1–14 von 14 Ergebnissen
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    Stability and control considerations for STOL AIRCRAFT.

    Anderson, S. B. / Innis, R. C. / Quigley, H. C. | NTRS | 1965

    A split-damper inertially coupled passive gravity-gradient attitude control system.

    Merrick, V. K. / Tinling, B. E. / Watson, D. M. | NTRS | 1966

    VTOL control system studies on a six-degree- of-freedom motion simulator.

    Fry, E. B. / Gerdes, R. M. / Gossett, T. D. et al. | NTRS | 1967

    A flight investigation of a terminal area navigation and guidance concept for STOL aircraft

    Smith, D. W. / Neuman, F. / Watson, D. M. et al. | NTRS | 1976

    Operational experience with a powered-lift STOL aircraft

    Innis, R. C. / Quigley, H. C. | NTRS | 1976

    A method for determining landing runway length for a STOL aircraft

    Watson, D. M. / Hardy, G. H. / Moran, J. F. et al. | NTRS | 1981

    Flight evaluation of a precision landing task for a powered-lift STOL aircraft

    Watson, D. M. / Hardy, G. H. / Innis, R. C. et al. | NTRS | 1986

    New capabilities and recent research programs of the NASA/Army CH-47B variable-stability helicopter

    Hindson, W. S. / Hilbert, K. B. / Tucker, G. E. et al. | NTRS | 1986