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  • 中图分类 V2-53;
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