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  • First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop [microform] : proceedings of a workshop held at Langley Research Center, Hampton, Virginia, February 27-29, 1996 / edited by Richard M. Wood.

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

  • Robust stability of second-order systems [microform] / Dr. C.-H. Chuang.

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

  • Antiwindup analysis and design aproaches for MIMO systems [microform] / Vincent R. Marcopoli and Stephen M. Phillips.

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

  • Robust control design with real parameter uncertainty using absolute stability theory [microform] / Jonathan P. How, Steven R. Hall.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • A new approach to mixed H2/H [infinity]-controller synthesis using gradient-based parameter optimization method [microform] : final technical report ... for the period of March 15, 1900 to March 14, 1993 / Uy-Loi Ly, Ewald Schömig.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Control strategies for systems with limited actuators [microform] / Vincent R. Marcopoli and Stephen M. Phillips.

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

  • Stable H(infinity) controller design for the longitudinal dynamics of an aircraft [microform] / Hitay Ozbay and Sanjay Garg.

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

  • NASA/DOD control/structures interaction technology, 1986 [microform] : proceedings of a conference sponsored by NASA Langley Research Center, Hampton, Virginia, and Air Force Wright Aeronautical Laboratories, Wright-Patterson, AFB, Ohio, and held in Norfolk, Virginia, November 18-21, 1986 / compiled by Robert L. Wright.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1987-
    • 1987-present

  • Flight test report of the NASA icing research airplane [microform] : performance, stability, and control after flight through natural icing conditions / Jerry L. Jordan, Stewart J. Platz, and William C. Schinstock.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • 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

  • TAILSIM users guide [microform] / Dale W. Hiltner ; prepared under grant NAG3-2007.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2000]
    • 2000

  • Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops [microform] / Zachary T. Applin and Paul L. Coe, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986

  • A method to stabilize linear systems using eigenvalue gradient information [microform] / Carol D. Wieseman.

    • 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

  • Wind-tunnel investigation of a full-scale canard-configured general aviation airplane [microform] / Long P. Yip.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS54941

  • Integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques [microform] / Sanjay Garg and Peter J. Ouzts.

    • Text
    • [Cleveland, Ohio : Lewis Research Center, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64062

  • Dynamic and control assessment of the Space Station Freedom payload pointing system [microform] / David T. Shannon, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64155

  • A piloted simulation of helicopter air combat to investigate effects of variations in selected performance and control response characteristics [microform] / Michael S. Lewis, M. Hossein Mansur, Robert T. N. Chen.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center : U.S. Army Aviation Systems Command, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92577

  • Flight test experience with pilot-induced-oscillation suppression filters [microform] / Mary F. Shafer, ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984.
    • 1984

  • Dynamic modeling and adaptive control for space stations [microform] / Che-Hang Charles Ih, Shyh Jong Wang.

    • Text
    • Pasadena, Calif. : National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology, [1985]
    • 1985

  • Design and test plans for a non-nuclear fission power system technology demonstration unit / Lee Mason ... [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27080

  • Stability robustness improvement of direct eigenspace assignment based feedback systems using singular value sensitivities / Sanjay Garg.

    • Text
    • Cleveland, Ohio : Sverdrup Technology, Inc. : Lewis Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo29946

  • Stability and control characteristics at transonic speeds of a model of a supersonic target drone with differentially deflected horizontal-tail surfaces / by Dewey E. Wornom.

    • Text
    • Washingon : National Aeronautics and Space Administration, March 1961.
    • 1961-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173089

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