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Airplanes -- Control systems -- Design and construction

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• Airplanes -- Control systems
• Airplanes -- Design and construction

• Airplanes -- Control systems -- Design and construction -- Mathematical models
• Automatic pilot (Airplanes) -- Design and construction

• Simulation development and evaluation of an improved longitudinal velocity-vector control-wheel steering mode and electronic display format (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), by George G. Steinmetz (page images at HathiTrust)
• NASA TM X-3108 (National Aeronautics and Space Administration, 1974), by Robert C. Seidel, Bruce Lehtinen, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Effects of errors on decoupled control systems (National Aeronautics and Space Administration, Scientific and Technical Information Service ;, 1978), by Harold A. Hamer, Katherine G. Johnson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Flight control system design factors for applying automated testing techniques (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Joel R. Sitz, Todd H. Vernon, and Dryden Flight Research Facility (page images at HathiTrust)
• Design and evaluation of a sensor fail-operational control system for a digitally controlled turbofan engine (National Aeronautics and Space Administration ;, 1975), by Frank J. Hrach, Dale J. Arpasi, William M. Bruton, and Lewis Research Center (page images at HathiTrust)
• A knowledge-based system design/information tool (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by James G. Allen, Scott E. Sikora, Dryden Flight Research Facility, and Charles Stark Draper Laboratory (page images at HathiTrust)
• Vehicle design considerations for active control application to subsonic transport aircraft (National Aeronautics and Space Administration ;, 1974), by L. G. Hofmann, Warren F. Clement, Langley Research Center, McDonnell Douglas Astronautics Company-West, and inc Systems Technology (page images at HathiTrust)
• Preliminary system design study for a digital fly-by-wire flight control system for an F-8C aircraft (National Aeronautics and Space Administration ;, 1976), by C. L. Seacord, Darrel Vaughn, Langley Research Center, and Honeywell Inc (page images at HathiTrust)
• Analysis and preliminary design of an advanced technology transport flight control system (National Aeronautics and Space Administration ;, 1975), by Ronald Frazzini, Darrel Vaughn, Langley Research Center, and Honeywell Inc. Government and Aeronautical Products Division (page images at HathiTrust)
• Flight control systems properties and problems (National Aeronautics and Space Administration ;, 1975), by Duane T. McRuer, Donald E. Johnston, Flight Research Center (U.S.), and inc Systems Technology (page images at HathiTrust)
• Stability and control of maneuvering high-performance aircraft (National Aeronautics and Space Administration ;, 1977), by Robert F. Stengel, Paul W. Berry, Analytic Sciences Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• F-8C adaptive flight control extensions (National Aeronautics and Space Administration ;, 1977), by Günter Stein, Gary L. Hartmann, Honeywell Inc, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Detailed design of a ride quality augmentation system for commuter aircraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Reiner Suikat, David R. Downing, Kent E. Donaldson, and Langley Research Center (page images at HathiTrust)
• Summary of design considerations for airplane spin-recovery parachute systems (National Aeronautics and Space Administration ;, 1972), by Sanger M. Burk and Langley Research Center (page images at HathiTrust)
• Flight propulsion control coupling for thrust vectoring fighter aircraft. Volume III, Phase II (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1980., 1980), by Frederick C. Glaser, Douglas Aircraft Company, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Multifunction flight control reference system. Volume 1, Design and development (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by Gene E. Barnard, Sven P. Greenquist, John F. Susek, William J. Luedde, David L. Sebring, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Aircraft Company (page images at HathiTrust)
• Flight test of advanced digital control concepts (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by Richard F. Whitbeck, Thomas T. Myers, James C. Smith, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)

• Integrated autopilot/autothrottle for the NASA TSRV B-737 aircraft : design and verification by nonlinear simulation (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), by Kevin R. Bruce and Langley Research Center (page images at HathiTrust)

• Integrated autopilot/autothrottle for the NASA TSRV B-737 aircraft : design and verification by nonlinear simulation (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), by Kevin R. Bruce and Langley Research Center (page images at HathiTrust)

• Development and flight test of an experimental maneuver autopilot for a highly maneuverable aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Eugene L. Duke, Ralph B. Roncoli, Frank P. Jones, and Ames Research Center (page images at HathiTrust)
• Design of integrated pitch axis for autopilot/autothrottle and integrated lateral axis for autopilot/yaw damper for NASA TSRV airplane using integral LQG methodology (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Isaac Kaminer, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• On the design of a high-gain saturating control system for use as an adaptive autopilot (National Aeronautics and Space Administration, 1960), by John D. McLean, Stanley F. Schmidt, and Ames Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Modern flight dynamics. (Prentice-Hall, 1961), by W. Richard Kolk (page images at HathiTrust)
• Limitations of the pilot in applying forces to airplane controls (National Advisory Committee for Aeronautics, 1936), by Melvin N. Gough, A. P. Beard, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• General aviation operations inspector's handbook (FAA, 1975), by United States Federal Aviation Administration (page images at HathiTrust)
• NASA-University Conference on Manual Control; [proceedings] 2d- 1966- (Scientific and Technical Information Division, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1966), by NASA-University Conference on Manual Control and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Synthesis of flight control systems subject to vehicle parameter variations. (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems command, 1967), by Eliezer Kreindler (page images at HathiTrust)
• Problem of the operational reliability of flight control systems and automatic piloting of aircraft. (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1970), by Olaf Peters (page images at HathiTrust; US access only)
• HIgh acceleration cockpit controller locations (Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1975), by Air Force Flight Dynamics Laboratory (U.S.) and McDonnell Aircraft Company (page images at HathiTrust)
• Aircraft control system hydraulic drives = Gidroprivody aviatsionnykh sistem upravleniya (U.S. National Aeronautics and Space Administration ;, 1976), by V G Neyman and SCITRAN. (page images at HathiTrust)
• Flight control systems development and flight test experience with the HiMAT research vehicles (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Robert W. Kempel, Michael R. Earls, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Development and flight test experiences with a flight-crucial digital control system (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Dale A. Mackall and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• A simulation evaluation of the Engine Monitoring and Control System display (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Terence S. Abbott and Langley Research Center (page images at HathiTrust)
• Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA) (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Jack D. Stephenson, Gordon H. Hardy, and Ames Research Center (page images at HathiTrust)
• Simulated-airline-service flight tests of laminar flow control with perforated-surface suction system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Dal V. Maddalon, Albert L. Braslow, and Langley Research Center (page images at HathiTrust)
• Development of an adaptive failure-detection and identification system for detecting aircraft control-element failures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by W. Thomas Bundick and Langley Research Center (page images at HathiTrust)
• Application and flight test of linearizing transformations using measurement feedback to the nonlinear control problem (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Robert F. Antoniewicz, Eugene L. Duke, P. K. A. Menon, and Dryden Flight Research Facility (page images at HathiTrust)
• Control integration concept for hypersonic cruise-turn maneuvers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David L. Raney, Frederick J. Lallman, and Langley Research Center (page images at HathiTrust)
• Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Francis J. Capone, Mary L. Mason, and Langley Research Center (page images at HathiTrust)
• Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by E. Ann Bare, Raymond C. Haddad, David E. Reubush, and Langley Research Center (page images at HathiTrust)
• Development and flight test results of an autothrottle control system at Mach 3 cruise (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Glenn B. Gilyard, John J. Burken, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Hugh L. Dryden Flight Research Center (page images at HathiTrust)
• A Preliminary investigation of the use of throttles for emergency flight control (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Frank W. Burcham and Dryden Flight Research Facility (page images at HathiTrust)
• A Simulation evaluation of a four-engine jet transport using engine thrust modulation for flightpath control (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Glenn B. Gilyard and Dryden Flight Research Facility (page images at HathiTrust)
• Variable-camber systems integration and operational performance of the AFTI/F-111 mission adaptive wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program , 1992), by John W. Smith, Gordon A. Payne, Wilton P. Lock, and Dryden Flight Research Facility (page images at HathiTrust)
• Flight investigation of cockpit-displayed traffic information utilizing coded symbology in an advanced operational environment (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Terence S. Abbott, Army Research and Technology Laboratories (U.S.). Structures Laboratory, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Mary L. Mason, Scott C. Asbury, Francis J. Capone, and Langley Research Center (page images at HathiTrust)
• Integrated flight propulsion control research results using the NASA F-15 HIDEC flight research facility (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by James F. Stewart and Dryden Flight Research Facility (page images at HathiTrust)
• Flight-determined benefits of integrated flight-propulsion control systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by James F. Stewart, Donald H. Gatlin, Frank W. Burcham, and Dryden Flight Research Facility (page images at HathiTrust)
• Simulation of a cockpit-display concept for executing a wake vortex avoidance procedure (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Terence S. Abbott and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Simulation comparison of a decoupled longitudinal control system and a velocity-vector control wheel steering system during landings in wind shear (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by G. Kimball Miller, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Piloted simulator study of allowable time delays in large-airplane response (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by William D. Grantham and Langley Research Center (page images at HathiTrust)
• Description of path-in-the-sky contact analog piloting display (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1977), by Charles E. Knox, John Leavitt, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Piloted simulation of an algorithm for onboard control of time-optimal intercept (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Douglas B. Price, Daniel D. Moerder, Anthony J. Calise, and Langley Research Center (page images at HathiTrust)
• NASA aviation safety reporting system : Quarterly report no. 13. (National Aeronautics and Space Administration, Scientific and Technical Information Branch :, 1981), by Aviation Safety Reporting System (U.S.), Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Simulator evaluation of the effects of reduced spoiler and thrust authority on a decoupled longitudinal control system during landings in wind shear (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by G. Kimball Miller, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aircraft ground tests and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Steven A. Johnson and Dryden Flight Research Facility (page images at HathiTrust)
• Simulator evaluation of a flight-path-angle control system for a transport airplane with direct lift control (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Wendell W. Kelley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Development and application of an optimization procedure for flutter supression using the aerodynamic energy concept (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by E. Nissim, Irving Abel, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Pilot-model analysis and simulation study of effect of control task desired control response (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by James J. Adams, Joel B. Jaudon, Joseph Gera, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Flight evaluation of the transonic stability and control charcteristics of an airplane incorporating a supercritical wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Neil W. Matheny, Donald H. Gatlin, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Analytical study of ride smoothing benefits of control system configurations optomized for pilot handling qualities (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Bruce G. Powers and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by David E. Hahne and Langley Research Center (page images at HathiTrust)
• Experimental characterization of the effects of pneumatic tubing on unsteady pressure measurements (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Stephen A. Whitmore and Dryden Flight Research Facility (page images at HathiTrust)
• Three input concepts for flight crew interaction with information presented on a large-screen electronic cockpit display (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Denise R. Jones and Langley Research Center (page images at HathiTrust)
• Propulsion system/flight control integration and optimization : flight evaluation and technology transition (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Frank W. Burcham, Lawrence P. Myers, Glenn B. Gilyard, and Dryden Flight Research Facility (page images at HathiTrust)
• An experimental investigation of thrust vectoring two-dimensional covergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Francis J. Capone, Laurence D. Leavitt, Mary L. Mason, and Langley Research Center (page images at HathiTrust)
• Simulator study of a flight director display (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by James J. Adams and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Wendell W. Kelley, Einar K. Enevoldson, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Hugh L. Dryden Flight Research Center, and Langley Research Center (page images at HathiTrust)
• Piloted simulator study of allowable time delay in pitch flight control system of a transport airplane with negative static stability (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by William D. Grantham and Langley Research Center (page images at HathiTrust)
• Optimal regulation in systems with stochastic time sampling (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Raymond C. Montgomery, Peter S. Lee, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Important factors in the maximum likelihood analysis of flight test maneuvers (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Kenneth W. Iliff, T. D. Montgomery, Richard E. Maine, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Three methods of presenting flight vector information in a head-up display during simulated STOL approaches (National Aeronautics and Space Administration ;, 1975), by James H. Dwyer, Everett A. Palmer, and Ames Research Center (page images at HathiTrust)
• Effects of cable geometry and aircraft attitude on the accuracy of a magnetic leader cable system for aircraft guidance during rollout and turnoff (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by W. Thomas Bundick, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Configuration management and automatic control of an augmentor wing aircraft with vectored thrust (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Luigi S. Cicolani, George Meyer, B. Sridhar, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Ames Research Center (page images at HathiTrust)
• Effects of curved approach paths and advanced displays on pilot scan patterns (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Randall L. Harris, Randolph W. Mixon, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Results from tests, with van-mounted sensor, of magnetic leader cable for aircraft guidance during roll-out and turnoff (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by James C. Young, Stewart H. Irwin, W. Thomas Bundick, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Flight test of the slide-slope track and flare-control laws for an automatic landing system for a powered-lift STOL airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by DeLamar M. Watson, David N. Warner, Gordon H. Hardy, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Diversity techniques for omnidirectional telemetry coverage of the HiMAT research vehicle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Paul F. Harney, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Hugh L. Dryden Flight Research Center (page images at HathiTrust)
• Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David J. Wing, Scott C. Asbury, and Langley Research Center (page images at HathiTrust)
• Nonlinear adaptive control systems with storage (National Aeronautics and Space Administration :, 1964), by Naresh K. Sinha, United States National Aeronautics and Space Administration, and University of Tennessee (System) (page images at HathiTrust)
• Stability of multirate sampled-data systems (National Aeronautics and Space Administration ;, 1975), by David P. Stanford, Alper K. Caglayan, Langley Research Center, and College of William and Mary (page images at HathiTrust)
• Research in digital adaptive flight controllers (U.S. National Aeronautics and Space Administration ;, 1976), by Howard Kaufman, United States National Aeronautics and Space Administration, Langley Research Center, and Rensselaer Polytechnic Institute (page images at HathiTrust)
• Digital flight control research (National Aeronautics and Space Administration, 1974), by James E. Potter, Langley Research Center, and Massachusetts Institute of Technology. Measurement Systems Laboratory (page images at HathiTrust)
• Application of active controls technology to the NASA JetStar airplane (National Aeronautics and Space Administration ;, 1975), by R. H. Lange, Flight Research Center (U.S.), and Lockheed-Georgia Company (page images at HathiTrust)
• F-8C digital CCV flight control laws (U.S. National Aeronautics and Space Administration ;, 1976), by Gary L. Hartmann, Russell C. Hendrick, James A. Hauge, Honeywell Systems and Research Center, and Langley Research Center (page images at HathiTrust)
• Lightning effects on the NASA F-8 digital-fly-by-wire airplane (National Aeronautics and Space Administration, 1975), by J. A. Plumer, L. C. Walko, F. A. Fisher, and Pittsfield General Electric Company (page images at HathiTrust)
• A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume III, Propulsion subsystems, performance, stability and control, propellers, and flight safety (National Aeronautics and Space Administration ;, 1970), by Clifford J. Moore, Dennis M. Phillips, Langley Research Center, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• XB-70 structural mode control system design and performance analyses (National Aeronautics and Space Administration, 1970), by John H. Wykes, Alva S. Mori, Louis U. Nardi, United States National Aeronautics and Space Administration, Flight Research Center (U.S.), and North American Rockwell Corporation (page images at HathiTrust)
• Development of approach control system requirements with applications to a jet transport (National Aeronautics and Space Administration ;, 1972), by Duane T. McRuer, Walter A. Johnson, Ames Research Center, and inc Systems Technology (page images at HathiTrust)
• Study of load alleviation and mode suppression (LAMS) on the YF-12A airplane (National Aeronautics and Space Administration ;, 1972), by Lester D. Edinger, Alan R. Curtis, Frederick L. Schenk, Flight Research Center (U.S.), Honeywell Inc, and Lockheed Aircraft Corporation (page images at HathiTrust)
• Insensitive control technology development (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Charles Arthur Harvey, R. E. Pope, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Design, implementation and flight testing of PIF autopilots for general aviation aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by John R. Broussard, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Reliable dual-redundant sensor failure detection and identification for the NASA F-8 DFBW aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by James C. Deckert, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• An analysis of aerodynamic requirements for coordinated bank-to-turn autopilots (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by A. Arrow, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Johns Hopkins University. Applied Physics Laboratory (page images at HathiTrust)
• Assessment of flying-quality criteria for air-breathing aerospacecraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Duane T. McRuer, Dryden Flight Research Facility, and inc Systems Technology (page images at HathiTrust)
• Effects of cockpit lateral stick characteristics on handling qualities and pilot dynamics (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David G. Mitchell, David H. Klyde, Bimal L. Aponso, Dryden Flight Research Facility, Inc PRC, and inc Systems Technology (page images at HathiTrust)
• A combined stochastic feedforward and feedback control design methodology with application to autoland design (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987), by Nesim Halyo and Langley Research Center (page images at HathiTrust)
• Optimal cooperative control synthesis of active displays (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987), by Sanjay Gary, D. K. Schmidt, and Dryden Flight Research Facility (page images at HathiTrust)
• Integrated application of active controls (IACC) technology to an advanced subsonic transport : project plan (National Aeronautics and Space Admininstration, Scientific and Technical Information Branch ;, 1981), by Boeing Commercial Airplane Company, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Integrated airframe propulsion control (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Robert E. Fennell, Stephen B. Black, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Stability and control of the Gossamer human-powered aircraft by analysis and flight test (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Henry R. Jex, David G. Mitchell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, inc Systems Technology, and Hugh L. Dryden Flight Research Center (page images at HathiTrust)
• Statistics of some atmospheric turbulence records relevant to aircraft response calculations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by William D. Mark, Raymond W. Fischer, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Characterization, parameter estimation, and aircraft response statistics of atmospheric turbulence (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by William D. Mark, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Design considerations of manipulator and feel system characteristics in roll tracking (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Donald E. Johnston, Bimal L. Aponso, and Dryden Flight Research Facility (page images at HathiTrust)
• Development and demonstration of a flutter-suppression system using active controls (National Aeronautics and Space Administration ;, 1975), by M. C. Sandford, David L. Gray, Irving Abel, and Langley Research Center (page images at HathiTrust)
• Development of a remote digital augmentation system and application to a remotely piloted research vehicle (National Aeronautics and Space Administration ;, 1975), by John W. Edwards, Dwain A. Deets, and Flight Research Center (U.S.) (page images at HathiTrust)
• NASA TN D-5298 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Wilton P. Lock, Shu W. Gee, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5299 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Harold G. Gaidsick, Robert C. McCracken, William H. Dana, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moving-base visual simulation study of decoupled controls during approach and landing of a STOL transport aircraft (National Aeronautics and Space Administration ;, 1975), by G. Kimball Miller, Perry L. Deal, and Langley Research Center (page images at HathiTrust)
• An analytical study and wind-tunnel tests of an aeromechanical gust-alleviation system for a light airplane (National Aeronautics and Space Administration ;, 1976), by Eric C. Stewart (page images at HathiTrust)
• Subsonic stability and control derivatives for an unpowered, remotely piloted 3/8 scale F-15 airplane model obtained from flight test (National Aeronautics and Space Administration ;, 1976), by Kenneth W. Iliff, Mary F. Shafer, Richard E. Maine, and Flight Research Center (U.S.) (page images at HathiTrust)
• Investigation of a digital automatic aircraft landing system in turbulence (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by Frank Neuman and John D. Foster (page images at HathiTrust; US access only)
• A method for the analysis of nonlinearities in aircraft dynamic response to atmospheric turbulence. (National Aeronautics and Space Administration ;, 1976), by Kenneth Sidwell (page images at HathiTrust)
• Analysis of a flare-director concept for an externally blown flap STOL aircraft (National Aeronautics and Space Administration ;, 1974), by David B. Middleton (page images at HathiTrust)
• Application of the aerodynamic energy concept to flutter suppression and gust alleviation by use of active controls (National Aeronautics and Space Administration ;, 1976), by E. Nissim, A. Caspi, I. Lottati, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Low-speed wind-tunnel tests of 1/10-scale model of a blended-arrow supersonic cruise aircraft (National Aeronautics and Space Administration ;, 1977), by H. Clyde McLemore, Lysle P. Parlett, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Recent advances in aerodynamic energy concept for flutter suppression and gust alleviation using active controls. (National Aeronautics and Space Administration ;, 1977), by E. Nissim, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Development and flight tests of a gyro-less wing leveler and directional autopilot (National Aeronautics and Space Administration ;, 1974), by H. Douglas Garner, Harold E. Poole, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of static longitudinal and lateral characteristics of a full-scale mockup of a light single-engine high-wing airplane (National Aeronautics and Space Administration ;, 1973), by H. Douglas Greer and Langley Research Center (page images at HathiTrust)
• Flight-determined derivatives and dynamic characteristics for the HL-10 lifting body vehicle at subsonic and transonic Mach numbers (National Aeronautics and Space Administration ;, 1972), by Larry W. Strutz and Flight Research Center (U.S.) (page images at HathiTrust)
• Fixed-base-simulator evaluation of a pilot's terrain-following display with various modes of presenting information (National Aeronautics and Space Administration, 1964), by Thomas E. Wempe, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Flight-determined stability and control characteristics of the M2-F3 lifting body vehicle (National Aeronautics and Space Administration ;, 1973), by Alex G. Sim and Flight Research Center (U.S.) (page images at HathiTrust)
• Flight investigation of a structural mode control system for the XB-70 aircraft (National Aeronautics and Space Administration ;, 1973), by Wilton P. Lock and Flight Research Center (U.S.) (page images at HathiTrust)
• Flight evaluation of advanced control systems and displays on a general aviation airplane (National Aeronautics and Space Administration ;, 1974), by Paul C. Loschke and Flight Research Center (U.S.) (page images at HathiTrust)
• Monte Carlo analysis of inaccuracies in estimated aircraft parameters caused by unmodeled flight instrumentation errors (National Aeronautics and Space Administration ;, 1975), by Ward F. Hodge, Wayne H. Bryant, and Langley Research Center (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Harold I. Johnson, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Investigation of the multiple model adaptive control (MMAC) method for flight control systems (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Michael Athans and Langley Research Center (page images at HathiTrust)
• Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. (National Advisory Committee for Aeronautics, 1957), by Harold L. Crane, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• A method for predicting the stability in roll of automatically controlled aircraft based on the experimental determination of the characteristics of an automatic pilot (National Advisory Committee for Aeronautics, 1949), by Robert T. Jones, Leonard Sternfield, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A theoretical analysis of the effect of time lag in an automatic stabilization system on the lateral oscillatory stability of an airplane (National Advisory Committee for Aeronautics, 1950), by Leonard Sternfield, Ordway B. Gates, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A survey of stability analysis techniques for automatically controlled aircraft (National Advisory Committee for Aeronautics, 1951), by Arthur L. Jones, Benjamin R. Briggs, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flight investigation of a mechanical feel device in an irreversible elevator control system of a large airplane (National Advisory Committee for Aeronautics, 1951), by B. Porter Brown, James B. Whitten, Robert G. Chilton, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Dynamics of mechanical feedback-type hydraulic servomotors under inertia load (National Advisory Committee for Aeronautics, 1952), by Harold Gold, Victor L. Ransom, Edward W. Otto, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Controllability of the X-15 research airplane with interim engines during high-altitude flights (National Aeronautics and Space Administration, 1961), by Euclid C. Holleman, Donald Reisert, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Several factors affecting roll control systems of interceptors (National Advisory Committee for Aeronautics, 1953), by Leonard Sternfield, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• A free-flight investigation at high subsonic and low supersonic speeds of the rolling effectiveness and drag of three spoiler controls having potentially low actuating-force requirements (National Advisory Committee for Aeronautics, 1955), by Eugene D. Schult, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), by Harold I. Johnson, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• General principles of designing control systems (National Aeronautics and Space Administration ;, 1974), by O. A. Chembrovskiĭ, Georgiĭ Vladimirovich Samoǐlovich, and I︠U︡. I. Topcheev (page images at HathiTrust)
• Bureau of Aeronautics flight control system manuals (The Division, 1959), by Northrop Corporation. NORAIR Division and United States. Navy Department. Bureau of Aeronautics (page images at HathiTrust; US access only)
• The evaluation of a digital hardware voter/monitor in an aircraft control system (Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1977), by Harry W. Schreadley, Air Force Flight Dynamics Laboratory (U.S.), and inc Dynamic Controls (page images at HathiTrust)
• Control of supersonic aircraft. (Wright-Patterson Air Force Base, Ohio, 1966), by Feliko Iosifovich Sklianskii (page images at HathiTrust)
• Development of a command control and communications system for light aircraft (Hanscom AFB, Massachusetts : Aerospace Instrumentation Division, Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1983., 1983), by Alan R. Griffin, United States. Air Force. Systems Command, and U.S. Air Force Geophysics Laboratory. Aerospace Instrumentation Division (page images at HathiTrust)
• Aircraft accident report : inadvertent in-flight slat deployment, China Eastern Airlines flight 583, McDonnell Douglas MD-11, B-2171, 950 nautical miles south of Shemya, Alaska, April 6, 1993. (National Transportation Safety Board ;, 1993), by United States. National Transportation Safety Board (page images at HathiTrust)
• Analytical sensor redundancy assessment (FAA Technical Center ;, 1988), by D. B. Mulcare, M. K. Smith, L. E. Downing, Federal Aviation Administration Technical Center (U.S.), and Lockheed-Georgia Company (page images at HathiTrust)
• Advanced flight vehicle self-adaptive flight control system : part IV -- notch filter development (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, U.S. Air Force, 1962., 1961), by M. W. Reed, D. L. Mellen, J. A. Wolfe, United States. Air Force. Air Research and Development Command, and Wright Air Development Division (page images at HathiTrust)
• Transfer of tracking performance as a function of a delay between the control and the display (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1953., 1953), by Marvin Levine, United States. Air Force. Air Research and Development Command, Wright Air Development Center, Antioch College, and Aerospace Medical Laboratory (U.S.) (page images at HathiTrust)
• Transfer of training in a simple motor skill along the speed dimension (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1954, 1954), by Robert B. Ammons, Ross L. Morgan, Carol H. Ammons, United States. Air Force. Air Research and Development Command, Wright Air Development Center, Aerospace Medical Laboratory (U.S.), and University of Louisville. Department of Psychology (page images at HathiTrust)
• Effects of variations in control deadspace and gain on tracking performance (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1957., 1957), by Marty R. Rockway, United States. Air Force. Air Research and Development Command, Wright Air Development Center, Aerospace Medical Laboratory (U.S.), and Ohio State University (page images at HathiTrust)
• The Air Force program for improved flight instrumentation (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 56-582., 1956), by Lawrence C. Wright, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• Analysis of digital flight control systems with flying qualities applications. Volume I, Executive summary (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), by Richard F. Whitbeck, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
• Effect of backlash on manual control of pitch of a simulated aircraft (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1956., 1956), by John W. Senders, James V. Bradley, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Aerospace Medical Laboratory (U.S.) (page images at HathiTrust)
• The effect of variations in control-display ratio and exponential time delay on tracking performance (Wright-Patterson Air Force Base, Ohio : Aero Medical Laboratory, Wright Air Development Center, Air Research and Development Command, United States Air Force, 1954., 1954), by Marty R. Rockway, Wright Air Development Center, United States. Air Force. Air Research and Development Command, Aerospace Medical Laboratory (U.S.), and Ohio State University (page images at HathiTrust)
• Analysis of limited authority manual control systems (Wright-Patterson AFB, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by Lee Gregor Hofmann, Dunstan Graham, Kishor V. Shah, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
• The effect of variations in control-display during training on transfer to a "high" ratio (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1955., 1955), by Marty R. Rockway, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Aerospace Medical Laboratory (U.S.) (page images at HathiTrust)
• Control-display association preferences for ganged controls (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1954., 1954), by James V. Bradley, Wright Air Development Center, United States. Air Force. Air Research and Development Command, and Antioch College (page images at HathiTrust)
• (Unclassified title) : summary and status of adaptive control system program (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research Development and Command, United States Air Force, 1958, 1958), by Raymond R. Rath, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• Flight investigation of fighter side-stick force-deflection characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1975., 1975), by G. Warren Hall, Rogers E. Smith, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Man-machine tracking performance with short-period oscillatory control system transients (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Frederick A. Muckler, United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command, and University of Illinois (Urbana-Champaign campus). Aviation Research Laboratory (page images at HathiTrust)
• Human pilot dynamic response in single-loop systems with compensatory and pursuit displays (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by R. J. Wasicko, R. E. Magdaleno, Duane T. McRuer, Wright-Patterson Air Force Base (Ohio), Inc Systems Technology, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Airplane flying characteristics in turbulence (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by E. D. Onstott, E. P. Salmon, Northrop Corporation. Aircraft Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Digital simulation of a Gaussian random process having an exponential autocorrelation function (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), by D. K. Bowser, G. R. Schubert, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• New approaches to human-pilot/vehicle dynamic analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), by Duane T. McRuer, Julian Wolkovitch, D. H. Weir, Anil V. Phatak, G. P. Moore, Henry R. Jex, L. G. Hofmann, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
• Handling qualities in single-loop roll tracking tasks : theory and simulator experiments (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by T. S. Durand, Henry R. Jex, United States. Air Force. Systems Command. Aeronautical Systems Division, and Inc Systems Technology (page images at HathiTrust)
• Investigation of measuring system requirements for instrument low visibility approach (Wright-Patterson AFB, Ohio : Air Force Flight Dynamics Laboratory, Aeronautical Systems Division, United States Air Force, 1971., 1971), by Dunstan Graham, Lee Gregor Hofmann, Warren F. Clement, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and Inc Systems Technology (page images at HathiTrust)
• Magnitude of forces which may be applied by the prone pilot to aircraft control devices. [Part] 3, Foot controls (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Air Materiel Command, 1949., 1949), by Clarence W. Brown, Robert M. U'Ren, Edward W. Minium, Rheem F. Jarrett, Edwin E. Ghiselli, Berkeley University of California, and United States. Air Force. Air Matériel Command (page images at HathiTrust)
• Effects of variations in control backlash and gain on tracking performance (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, [1959], 1959), by Marty R. Rockway, Paul E. Franks, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• Influence of forebody geometry on aerodynamic characteristics and a design guide for defining departure/spin resistant forebody configurations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), by William Bihrle, E. Dickes, B. Barnhart, Inc Bihrle Applied Research, Wright Research and Development Center, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Output feedback control and sensor placement for a hypersonic vehicle model : preprint (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2006., 2006), by Pete Jankovsky, David B. Doman, Michael A. Bolender, Stephan Yurkovich, Andrea Serrani, David O. Sigthorsson, Ohio State University. Department of Electrical and Computer Engineering, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Magnitude of forces which may be applied by the prone pilot to aircraft control devices. [Part] 2, Two-dimensional hand controls (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Air Materiel Command, 1949., 1949), by Clarence W. Brown, Robert M. U'Ren, Edward W. Minium, Rheem F. Jarrett, Edwin E. Ghiselli, Berkeley University of California, and United States. Air Force. Air Matériel Command (page images at HathiTrust)
• Influence of friction in making settings on a linear scale (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Air Materiel Command, 1949., 1949), by William Leroy Jenkins, David Rigler, Louis O. Maas, Lehigh University, and United States. Air Force. Air Matériel Command (page images at HathiTrust)
• A study of digitally controlled flight control actuation (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), by Howard H. Belmont, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Hydraulic Research Textron (Firm) (page images at HathiTrust)
• Static and rotational aerodynamic data from O° to 90° angle of attack for a series of basic and altered forebody shapes (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), by William Bihrle, E. Dickes, B. Barnhart, Inc Bihrle Applied Research, Wright Research and Development Center, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Speed of reaching to critical control areas in a fighter-type cockpit (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by M. R. Green, F. A. Muckler, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Martin Company (page images at HathiTrust)
• F/A-18 forebody vortex control (National Aeronautics and Space Administration, Ames Research Center, 1994), by Brian R. Kramer and Ames Research Center (page images at HathiTrust)

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