Livres sur le sujet « Longitudinal Stability Control »
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H, Hardy Gordon, et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA). [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Trouver le texte intégralOstroff, Aaron J. Longitudinal-control design approach for high-angle-of-attack aircraft. Hampton, Va : Langley Research Center, 1993.
Trouver le texte intégralS, Proffitt Melissa, et United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., dir. Longitudinal-control design approach for high-angle-of-attack aircraft. [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
Trouver le texte intégralOstroff, Aaron J. Longitudinal-control design approach for high-angle-of-attack aircraft. [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
Trouver le texte intégralSuit, William T. Lateral and longitudinal stability and control parameters for the space shuttle Discovery as determined from flight test data. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1988.
Trouver le texte intégralSanjay, Garg, et United States. National Aeronautics and Space Administration., dir. Stable H(infinity) controller design for the longitudinal dynamics of an aircraft. [Washington, DC] : National Aeronautics and Space Administration, 1995.
Trouver le texte intégralStephenson, Jack D. Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA). Moffett Field, Calif : Ames Research Center, 1989.
Trouver le texte intégralMooij, H. A. Criteria for Low-Speed Longitudinal Handling Qualities. Dordrecht : Springer Netherlands, 1985.
Trouver le texte intégralOstroff, Aaron J. Redesign of a variable-gain output feedback longitudinal controller flown on the High-Alpha Research Vehicle (HARV). Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1998.
Trouver le texte intégralBatterson, James G. Estimation of longitudinal stability and control derivatives for an icing research aircraft from flight data. Hampton, Va : Langley Reserach Center, 1989.
Trouver le texte intégralNationaal Lucht- en Ruimtevaartlaboratorium (Netherlands), dir. Criteria for low-speed longitudinal handling qualities of transport aircraft with closed-loop flight control systems. Dordrecht : M. Nijhoff for Nationaal Lucht- en Ruimtevaartlaboratorium, National Aerospace Laboratory, NLR, The Netherlands, 1985.
Trouver le texte intégralHinds, H. A. Measurement of the longitudinal static stability and the moments of 0inertia of a 1/12th scale model of a B.Ae Hawk. Cranfield, Bedford : College of Aeronautics, Cranfield Institute of Technology, 1990.
Trouver le texte intégralSuit, William T. Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1986.
Trouver le texte intégralM, O'Mara Thomas, et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. Estimation of longitudinal stability and control derivatives for an icing research aircraft from flight data James G. Batterson, Thomas M. O'Mara. [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Trouver le texte intégralL, Berrier Bobby, et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Trouver le texte intégralReubush, David E. Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane. Hampton, Va : Langley Research Center, 1987.
Trouver le texte intégralIliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif : NASA, Dryden Flight Research Center, 1997.
Trouver le texte intégralIliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif : National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.
Trouver le texte intégralIliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif : National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.
Trouver le texte intégralIliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif : National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.
Trouver le texte intégralIliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif : National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.
Trouver le texte intégralCenter, Ames Research, dir. Reduction of Blade-Vortex Interaction (BVI) noise through X-force control. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1995.
Trouver le texte intégralCenter, Ames Research, dir. Reduction of Blade-Vortex Interaction (BVI) noise through X-force control. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1995.
Trouver le texte intégralCenter, Ames Research, dir. Reduction of Blade-Vortex Interaction (BVI) noise through X-force control. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1995.
Trouver le texte intégralCenter, Ames Research, dir. Reduction of Blade-Vortex Interaction (BVI) noise through X-force control. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1995.
Trouver le texte intégralGeorge C. Marshall Space Flight Center., dir. Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept. MSFC, Ala : National Aeronautics and Space Administration, Marshall Space Flight Center, 1995.
Trouver le texte intégralSummary of longitudinal stability and control parameters as determined from space shuttle Columbia flight test data. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1986.
Trouver le texte intégralLongitudinal stability and control derivatives obtained from flight data of a PA-30 aircraft : Final report. San Luis Obispo, Calif : California Polytechnic State University, Aeronautical Engineering Dept., 1986.
Trouver le texte intégralNational Aeronautics and Space Administration (NASA) Staff. Lateral and Longitudinal Stability and Control Parameters for the Space Shuttle Discovery As Determined from Flight Test Data. Independently Published, 2018.
Trouver le texte intégralDetermination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method : Progress report. Morgantown, WV : West Virginia University, 1995.
Trouver le texte intégralA preliminary evaluation of the generalized likelihood ratio for detecting and identifying control element failures in a transport aircraft. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1985.
Trouver le texte intégralEffects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Trouver le texte intégralEffects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
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