For pt.I see ibid., p.333-6 (Oct. 1990). It is indicated that fault-tolerant guidance and control systems can be employed to meet the goals of the advanced launch system. Proven redundancy management techniques are proposed for implementation in such guidance systems. The methods discussed provide a high probability of failure detection while maintaining a low probability for false alarms. A hardware architecture that stresses robustness, simplicity, and ease of verification is advocated. The channelized repartition of instruments and electronics can be modified to support different requirements and applications. The issue of simultaneous or dormant failures is addressed. The fault-tolerant architecture and implementation discussed is considered to provide excellent reliability and probability of mission success, while maintaining very reasonable costs.


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    Title :

    A fault-tolerant architecture for launch vehicle guidance and control. II. Implementation


    Additional title:

    Eine fehlertolerante Architektur für die Startraketenleitung und -steuerung. II. Implementierung


    Contributors:
    Tazartes, D.A. (author) / Mark, J.G. (author)


    Publication date :

    1990


    Size :

    7 Seiten, 2 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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