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  • Numerical analysis of tangential slot blowing on a generic chined forebody [microform] / Roxana M. Agosta.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Computational analysis of forebody tangential slot blowing on the high alpha research vehicle [microform] / Ken Gee.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Feedback control laws for highly maneuverable aircraft [microform] / by William L. Garrard and Gary J. Balas.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Performance of an aerodynamic yaw controller mounted on the space shuttle orbiter body flap at Mach 10 [microform] / W.I. Scallion.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A vehicle health monitoring system for the space shuttle reaction control system during reentry [microform] / by Anthony David Rosello.

    • Text
    • Cambridge, Mass. : Charles Stark Draper Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail [microform] / by Matthew Robert Whiting.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle [microform] / Roger A. Lepsch, Jr. and George M. Ware, Ian O. MacConochie.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Biomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers [microform] / John W. Smith and Terry Montgomery.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996

  • Design and integration of an actuated nose strake control system [microform] / Bradley C. Flick ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996

  • QFT multi-input, multi-output design with non-diagonal, non-square compensation matrices [microform] / R.A. Hess and D.K. Henderson.

    • Text
    • [Elmsford, N.Y.] : Pergamon Press ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Adaptive variable bias magnetic bearing control [microform] / Dexter Johnson and Gerald V. Brown ; Daniel J. Inman.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Euler technology assessment for preliminary aircraft design [microform] : unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration / Todd R. Michal.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : Available from the National Technical Information Service, [1998]
    • 1998

  • High-alpha research vehicle lateral-directional control law description, analyses, and simulation results [microform] / John B. Davidson ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996

  • A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane [microform] / Frederick J. Lallman, John B. Davidson, and Patrick C. Murphy.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • A comprehensive C++ controller for a magnetically supported vertical rotor [microform] / Carlos R. Morrison.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS22930

  • Relative control effectiveness technique with application to airplane control coordination [microform] / Frederick J. Lallman.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service,] 1985.
    • 1985

  • Independent Orbiter assessment [microform] : analysis of the guidance, navigation, and control subsystem / [prepared by W.H. Trahan ... et al.].

    • Text
    • Houston, Tex. : McDonnell Douglas Astronautics Company, Houston Division ; [Washington, DC : National Aeronautics and Space Administration, 1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70168

  • Independent Orbiter assessment [microform] : analysis of the rudder/speed brake subsystem / [prepared by R.E. Wilson, J.R. Riccio].

    • Text
    • Houston, Tex. : McDonnell Douglas Astronautics Company, Houston Division ; [Washington, DC : National Aeronautics and Space Administration, 1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70207

  • Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration [microform] / David E. Hahne.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97104

  • The effect of faster engine response on the lateral directional control of a damaged aircraft / Ryan D. May ... [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo26324

  • Design and integration of an actuated nose strake control system / Bradley C. Flick [and five others].

    • Text
    • Edwards, California. : National Aeronautics and Space Administration, Dryden Flight Research Center, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66653

  • Experimental aerodynamic characteristics of the Pegasus air-launched booster and comparisons with predicted and flight results / M.N. Rhode and W.C. Engelund, M.R. Mendenhall.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1995]
    • 1995
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo77772

  • Experimental aerodynamic characteristics of the Pegasus air-launched booster and comparisons with predicted and flight results / M.N. Rhode and W.C. Engelund, M.R. Mendenhall.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1995]
    • 1995

  • Adaptive variable bias magnetic bearing control / Dexter Johnson and Gerald V. Brown ; Daniel J. Inman.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, April 1998.
    • 1998-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82970

  • A comprehensive C++ controller for a magnetically supported vertical rotor : version 1.0 / Carlos R. Morrison.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2001.
    • 2001-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS22930

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