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  • Active load control during rolling maneuvers [microform] / Jessica A. Woods-Vedeler, Anthony S. Pototzky, and Sherwood T. Hoadley.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service [distributor, 1994]
    • 1994

  • Development of a mulicomponent force and moment balance for water tunnel applications [microform] / Carlos J. Suárez ... [et al.].

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

  • An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities [microform] / C.L. Blanken, H.-J. Pausder and C.J. Ockier.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Roll-yaw control at high angle of attack by forebody tangential blowing [microform] / N. Pedreiro ... [et al.].

    • Text
    • [Stanford, Calif.?] : Joint Institute for Aeronautics and Acoustics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Scuffing characteristics of high-load rolling/sliding contacts operating in liquid oxygen [microform] : effects of materials and surface roughness : technical report for the research conducted under grant/contract no. NAG8-1134 / submitted by L. Chang, [P.B. Hall, R. Thom].

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

  • Experiments in aircraft roll-yaw control using forebody tangential blowing [microform] / Nelson Pedreiro.

    • Text
    • [Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • A theory for the roll-ratchet phenomenon in high performance aircraft [microform] / Ronald A. Hess.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • A parametric study of accelerations of an airplane due to a wake vortex system [microform] / Eric C. Stewart.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Design considerations of manipulator and feel system characteristics in roll tracking [microform] / Donald E. Johnston and Bimal L. Aponso.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58935

  • Determination of shuttle orbiter center of gravity from flight measurements [microform] / E. W. Hinson, J. Y. Nicholson, R. C. Blanchard.

    • Text
    • Hampton, Va. : NASA Langley Research Center, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60549

  • Nonlinear motion cueing algorithm : filtering at pilot station and development of the nonlinear optimal filters for pitch and roll / Kirill B. Zaychik and Frank M. Cardullo.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27991

  • Methods for estimating stability and control derivatives of conventional subsonic airplanes.

    • Text
    • [Lawrence? Kan.], [1971]
    • 1971
    • 1 Item
    FormatCall NumberItem Location
    Text TL574.S7R57Off-site

  • Tandem helicopter lateral stability and control.

    • Text
    • Ft. Belvoir Defense Technical Information Center OCT 1956.
    • 1956
    • 1 Item
    FormatCall NumberItem Location
    Text 92528.847Off-site

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