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  • 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

  • Piloted evaluation of an integrated methodology for propulsion and airframe control design [microform] / Michelle M. Bright ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Adelphi, Md.] : U.S. Army Research Laboratory ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • STOVL Control Integration Program [microform] / C. Weiss, P. McDowell and S. Watts.

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

  • Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft [microform] / Sanjay Garg and Duane Mattern.

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

  • Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft [microform] / Barbara S. Esker and James R. DeBonis.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Aerodynamics model for a generic ASTOVL lift-fan aircraft [microform] / Lourdes G. Birckelbaw, Walter E. McNeill, and Douglas A. Wardwell.

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

  • Simulation model of the integrated flight/propulsion control system, displays, and propulsion system for an ASTOVL lift-fan aircraft [microform] / William W. Y. Chung, Paul F. Borchers, and James A. Franklin.

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

  • Moving base simulation of an integrated flight and propulsion control system for an ejector-augmentor STOVL aircraft in hover [microform] / Walter E. McNeill ... [et al.].

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

  • Moving base simulation of an ASTOVL Lift-fan aircraft [microform] / William W.Y. Chung, Paul F. Borchers, and James A. Franklin.

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

  • Integrator windup protection [microform] : techniques and a STOVL aircraft engine controller application : final report / K. KrishnaKumar, S. Narayanaswamy.

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

  • Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover [microform] / James A. Franklin and Michael W. Stortz.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet [microform] / Richard E. Kuhn.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Moving-base simulation evaluation of control/display integration issues for ASTOVL aircraft [microform] / James A. Franklin.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • The effects of crossflow on the pressures and lift induced by the fountain generated between two impinging jets [microform] / Richard E. Kuhn.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Numerical investigation of hot gas ingestion by STOVL aircraft [microform] : prepared under grant NAG3-1026 / S.P. Vanka.

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

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