Books on the topic 'Longitudinal Stability Control'

H, Hardy Gordon, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. 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.

Ostroff, Aaron J. Longitudinal-control design approach for high-angle-of-attack aircraft. Hampton, Va: Langley Research Center, 1993.

S, Proffitt Melissa, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. 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.

Ostroff, 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.

Suit, 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.

Sanjay, Garg, and United States. National Aeronautics and Space Administration., eds. Stable H(infinity) controller design for the longitudinal dynamics of an aircraft. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Stephenson, Jack D. Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA). Moffett Field, Calif: Ames Research Center, 1989.

Mooij, H. A. Criteria for Low-Speed Longitudinal Handling Qualities. Dordrecht: Springer Netherlands, 1985.

Ostroff, 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.

Batterson, James G. Estimation of longitudinal stability and control derivatives for an icing research aircraft from flight data. Hampton, Va: Langley Reserach Center, 1989.

Nationaal Lucht- en Ruimtevaartlaboratorium (Netherlands), ed. 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.

Hinds, 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.

Suit, 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.

M, O'Mara Thomas, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. 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.

L, Berrier Bobby, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. 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.

Reubush, 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.

Iliff, 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.

Iliff, 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.

Iliff, 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.

Iliff, 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.

Iliff, 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.

Center, Ames Research, ed. Reduction of Blade-Vortex Interaction (BVI) noise through X-force control. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

Center, Ames Research, ed. Reduction of Blade-Vortex Interaction (BVI) noise through X-force control. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

Center, Ames Research, ed. Reduction of Blade-Vortex Interaction (BVI) noise through X-force control. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

Center, Ames Research, ed. Reduction of Blade-Vortex Interaction (BVI) noise through X-force control. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

George C. Marshall Space Flight Center., ed. Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept. MSFC, Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1995.

Summary 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.

Longitudinal 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.

National 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.

Determination 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.

A 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.

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.

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.