The special structural design and certification requirements that are needed for military aircraft incorporating active control technology (ACT) are considered. United Kingdom requirements are introduced which cover static strength, fatigue performance, aeroelesticity, and the need to assess the influence of modifications to ACT software. The requirements draw attention to the essential role of flight load measurements undertaken during both development and operational flying in the process of structural substantiation.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Structural Design Requirements for Aircraft Incorporating Active Control Technology


    Contributors:

    Publication date :

    1988


    Size :

    7 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Design synthesis for swept-wing aircraft incorporating stealth technology

    Siegers, F. / Cranfield University | TIBKAT | 1994


    Incorporating uncertainties in aircraft design

    Qiqi Wang | Online Contents | 2016


    Requirements-Based Testing in Aircraft Control Design

    Ghidella, Jason / Mosterman, Pieter | AIAA | 2005