Automatic pilot (Airplanes) -- Design and construction
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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)
- 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)
Items below (if any) are from related and broader terms.
Filed under: Automatic pilot (Airplanes)- Copies of slides to be presented for NACA Conference on Automatic Stability and Control of Aircraft, Ames Aeronautical Laboratory, Moffett Field, Calif., March 29 and 30, 1955. (Washington, 1955), by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Flight control system manuals. (The Division], 1952), by Inc. Northrop Aircraft and United States. Navy Dept. Bureau of Aeronautics (page images at HathiTrust)
- Flight text of an autopilot installation as a lateral gust alleviator in a PT-26 airplane. (Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1956), by Charles Chalk (page images at HathiTrust)
- A feasibility study of self-learning adaptive flight control for high performance aircraft (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1967), by Stephen G. Hoppe, Claron W. Swonger, and Semmelhack Henry P. (page images at HathiTrust)
- Flight tests of the total automatic flight control system (TAFCOS) concept on a DHC-6 Twin Otter aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by William R. Wehrend, George Meyer, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Ames Research Center (page images at HathiTrust)
- Design criteria for flightpath and airspeed control for the approach and landing of STOL aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by James A. Franklin, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Ames Research Center (page images at HathiTrust)
- A nonlinear trajectory command generator for a digital flight-control system (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Luigi S. Cicolani, Stein Weissenberger, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (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)
- 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)
- 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)
- The effects of display and autopilot functions on pilot workload for single pilot instrument flight rule (SPIFR) operations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Roger H. Hoh, David A. Hinton, and James C. Smith (page images at HathiTrust)
- A formal structure for advanced automatic flight-control systems (National Aeronautics and Space Administration ;, 1975), by George Meyer, Luigi S. Cicolani, and Ames Research Center (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)
- 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)
- The effects of an autopilot on airplane responses to turbulence with emphasis on tail loads (National Aeronautics and Space Administration ;, 1973), by Boyd Perry, United States National Aeronautics and Space Administration, and Langley Research Center (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)
- An investigation of the stability of a system composed of a subsonic canard airframe and a canted-axis gyroscope automatic pilot (National Advisory Committee for Aeronautics, 1950), by Robert A. Gardiner, H. O. Ankenbruck, Jacob Zarovsky, 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)
- A theoretical method of determining the control gearing and time lag necessary for a specified damping of an aircraft equipped with a constant-time-lag autopilot (National Advisory Committee for Aeronautics, 1951), by Ordway B. Gates, Albert A. Schy, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A flight and analytical study of methods for reducing automatic-interceptor tracking errors caused by target maneuvers (National Advisory Committee for Aeronautics, 1956), by Charles W. Mathews, Howard C. Kyle, Donald C. Cheatham, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Fundamentals of design of piloted aircraft flight control systems. (U.S. Govt. Print. Off.], 1952), by United States. Navy Department. Bureau of Aeronautics, C. L. Bates, and Duane T. McRuer (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)
- Standard performance criteria for autopilot/coupler equipment (Radio Technical Commission for Aeronautics, 1963), by Radio Technical Commission for Aeronautics (U.S.). Special Committee 79 (page images at HathiTrust)
- The Gyroscope through the ages. (Sperry Gyroscope Co., Inc., 1946), by inc Sperry Gyroscope Company (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)
- Research and feasibility study to achieve reliability in automatic flight control systems (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Wright Air Development Division, Air Research and Development Command, U.S. Air Force, 1960., 1960), by J. J. Fleck, M. F. Marx, G. T. Sendzuk, D. M. Merz, J. C. Kemp, United States. Air Force. Air Research and Development Command, Wright Air Development Division, and General Electric Company (page images at HathiTrust)
- Analysis of two nonlinear flight control systems. Part I, Liapounov-Lurje approach to a simplified pitch rate autopilot. Part II, Analysis of a high-gain adaptive pitch rate autopilot (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1964., 1964), by T. R. Alex, C. R. Heermann, Air Force Flight Dynamics Laboratory (U.S.), General Dynamics Corporation. Astronautics Division, and United States. Air Force. Systems Command. Aeronautical Systems Division (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)
- Integrated autopilot/autothrottle based on a total energy control concept : design and evaluation of additional autopilot modes (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Kevin R. Bruce and Langley Research Center (page images at HathiTrust)
- Programmed text : gyrocompass failure. (U.S. Army Aviation Center, 1985), by U.S. Army Aviation Center (page images at HathiTrust)
- DS, GS, and depot maintenance manual : controllers, flight, automatic pilot C-3107/ASW-12(V) and C-3107A/ASW-12(V), and panel, directional control SB-1453/ASW-12(V). (Headquarters, Dept. of the Army, 1989), by United States. Department of the Army (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)
- Interfaces between flightcrews and modern flight deck systems (the Administration, 1996), by United States. Federal Aviation Administration. Human Factors Team (page images at HathiTrust)
- NASA TN D-1782 (National Aeronautics and Space Administration ;, 1963), by James J. Adams, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Human factors for flight deck certification personnel (U.S. Department of Transportation, Federal Aviation Administration, Research and Development Service ;, 1993), by M. Stephen Huntley, Kim M. Cardosi, and United States. Federal Aviation Administration. Research and Development Service (page images at HathiTrust)
- Radium hazard in a military aircraft instrument shop : final report (San Francisco, California : U.S. Naval Radiological Defense Laboratory, 1951., 1951), by R. K. Skow, Willa Wadleigh, O. J. Sobol, U.S. Naval Radiological Defense Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
- Training evaluation of an instrument panel homogeneous with respect to the principle of the moving part (Wright-Patterson Air Force Base, Ohio, Aero Medical Laboratory, Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1957., 1957), by Robert C. Houston, M. R. Green, United States. Air Force. Air Research and Development Command, Wright Air Development Center, Aerospace Medical Laboratory (U.S.), and University of Illinois (Urbana-Champaign campus). Aviation Psychology Laboratory (page images at HathiTrust)
- Psychological variables in the design of flight simulators for training (Wright-Patterson Air Force Base, Ohio, Aero Medical Laboratory, Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1959., 1959), by F. A. Muckler, United States. Air Force. Air Research and Development Command, Wright Air Development Center, Aerospace Medical Laboratory (U.S.), and University of Illinois (Urbana-Champaign campus). Aviation Psychology Laboratory (page images at HathiTrust)
- Instrumentation package for inflight physiological studies (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by M. N. Goldberg, W. V. Blockley, R. A. Mills, Aerospace Medical Laboratory, North American Aviation, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development 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)
- An impulse accelerometer (Lawrence Radiation Laboratory, 1964), by William E. Nelson, G. Wayne Brown, and Lawrence Radiation Laboratory (page images at HathiTrust)
- The design and construction of a recording accelerometer (1909), by Robert Beam Rodgers (page images at HathiTrust; US access only)
- A rigidly forced oscillation system for meaasuring dynamic-stability parameters in transonic and supersonic wind tunnels (National Aeronautics and Space Administration :, 1962), by Albert L. Braslow, Cullen Q. Lee, Harleth G. Wiley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- 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)
- Rationale and description of a coordinated cockpit display for aircraft flight management (National Aeronautics and Space Administration ;, 1976), by Daniel L. Baty and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Pilot opinions on high level flight deck automation issues : toward the development of a design philosophy (National Aeronautics and Space Administration, Langley Research Center ;, 1995), by Yvette J. Tenney, Richard W. Pew, William H. Rogers, Langley Research Center, and BBN Systems and Technologies Corporation (page images at HathiTrust)
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