Accurate data are necessary for the identification of aerodynamic parameters at high angle of attack and in spinning flight. Modern sensors and microelectronic devices are employed in a stall/spin data acquisition system that will be tested in a Schweizer 2-32 sailplane. This instrumentation package will use a quaternion-based "strapdown IMU" algorithm to derive vehicle attitude from angular rate data, and it will use fault-detection logic to identify inflight sensor failures. Details of the system and flight test program are presented, together with results of preflight digital simulation analysis.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A Microprocessor-Based Data-Acquisition System for Stall/Spin Research


    Beteiligte:


    Erscheinungsdatum :

    1983-01-01


    Format / Umfang :

    2333993 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    A microprocessor-based data-acquisition system for stall/spin research

    Sri-Jayantha, M. / Stengel, R.F. | Tema Archiv | 1983



    Stall/spin research status report

    Bowman, J. S., Jr. / Burk, S. M., Jr. | NTRS | 1974


    Stall/Spin Research Status Report

    Bowman, James S. / Burk, Sanger M. | SAE Technical Papers | 1974