Space vehicles -- Control systems -- Computer programsSee also what's at your library, or elsewhere.
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Filed under: Space vehicles -- Control systems -- Computer programs- The USAF Stability and Control Digital Datcom. Volume III, Pilot module (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), by John E. Williams, Steven R. Vukelich, Air Force Flight Dynamics Laboratory (U.S.), McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)
- The USAF Stability and Control Digital Datcom. Volume I, Users manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), by John E. Williams, Steven R. Vukelich, Air Force Flight Dynamics Laboratory (U.S.), McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)
- The USAF Stability and Control Digital Datcom. Volume II, Implementtion of Datacom methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), by John E. Williams, Steven R. Vukelich, Air Force Flight Dynamics Laboratory (U.S.), McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)
- The USAF Stability and Control Digital Datcom. Volume I, Users manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), by John E. Williams, Steven R. Vukelich, Air Force Flight Dynamics Laboratory (U.S.), McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)
Filed under: Space vehicles -- Control systems -- Computer programs -- ManagementFiled under: Space vehicles -- Control systems -- Design and construction -- Computer programs
Items below (if any) are from related and broader terms.
Filed under: Space vehicles -- Control systems- Navigation algorithms for the SeaWiFS mission (National Aeronautics and Space Administration, Goddard Space Flight Center, 2002), by Frederick S Patt and Goddard Space Flight Center (page images at HathiTrust)
- Structural interaction with control systems. (National Aeronautics and Space Administration;, 1971), by R. B. Noll and J. Zvara (page images at HathiTrust)
- Assessment and control of spacecraft electromagnetic interference. (National Aeronautics and Space Administration [for sale by the National Technical Information Service, Springfield, Va.], 1972), by Robert G. Lyle and Robert Stroud (page images at HathiTrust)
- Effects of structural flexibility on entry vehicle control systems. [Prepared for NASA under the cognizance of the Jet Propulsion Laboratory, California Institute of Technology. (National Aeronautics and Space Administraiton;, 1972), by John J. Deyst, R. B. Noll, Jet Propulsion Laboratory (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Spacecraft thermal control. (National Aeronautics and Space Administration, 1973), by Robert G Lyle, Robert Stroud, and Perikles Stabekis (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)
- Components and Hardware Systems Branch (National Aeronautics and Space Administration, Goddard Space Flight Center, 2000), by Goddard Space Flight Center (page images at HathiTrust)
- Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Howard W. Stone, Richard W. Powell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Automating a spacecraft electrical power system using expert systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Louis F. Lollar and George C. Marshall Space Flight Center (page images at HathiTrust)
- Analysis of the space shuttle orbiter entry dynamics from Mach 10 to Mach 2.5 with the November 1976 flight control system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Richard W. Powell, Howard W. Stone, and Langley Research Center (page images at HathiTrust)
- Effect of aerodynamic and angle-of-attack uncertainties on the May 1979 entry flight control system of the space shuttle from Mach 8 to 1.5 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Howard W. Stone, Richard W. Powell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
- Analysis of random signal combinations for spacecraft pointing stability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Leonard W. Howell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Evaluation of a laboratory test model annular momentum control device (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Nelson J. Groom and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Analytical prediction with multidimensional computer programs and experimental verification of the performance, at a variety of operating conditions, of two traveling wave tubes with depressed collectors (National Aeronatuics and Space Administration, Scientific and Technical Information Office ;, 1979), by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, James A. Dayton, and Lewis Research Center (page images at HathiTrust)
- Analysis and simulation of a magnetic bearing suspension system for a laboratory model annular momentum control device (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Nelson J. Groom, Suresh M. Joshi, Charles T. Woolley, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Space shuttle active-pogo suppressor control design using linear quadratic regulator techniques (National Aeronatuics and Space Administration, Scientific and Technical Information Office ;, 1979), by Bruce Lehtinen, Carl F. Lorenzo, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Pitfalls and guidelines for the numerical evaluation of moderate-order system frequency response (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Harold P. Frisch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Goddard Space Flight Center (page images at HathiTrust)
- Time and frequency domain analysis of sampled data controllers via mixed operation equations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Harold P. Frisch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Goddard Space Flight Center (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)
- Temperature control by thermostatic fins-analysis (NASA, 1964), by J. A. Wiebelt, J. F. Parmer, Oklahoma State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Techniques for generation of control and guidance signals derived from optical fields : Part II (National Aeronautics and Space Administration :, 1971), by H. Hemami, S. R. Gardner, R. B. McGhee, Langley Research Center, Ohio State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Temperature control by thermostatic fins-analysis (NASA, 1965), by John A. Wiebelt, G. J. Kneissl, J. F. Parmer, Oklahoma State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Control moment gyro optimization study (National Aeronautics and Space Administration, 1966), by G. W. Yarber (page images at HathiTrust; US access only)
- Transfer function approximations for large highly coupled elastic boosters with fuel slosh (National Aeronautics and Space Administration, 1966), by R. L. Stapleford (page images at HathiTrust; US access only)
- Spaceborne multiprocessing (National Aeronautics and Space Administration, 1968), by North American Rockwell Corporation. Autonetics Division and L. J. Koczela (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)
- Design of the Annular Suspension and Pointing System (ASPS) : (including design addendum) (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by D. Cunningham, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Geometric theory of optimum disorbit problems (National Aeronautics and Space Administration, 1967), by A. Busemann and N. X. Vinh (page images at HathiTrust; US access only)
- 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)
- NASA TN D-2049 (National Aeronautics and Space Administration, 1963), by Jack A. White, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Apollo experience report : guidance and control systems : lunar module mission programer (National Aeronautics and Space Administration, 1975), by Jesse A. Vernon and Lyndon B. Johnson Space Center (page images at HathiTrust)
- Apollo experience report : guidance and control systems : command and service module entry monitor subsystem (National Aeronautics and Space Administration ;, 1975), by Ben Reina, Herbert G. Patterson, and Lyndon B. Johnson Space Center (page images at HathiTrust)
- Apollo experience report : guidance and control systems : command and service module stabilization and control system (National Aeronautics and Space Administration, 1974), by Orval P. Littleton and Lyndon B. Johnson Space Center (page images at HathiTrust)
- Apollo experience report : guidance and control systems : automated control system for unmanned mission AS-201 (National Aeronautics and Space Administration ;, 1975), by Gene F. Holloway and Lyndon B. Johnson Space Center (page images at HathiTrust)
- Apollo experience report : guidance and control systems : lunar module abort guidance system (National Aeronautics and Space Administration ;, 1975), by Pat M. Kurten and Lyndon B. Johnson Space Center (page images at HathiTrust)
- Apollo experience report : guidance and control systems : orbital-rate drive electronics for the Apollo command module and lunar module (National Aeronautics and Space Administration, 1974), by Roy B. Parker, Paul E. Sollock, and Lyndon B. Johnson Space Center (page images at HathiTrust)
- Effects of modifications to the space shuttle entry guidance and control systems (National Aeronautics and Space Administration ;, 1976), by Richard W. Powell, Lawrence F. Rowell, Howard W. Stone, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Analysis of a linear system for variable-thrust control in the terminal phase of rendezvous (National Aeronautics and Space Administration, 1961), by Richard A. Hord, Barbara J. Durling, United States National Aeronautics and Space Administration, and Langley Research Center (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 demonstration of a nose-mounted rotating-solid-propellant rocket control system and a comparison with analog studies (National Aeronautics and Space Administration ;, 1966), by Kirby H. Williams, Robert L. James, and Langley Research Center (page images at HathiTrust)
- Apollo experience report : systems and flight procedures development (National Aeronautics and Space Administration ;, 1973), by Paul C. Kramer and Lyndon B. Johnson Space Center (page images at HathiTrust)
- Apollo experience report : flight-control data needs, terminal display devices, and ground system configuration requirements (National Aeronautics and Space Administration, 1974), by Richard A. Hoover and Lyndon B. Johnson Space Center (page images at HathiTrust)
- Effectiveness of several control arrangements on a Mercury-type capsule (National Aeronautics and Space Administration, 1961), by Robert I. Sammonds, Robert R. Dickey, 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)
- NASA TN D-4481 (National Aeronautics and Space Administration ;, 1968), by Richard L. Kurkowski, Gordon H. Hardy, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Integrating spacecraft systems (National Aeronautics and Space Administration ;, 1966), by Allen L. Franta and Goddard Space Flight Center (page images at HathiTrust)
- Guidance and control during direct-descent parabolic reentry (National Aeronautics and Space Administration, 1961), by Edwin C. Foudriat, Rodney C. Wingrove, United States National Aeronautics and Space Administration, Ames Research Center, Langley Research Center, and D.C.) NASA-Industry Apollo Technical Conference (1961 : Washington (page images at HathiTrust)
- NASA TN D-1965 (National Aeronautics and Space Administration, 1963), by Robert H. Kirby, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Apollo experience report : spacecraft pyrotechnic systems (National Aeronautics and Space Administration ;, 1973), by Mario J. Falbo, Robert L. Robinson, and Manned Spacecraft Center (U.S.) (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)
- The BATCAVE ([U.S. Dept. of the Navy], 1995), by United States Navy Department (page images at HathiTrust)
- Methodologies for the direct digital control of highly flexible vehicles (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), by Duane T. McRuer, Raymond E. Magdaleno, Richard F. Whitbeck, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Inc Systems Technology (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)
- Analytical study of a drag brake control systen for hypersonic vehicles (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by J. E. Hayes, Wallace E. Vander Velde, P. H. Rose, Avco-Everett Research Laboratory, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
- Integrated passive and active control of structures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate , Wright Laboratory, Air Force Materiel Command, United States Air Force, 1993., 1993), by Vernon H. Neubert, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and Pennsylvania State University. Department of Engineering Sciences and Mechanics (page images at HathiTrust)
- Robustness improvement of actively controlled structures through integrated structural/control design (Wright-Patterson Air Force Base, Ohio : Fliight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, 1991, 1991), by S. S. Rao, T. S. Pan, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and Purdue University. School of Mechanical Engineering (page images at HathiTrust)
- Streamlined design and self reliant hardware for active control of precision space structures (National Aeronautics and Space Administration, Langley Research Center ;, 1994), by David C. Hyland, Douglas J. Phillips, James A. King, and Langley Research Center (page images at HathiTrust)
- Analysis and design of space vehicle flight control systems (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1967), by General Dynamics Corporation. Convair Division, Arthur L. Greensite, and George C. Marshall Space Flight Center (page images at HathiTrust)
- Analytical methods for space vehicle atmospheric control processes: Part II (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by C. S. Coe, A. Shaffer, J. Rousseau, United States. Air Force. Systems Command. Aeronautical Systems Division, North American Aviation. Space and Information Systems Division, Garrett Corporation, and AiResearch Manufacturing Company of Los Angeles (Calif.) (page images at HathiTrust)
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