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Guidance systems (Flight) -- Computer simulation

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• Guidance systems (Flight)
• Navigation (Aeronautics) -- Computer simulation
• Computer simulation

• Flight control -- Computer simulation

• Four-dimensional guidance algorithms for aircraft in an air traffic control environment (National Aeronautics and Space Administration ;, 1975), by Thomas Pecsvaradi and Ames Research Center (page images at HathiTrust)
• Real-time manned simulation of advanced terminal area guidance concepts for short-haul operations (National Aeronautics and Space Administration ;, 1977), by Leonard Tobias, Paul J. O'Brien, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Linearized aerodynamic and control law models of the X-29A airplane and comparison with flight data (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by John T. Bosworth and Dryden Flight Research Facility (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)

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

• Inertial guidance engineering (Prentice-Hall, 1962), by Manuel Ferná́ndez and George R. Macomber (page images at HathiTrust)
• 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)
• Automatic flight control theory. (Joint Publications Research Service, 1965), by Vasiliĭ Afanasʹevich Bodner and United States. Joint Publications Research Service (page images at HathiTrust)
• Basics of missile guidance and space techniques (J. F. Rider, 1959), by Marvin Hobbs (page images at HathiTrust; US access only)
• Demonstration of the Aventech aircraft mounted meteorological measurement system (U.S. Dept. of Agriculture, Forest Service, Technology & Development Program, 2001), by Dick Karsky, John A. Anhold, Harold Thistle, and Technology & Development Program (U.S.) (page images at HathiTrust)
• Satellite navigation : hearing before the Subcommittee on Aviation of the Committee on Commerce, Science, and Transportation, United States Senate, Ninety-eighth Congress, second session, on S. Con. Res. 69 ... May 23, 1984. (U.S. G.P.O., 1984), by Science United States. Congress. Senate. Committee on Commerce (page images at HathiTrust)
• A digest of adaptive systems; internal research. (Cornell Aeronautical Laboratory, Inc., 1962), by Vincent C. Rideout and V. Rajaraman (page images at HathiTrust)
• A study of an adaptive control system using digital simulation. (Buffalo, 1960), by Cornell Aeronautical Laboratory and T. R. Benedict (page images at HathiTrust)
• Aerospace vehicles as objects of control (National Aeronautics and Space Administration ;, 1974), by Aleksandr Stepanovish Shatalov (page images at HathiTrust)
• Effects of combining vertical and horizontal information into a primary flight display (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), by Terence S. Abbott, Mark Nataupsky, George G. Steinmetz, and Langley Research Center (page images at HathiTrust)
• Reference energy-altitude descent guidance : simulator evaluation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Kathy H. Abbott, Charles E. Knox, and Langley Research Center (page images at HathiTrust)
• Simulation studies of time-control procedures for the Advanced Air Traffic Control system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Leonard Tobias and Ames Research Center (page images at HathiTrust)
• Flight tests of three-dimensional path-redefinition algorithms for transition from radio navigation to microwave landing system navigation when flying an aircraft on autopilot (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), by Richard M. Hueschen (page images at HathiTrust)
• Advanced control technology and its potential for future transport aircraft (U.S. National Aeronautics and Space Administration ;, 1976), by Hugh L. Dryden Flight Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparison of two head-up displays in simulated standard and noise abatement night visual approaches (National Aeronautics and Space Administration ;, 1975), by Fred Cronn, Everett Palmer, and Ames Research Center (page images at HathiTrust)
• Flight evaluation of two-segment approaches using area navigation guidance equipment (U.S. National Aeronautics and Space Administration ;, 1976), by G. K. Schwind, inc United Air Lines, and Ames Research Center (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)
• Radio/optical/strapdown inertial guidance study for advanced kick-stage applications. Volume I, Summary. (National Aeronautics and Space Administration ;, 1969), by TRW Inc and Electronics Research Center (U.S.) (page images at HathiTrust)
• Development of advanced avionics systems applicable to terminal-configured vehicles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by R. L. Heimbold, M. F. Leffler, H. P. Lee, Langley Research Center, and Lockheed-California Company (page images at HathiTrust)
• Automatic guidance and control of a transport aircraft during a helical landing approach (National Aeronautics and Space Administration ;, 1975), by Daniel J. Crawford, Roland L. Bowles, and Langley Research Center (page images at HathiTrust)
• Effect of external disturbances and data rate on the response of an automatic landing system capable of curved trajectories (National Aeronautics and Space Administration ;, 1975), by Windsor L. Sherman and Langley Research Center (page images at HathiTrust)
• Apollo experience report : guidance and control systems (U.S. National Aeronautics and Space Administration ;, 1976), by Raymond E. Wilson, United States National Aeronautics and Space Administration, and Lyndon B. Johnson Space Center (page images at HathiTrust)
• NASA TN D-4597 (National Aeronautics and Space Administration ;, 1968), by Lannie D. Webb, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of error progression in terminal guidance for lunar landing (National Aeronautics and Space Administration :, 1961), by P. J. De Fries (page images at HathiTrust)
• NASA TN D-6232 (National Aeronautics and Space Administration ;, 1971), by Gilbert G. Robinson, Michael J. Bondi, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Investigation toward simplification of missile control systems (National Advisory Committee for Aeronautics, 1953), by Howard J. Curfman, Harold L. Crane, H. Kurt Strass, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Fine guidance sensor (FGS) (National Aeronautics and Space Administration, 1996), by United States National Aeronautics and Space Administration (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)
• Flight path recovery system (FPRS) design study (New York, New York : Systech Incorporated, 1978., 1978), by Bendix Field Engineering Corporation and United States. Department of Energy. Grand Junction Office (page images at HathiTrust)
• Windspeed profile, windshear, and gusts for design of guidance systems for vertical rising air vehicles (Cambridge, Massachusetts : Special Projects Laboratory, Geophysics Research Directorate, Air Force Cambridge Research Center, Air Research and Development Command, [1954], 1954), by Norman Sissenwine and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate (page images at HathiTrust)
• Tropospheric variations of refractive index at microwave frequencies (Bedford, Massachusetts : Programs and Requirements Branch, Geophysics Research Directorate, Air Force Cambridge Research Center, Air Research and Development Command, 1955., 1955), by Charles F. Campen, Allen E. Coe, and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate (page images at HathiTrust)
• Performance criteria for linear constant-coefficient systems with random inputs (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Raymond Magdaleno, Julian Wolkovitch, United States. Air Force. Systems Command. Aeronautical Systems Division, and Inc Systems Technology (page images at HathiTrust)
• Six-Degree-of-Freedom flight path study generalized computer program (SDFCP) User's manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1975., 1975), by Fay O. Young and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)

• Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems (National Advisory Committee for Aeronautics, 1955), by Howard J. Curfman, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)

• Present and future state of the art in guidance computer memories (National Aeronautics and Space Administration ;, 1967), by Robert C. Ricci and Electronics Research Center (U.S.) (page images at HathiTrust)
• En route position and time control of aircraft using Kalman filtering of radio aid data (National Aeronautics and Space Administration ;, 1973), by Leonard A. McGee, Jay V. Christensen, and Ames Research Center (page images at HathiTrust)

• 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)

• Fine Guidance Sensor instrument handbook (Space Telescope Science Institute, 1985), by A. Fresneau and Space Telescope Science Institute (U.S) (page images at HathiTrust)

• Supersonic aerodynamic characteristics of the Active Laser Seeker (ALS) configuration of a proposed maneuvering air-to-air missile design (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1977., 1977), by D. H. Fikes, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)

• Navigation and guidance in space (Prentice-Hall, 1963), by Edward V. B. Stearns (page images at HathiTrust)

• Flight service station system modernization hearing before the Subcommittee on Aviation of the Committee on Public Works and Transportation, House of Representatives, Ninety-fifth Congress, first session, on H.R. 7699 ... October 3, 1977. (U.S. Govt. Print. Off., 1977), by United States. Congress. House. Committee on Public Works and Transportation. Subcommittee on Aviation (page images at HathiTrust)
• Roll-yaw control at high angle of attack by forebody tangential blowing (Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center :, 1995), by Nelson Pedreiro and Joint Institute for Aeronautics and Acoustics (page images at HathiTrust)
• An analysis of flexible aircraft structural mode control. Part 1, Unclassified data (Wright-Patterson Air Force Base, Ohio : AF Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1966., 1966), by John H. Wykes, Alva S. Mori, Wright-Patterson Air Force Base (Ohio), Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation (page images at HathiTrust)
• A Piloted evaluation of an oblique-wing research aircraft motion simulation with decoupling control laws (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Robert W. Kempel and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (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)
• 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)
• NASA Information Sciences and Human Factors Program annual report, 1990 (NASA, Scientific and Technical Information Division, 1991), by United States. National Aeronautics and Space Administration. Information Sciences and Human Factors Division (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)
• Space shuttle separate-surface control-system study (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Lawrence W. Brown, Raymond C. Montgomery, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• NASA Information Sciences and Human Factors Program annual report, 1987 (NASA, Scientific and Technical Information Division, 1988), by United States. National Aeronautics and Space Administration. Information Sciences and Human Factors Division (page images at HathiTrust)
• Flight investigation of a solar orientation control system for spacecraft (National Aeronautics and Space Administration , 1964), by Anthony Fontana and Langley Research Center (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)
• 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)
• Study of the use of a nonlinear, rate-limited filter on pilotcontrol signals (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by James J. Adams and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• NASA Information Sciences and Human Factors Program annual report, 1988 (NASA, Scientific and Technical Information Division, 1989), by United States. National Aeronautics and Space Administration. Information Sciences and Human Factors Division (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)
• 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)
• NASA Information Sciences and Human Factors Program annual report, 1989 (NASA, Scientific and Technical Information Division, 1990), by United States. National Aeronautics and Space Administration. Information Sciences and Human Factors Division (page images at HathiTrust)
• Study of the application of an implicit model-following flight controller to lift-fan VTOL aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Vernon K. Merrick, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (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)
• 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)
• 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)
• Development and evaluation of a Kalman-filter algorithm for terminal area navigation using sensors of moderate accuracy (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Gerd Kanning, Stanley F. Schmidt, Luigi S. Cicolani, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Attitude sensor study. (National Aeronautics and Space Administration :, 1964), by United States National Aeronautics and Space Administration and Hughes Aircraft Company. Research Laboratories (page images at HathiTrust)
• Rapid optimization of multiple-burn rocket flights (National Aeronautics and Space Administration ;, 1969), by K. R. Brown, G. W. Johnson, E. F. Harrold, George C. Marshall Space Flight Center, and International Business Machines Corporation. Federal Systems Division (page images at HathiTrust)
• Computer mechanization of reentry equations with four degrees of freedom (National Aeronautics and Space Administration ;, 1968), by R. M. Howe, University of Michigan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Manual attitude control systems (National Aeronautics and Space Administration :, 1964), by R. O. Besco, D. K. Bauerschmidt, G. G. Depolo, United States National Aeronautics and Space Administration, and Hughes Aircraft Company (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)
• Inverse optimal control problem in manual control systems. (National Aeronautics and Space Administration, 1965), by R. W. Obermayer, Frederick A. Muckler, Bunker-Ramo Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pilot describing function measurements in a multiloop task (National Aeronautics and Space Administration, 1966), by R. L. Stapleford, R. Magdaleno, and D. T. McRuer (page images at HathiTrust; US access only)
• Data requirements for in-flight synthesis and multiple blender studies (National Aeronautics and Space Administration, 1966), by L. D. Edinger and G. D. White (page images at HathiTrust; US access only)
• The development of a pseudo-Nyquist analysis technique for hybrid sampled-data control systems (National Aeronautics and Space Administration ;, 1973), by Milford G. Burnitt, George C. Marshall Space Flight Center, and Chrysler Corporation. Space Division (page images at HathiTrust)
• Digital adaptive flight controller development (National Aeronautics and Space Administration ;, 1974), by Howard Kaufman, Langley Research Center, and Rensselaer Polytechnic Institute. Systems Engineering Division (page images at HathiTrust)
• Applicability of the control configured design approach to advanced earth orbital transportation systems (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Andrew K. Hepler, and Boeing Aerospace Company (page images at HathiTrust)
• F-8C adaptive flight control laws (National Aeronautics and Space Administration ;, 1977), by Honeywell Systems and Research Center, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Radio/optical/strapdown inertial guidance study for advanced kick-stage applications. Volume I, Summary. (National Aeronautics and Space Administration ;, 1969), by TRW Inc and Electronics Research Center (U.S.) (page images at HathiTrust)
• Flight computer and language processor study (National Aeronautics and Space Administration ;, 1970), by Raymond J. Rubey, Laurel Bentley, William C. Nielsen, Electronics Research Center (U.S.), and inc Logicon (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)
• A Study of flight control requirements for advanced, winged, earth-to-orbit vehicles with far-aft center-of-gravity locations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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)
• Verification of the FtCayuga fault-tolerant microprocessor system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by Mandayam Srivas, Mark Bickford, Langley Research Center, and ORA Corporation (page images at HathiTrust)
• Formal specification and verification of a fault-masking and transient-recovery model for digital flight-control systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by John Rushby, Langley Research Center, and SRI International (page images at HathiTrust)
• Dynamics of spacecraft control laboratory experiment (SCOLE) slew maneuvers (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987), by Yogendra P. Kakad (page images at HathiTrust)
• 4D-TECS integration for NASA TSRV airplane (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by I. Kaminer, P. R. O'Shaughnessy, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Aircraft flight test trajectory control (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by P. K. A. Menon, R. A. Walker, and Dryden Flight Research Facility (page images at HathiTrust)
• Several methods for aerodynamic reduction of static-pressure sensing errors for aircraft at subsonic, near-sonic, and low supersonic speeds (U.S. G.P.O.], 1959), by Virgil S. Ritchie (page images at HathiTrust)
• Dynamic response of airplanes to atmospheric turbulence including flight data on input and response (National Aeronautics and Space Administration, 1964), by John C. Houbolt, Kermit G. Pratt, Roy Steiner, and Langley Research Center (page images at HathiTrust)
• Automatic guidance and control of a transport aircraft during a helical landing approach (National Aeronautics and Space Administration ;, 1975), by Daniel J. Crawford, Roland L. Bowles, and Langley Research Center (page images at HathiTrust)
• Practical aspects of using a maximum likelihood estimation method to extract stability and control derivitives from flight data (National Aeronautics and Space Administration ;, 1976), by Kenneth W. Iliff, Richard E. Maine, United States National Aeronautics and Space Administration, and Hugh L. Dryden Flight Research Center (page images at HathiTrust)
• NASA TN D-4963 (National Aeronautics and Space Administration ;, 1969), by Robert S. Ryan, Alberta W. King, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6708 (National Aeronautics and Space Administration :, 1972), by Richard R. Larson, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight-determined derivatives and dynamic characteristics of the CV-990 airplane (National Aeronautics and Space Administration ;, 1972), by Glenn B. Gilyard and Flight Research Center (U.S.) (page images at HathiTrust)
• Ground effect for lifting rotors in forward flight (National Aeronautics and Space Administration, 1960), by Harry H. Heyson and Langley Research Center (page images at HathiTrust)
• An examination of handling qualities criteria for V/STOL aircraft (National Aeronautics and Space Administration :, 1960), by Seth B. Anderson and Ames Research Center (page images at HathiTrust)
• NASA TN D-1828 (National Aeronautics and Space Administration, 1963), by R. B. Noll, Robert L. Halasey, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• The effects of various combinations of damping and control power on helicopter handling qualities during both instrument and visual flight (National Aeronautics and Space Administration, 1959), by Seymour Salmirs, Robert J. Tapscott, and Langley Research Center (page images at HathiTrust)
• Flight investigation of a centrally located rigid force control stick used with electronic control systems in a fighter airplane (National Aeronautics and Space Administration, 1959), by Walter R. Russell, William L. Alford, and Langley Research Center (page images at HathiTrust)
• NASA TN D-4122 (National Aeronautics and Space Administration ;, 1967), by Jim A. Penland, Peter T. Bernot, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experience with the X-15 adaptive flight control system (National Aeronautics and Space Administration ;, 1971), by United States National Aeronautics and Space Administration and Flight Research Center (U.S.) (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)
• C-130BL category I performance test and qualitative stability and control evaluation (U.S. Air Force, Air Research and Development Command, Air Force Flight Test Center, 1961), by Kenneth C. Carter, Emil Sturmthal, and Air Force Flight Test Center (U.S.) (page images at HathiTrust)
• Advanced integrated aircraft displays and augmented flight control : scientific final report : prepared for Engineering Psychology Programs, Office of Naval Research (Aviation Research Laboratory, University of Illinois at Urbana-Champaign, 1976), by Stanley Nelson Roscoe and United States. Office of Naval Research (page images at HathiTrust; US access only)
• Dispersion control system for sounding rockets (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1976., 1976), by James R. Pickell and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• The problem: instantaneously effecting controlled balloon-system descent from high altitude (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), by James F. Dwyer and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• Modified gas valve for improved balloon descent control (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), by George F. Nolan, Bernard D. Gildenberg, Larry D. Wrinkle, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• A study of Russian feed-back control theory (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, U.S. Air Force, 1961., 1961), by Fredric R. Alex, C. R. Heerman, United States. Air Force. Air Research and Development Command, Wright Air Development Center, General Dynamics Corporation. Convair Division, and United States. Wright Air Development Division (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)
• Effects of manipulator restraints on human operator performance (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. E. Magdaleno, Duane T. McRuer, Wright-Patterson Air Force Base (Ohio), Pa.). Laboratories for Research and Development Franklin Institute (Philadelphia, Inc Systems Technology, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Control configured vehicle ride control system (CCV RCS) : B-52 control system analysis, synthesis, and design (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by C. R. Stockdale, R. D. Poyneer, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Fixed-base in-flight simulations of longitudinal and lateral-directional handling qualities for piloted re-entry vehicles (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), by Edwin A. Kidd, Robert P. Harper, Wright-Patterson Air Force Base (Ohio), Cornell Aeronautical Laboratory, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Performance criteria for linear constant-coefficient systems with random inputs (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Raymond Magdaleno, Julian Wolkovitch, United States. Air Force. Systems Command. Aeronautical Systems Division, and Inc Systems Technology (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)
• Theoretical and experimental investigation of some new longitudinal handling qualities parameters (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Henry R. Jex, United States. Air Force. Systems Command. Aeronautical Systems Division, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
• Aerodynamic stability and control/wind tunnel data correlation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by G. R. Casteel, Air Force Flight Dynamics Laboratory (U.S.), and North American Rockwell Corporation (page images at HathiTrust)
• Human pilot dynamics with various manipulators (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 Duane T. McRuer, R. E. Magdaleno, Wright-Patterson Air Force Base (Ohio), Inc Systems Technology, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Development of weapon delivery models and analysis programs. Volume I, System modeling and performance optimization (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by A. Ferit Konar, Honeywell Inc. Systems and Research Division, Air Force Flight Dynamics Laboratory (U.S.), and Armament Delivery Analysis Programming System (ADAPS) (page images at HathiTrust)
• Design criteria for the future of flight controls : proceedings of the Flight Dynamics Laboratory Flying Qualities and Flight Control Symposium, 2-5 March, 1982. (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 Flight Dynamics Laboratory Flying Qualities and Flight Control Symposium (1982 : Dayton), D. W. Potts, S. G. Fuller, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (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)
• Development of weapon delivery models and analysis programs. Volume II, Documentation of the Armament Delivery Analysis Programming System (ADAPS) (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by A. Ferit Konar, Michael D. Ward, Honeywell Inc. Systems and Research Division, Air Force Flight Dynamics Laboratory (U.S.), and Armament Delivery Analysis Programming System (ADAPS) (page images at HathiTrust)
• Development of weapon delivery models and analysis programs. Volume III, Testing and demonstration of the Armament Delivery Analysis Programming System (ADAPS) (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by A. Ferit Konar, Michael D. Ward, Honeywell Inc. Systems and Research Division, Air Force Flight Dynamics Laboratory (U.S.), and Armament Delivery Analysis Programming System (ADAPS) (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)
• Linearized dynamics of rotating aerospace vehicles with internal angular momenta (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by Duane T. McRuer, Julian Wolkovitch, United States. Air Force. Systems Command. Aeronautical Systems Division, United States. Air Force. Systems Command, and Inc Systems Technology (page images at HathiTrust)
• A comparison between tracking with "optimum" dynamics and tracking with a simple velocity control (Behavioral Sciences Laboratory, 6570th Aerospace Medical Research Laboratories, Aerospace Medical Division, Air Force Systems Command, 1962), by George G. Frost and Aerospace Medical Research Laboratories (U.S.). Behavioral Sciences Laboratory (page images at HathiTrust)
• Analysis of digital flight control systems with flying qualities applications. Volume II, Technical report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), by Richard F. Whitbeck, L. G. Hofmann, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
• Six-Degree-of-Freedom flight path study generalized computer program (SDFCP) User's manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1975., 1975), by Fay O. Young 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)
• Roll handling qualities (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by I. L. Ashkenas, Wright-Patterson Air Force Base (Ohio), Inc Systems Technology, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Single-axis attitude regulation of extra-atmospheric vehicles (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by R. A. Peters, Dunstan Graham, V.J. Kovacevich, United States. Air Force. Systems Command. Aeronautical Systems Division, and Inc Systems Technology (page images at HathiTrust)
• Operating points, particle dynamics, and coordinate systems for aerospace vehicle stability and control (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Duane T. McRuer, Irving Ashkenas, United States. Air Force. Systems Command. Aeronautical Systems Division, Wright-Patterson Air Force Base (Ohio), and Inc Systems Technology (page images at HathiTrust)
• A study to determine the feasibility of a self-optimizing automatic flight control system (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Aeronutronic Ford Corporation, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Investigation of numerical techniques as applied to digital flight control systems (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 J. W. Hung, J. A. Spicer, P. P. Shipley, K. W. Nielsen, C. L. Lutes, Wright-Patterson Air Force Base (Ohio), North American Aviation. Autonetics Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Modeling flexible aircraft for flight control design (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1989., 1989), by E. C. Bekir, G. A. Watts, R. N. Moon, E. J. Horowitz, H. Hassig, A. Goforth, William Davis, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (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)
• Flight control study of a manned re-entry vehicle (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Control Laboratory, Air Research and Development Command, United States Air Force, 1960., 1960), by General Electric Company, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• DIGITAC III : Advanced Fault Tolerant Control Techniques (Wright-Patterson Air Force Base, Ohio : Fliight Dynamics Directorate, Wright Laboratory, Air Force Materiel Command, 1992., 1992), by Greg Hanson, Tom Lahn, Tom McManus, Eric Larson, Russel Hendrick, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and Honeywell Inc (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)
• In-flight investigation of the effects of higher-order control system dynamics on longitudinal handling qualities (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1968., 1968), by Dante A. Di Franco, Cornell Aeronautical Laboratory, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (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)
• An experimental study on multi-wall structures for space vehicles (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Dynamics Laboratory, Air Research and Development Command, U.S. Air Force, 1961., 1961), by D. G. Younger, S. Lampert, Aeronutronic Ford Corporation, Air Force Flight Dynamics Laboratory (U.S.), United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• High altitude supersonic target (HAST) : phase III (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Development and Test Center, Air Force Systems Command, United States Air Force, 1977., 1977), by D. E. Wells, W. M. Byrne, United States. Air Force. Systems Command, Air Force Armament Laboratory, and Beech Aircraft Corporation (page images at HathiTrust)
• Proceedings of the workshop on multivariable control systems (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1983., 1983), by Michael A. Masi, Daniel E. Russ, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Analytical investigations in aircraft and spacecraft trajectory optimization and optimal guidance (National Aeronautics and Space Administration, Langley Research Center ;, 1995), by Nikos Markopoulos, Anthony J. Calise, Langley Research Center, and Georgia Institute of Technology. School of Aerospace Engineering (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)
• Optimal incomplete feedback control of linear stochastic systems (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by Robert E. Heath, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Flight control principles for control configured vehicles (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by Edmund G. Rynaski, Norman C. Weingarten, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Engineering analysis methods for linear time varying systems (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, [1963], 1963), by Dunstan Graham, Harry Passmore, Walter Johnson, Eugene J. Brunelle, United States. Air Force. Systems Command. Aeronautical Systems Division, Wright-Patterson Air Force Base (Ohio), and Inc Systems Technology (page images at HathiTrust)
• Advanced electromechanical actuation system (EMAS) development and flight test (C-141 aircraft) demonstration (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1988., 1988), by T. Mark Bailey, K. C. Thompson, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), Sundstrand Corporation, and Lockheed Aeronautical Systems Company. Georgia Division (page images at HathiTrust)
• Design method for fully augmented systems for variable flight conditions (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, AIr Force Systems Command, United States Air Force, 1972., 1972), by Albert J. VanDierendonck, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Honeywell Inc. Systems and Research Division (page images at HathiTrust)
• Stochastic disturbance data for flight control system analysis (Directorate of Aeromechanics, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962), by John E. Hart, Larry L. Lacau, Lowry A. Adkins, United States. Air Force. Systems Command. Aeronautical Systems Division, Wright-Patterson Air Force Base (Ohio), and Lockheed-Georgia Company (page images at HathiTrust)

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