1–20 von 25 Ergebnissen
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    Identification of a nonlinear aerodynamic model of the F-14 aircraft

    Trankle, Thomas L. / Bachner, Stephen D. | AIAA | 1995

    Control Logic to Track Outputs of a Command Generator

    Thomas L. Trankle / Arthur E . Bryson | AIAA | 1978

    Combustion zone - Acoustic cavity interactions in rocket combustors

    Acker, Thomas L. / Mitchell, Charles E. | AIAA | 1994

    Buffet response of a hammerhead launch vehicle wind-tunnel model

    COLE, STANLEY R. / HENNING, THOMAS L. | AIAA | 1992

    Some Aspects of Aerial Combat

    WILLY Y. PENG AND THOMAS L. VINCEN | AIAA | 1975

    Estimating projections of the controllable set

    VINCENT, THOMAS L. / WU, ZONG Y. | AIAA | 1990

    Maximum likelihood tuning of a vehicle motion filter

    TRANKLE, THOMAS L. / RABIN, URI H. | AIAA | 1990

    Advanced Advanced Advanced Methods of Model Structure Determination from Test Data

    Gupta, Narendra K. / Hall Earl / Trankle et al. | AIAA | 1978

    Minimizing interceptor size using neural networks for terminal guidance law synthesis

    Cottrell, Ronald G. / Vincent, Thomas L. / Sadati, Seyed H. | AIAA | 1996

    Solid Rocket Enabling Technologies and Milestones in the United States

    Leonard H. Caveny / Robert L. Geisler / Russell A. Ellis et al. | AIAA | 2003