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Lessons Learned on Implementing Fault Detection, Isolation, and Recovery (FDIR) in a Ground Launch Environment

机译:在地面发射环境中实施故障检测,隔离和恢复(FDIR)的经验教训

摘要

This paper's main purpose is to detail issues and lessons learned regarding designing, integrating, and implementing Fault Detection Isolation and Recovery (FDIR) for Constellation Exploration Program (CxP) Ground Operations at Kennedy Space Center (KSC). Part of the0 overall implementation of National Aeronautics and Space Administration's (NASA's) CxP, FDIR is being implemented in three main components of the program (Ares, Orion, and Ground Operations/Processing). While not initially part of the design baseline for the CxP Ground Operations, NASA felt that FDIR is important enough to develop, that NASA's Exploration Systems Mission Directorate's (ESMD's) Exploration Technology Development Program (ETDP) initiated a task for it under their Integrated System Health Management (ISHM) research area. This task, referred to as the FDIIR project, is a multi-year multi-center effort. The primary purpose of the FDIR project is to develop a prototype and pathway upon which Fault Detection and Isolation (FDI) may be transitioned into the Ground Operations baseline. Currently, Qualtech Systems Inc (QSI) Commercial Off The Shelf (COTS) software products Testability Engineering and Maintenance System (TEAMS) Designer and TEAMS RDS/RT are being utilized in the implementation of FDI within the FDIR project. The TEAMS Designer COTS software product is being utilized to model the system with Functional Fault Models (FFMs). A limited set of systems in Ground Operations are being modeled by the FDIR project, and the entire Ares Launch Vehicle is being modeled under the Functional Fault Analysis (FFA) project at Marshall Space Flight Center (MSFC). Integration of the Ares FFMs and the Ground Processing FFMs is being done under the FDIR project also utilizing the TEAMS Designer COTS software product. One of the most significant challenges related to integration is to ensure that FFMs developed by different organizations can be integrated easily and without errors. Software Interface Control Documents (ICDs) for the FFMs and their usage will be addressed as the solution to this issue. In particular, the advantages and disadvantages of these ICDs across physically separate development groups will be delineated.
机译:本文的主要目的是详细介绍有关为肯尼迪航天中心(KSC)的星座探索计划(CxP)地面行动设计,集成和实施故障检测隔离与恢复(FDIR)的问题和经验教训。 FDIR是美国国家航空航天局(NASA)CxP总体实施的一部分,目前正在该计划的三个主要组成部分(Ares,Orion和地面运行/处理)中实施。尽管最初并不是CxP地面作战的设计基准的一部分,但NASA认为FDIR具有足够的发展意义,但NASA的勘探系统任务局(ESMD)的勘探技术开发计划(ETDP)为其开展了一项任务,即“集成系统健康”。管理(ISHM)研究领域。该任务称为FDIIR项目,是一项多年的多中心工作。 FDIR项目的主要目的是开发一个原型和途径,在此基础上,故障检测和隔离(FDI)可以过渡到地面作战基准。当前,在FDIR项目中的FDI实施中,利用了Qualtech Systems Inc(QSI)商业现货(COTS)软件产品可测试性工程和维护系统(TEAMS)设计器和TEAMS RDS / RT。正在使用TEAMS Designer COTS软件产品通过功能故障模型(FFM)对系统进行建模。 FDIR项目正在对地面作战中的一组有限系统进行建模,整个马瑞斯运载火箭正在Marshall太空飞行中心(MSFC)的功能故障分析(FFA)项目中进行建模。在FDIR项目下,还使用TEAMS Designer COTS软件产品完成了Ares FFM和地面处理FFM的集成。与集成相关的最重大挑战之一是确保不同组织开发的FFM可以轻松集成且没有错误。 FFM的软件接口控制文档(ICD)及其用法将作为解决此问题的方法。特别是,将描述这些ICD在物理上分开的开发小组中的优缺点。

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