The objective of this study was to investigate the stability derivatives and the stability of the vectored thrust P-1127 airplane. Expressions were derived for the derivatives. The performance, derivatives and stability were found for both an accelerating and nonaccelerating transition from hover to conventional flight. The results of the accelerating transition were compared to values available from Hawker Siddeley. Both transitions were unstable for many airspeeds but the times to double amplitude were such that a pilot could control the airplane. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    VTOL -- Composite or vectored thrust

    Rolfe, J. | Engineering Index Backfile | 1962


    Geometric trajectory tracking with attitude planner for vectored-thrust VTOL UAVs

    Invernizzi, Davide / Lovera, Marco / Zaccarian, Luca | BASE | 2018

    Free access


    THRUST VECTORED MULTICOPTERS

    KHOO SUI YANG / NORTON MICHAEL JOHN / KOUZANI ABBAS ZAHEDI | European Patent Office | 2019

    Free access

    THRUST VECTORED MULTICOPTERS

    KHOO SUI YANG / NORTON MICHAEL JOHN / KOUZANI ABBAS ZAHEDI | European Patent Office | 2022

    Free access