The correct integration of the Automatic Flight Control System (AFCS), into an aircraft will provide the best performance that a system can produce. Improper integration of the AFCS, along with poor installation practices, account for the majority of problems.The Avionics subsystems are becoming increasingly complex, using digital designs, and the components used are much more fragile than in previous avionics.The AFCS integration requirements must include consideration of regulatory requirements, location of the equipment, installation design criteria, human factors, sensor installation tolerances, interfaces with aircraft systems, and customer special requirements.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    AFCS Integration Requirements


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Business Aircraft Meeting and Exposition ; 1981



    Publication date :

    1981-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    A study of (AFCS) communications measurement program

    Breipohl, A.M. / Shanmugam, K.S. / Doemland, H. | Tema Archive | 1973


    Digital Computation Makes AFCS More Reliable

    Raymond, R. G. / Larson, J. C. | IEEE | 1975


    Development of an AFCS SIL Twin for Autopilot Software Design and Integration

    Demirer, Serkan / Duran, Sabahat / Yilmaz, Murat | TIBKAT | 2023


    A-7A AFCS -- Flight-proved high-gain system

    Kramer, K.C. | Engineering Index Backfile | 1966


    Development of an AFCS SIL Twin for Autopilot Software Design and Integration

    Demirer, Serkan / Duran, Sabahat / Yilmaz, Murat | AIAA | 2023