In Task 1, the requirements for the electrical power system and the integrated power system control were defined. In Task 2, three conceptual designs for the electrical power system were prepared. Each design incorporated a different data bus architecture, integrated, hierarchical, and non-integrated dedicated. The three designs were evaluated for application to a two engine tactical aircraft. Processor and data bus loading were examined for each architecture. Based on the evaluation, the conceptual design based on the integrated architecture is recommended for preliminary design in Task 3, Phase I. (Author)


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    Title :

    Advanced Aircraft Electrical System Control Technology Demonstrator. Phase I. Requirements Analysis and Conceptual Design


    Contributors:
    G. L. Dunn (author) / P. J. Leong (author) / I. S. Mehdi (author)

    Publication date :

    1981


    Size :

    103 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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