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Guidance and homing systems

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• An analytical approach to the design of an automatic discontinuous control system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Lawrence W. Taylor, John W. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An explicit linear filtering solution for the optimization of guidance systems with statistical inputs / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Elwood C. Stewart and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theory and design curves for a yo-yo de-spin mechanism for satellites / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by J. V. Fedor and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Velocity requirements for abort from the boost trajectory of a manned lunar mission / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Robert E. Slye and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A study of the optimum velocity change to intercept and rendezvous / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by John M. Eggleston and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analytical method for studying the lateral motion of atmosphere entry vehicles. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Robert E. Slye and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A self-adaptive missile guidance system for statistical inputs / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by H. Rodney Peery and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Saturn vehicle attitude resolver computer error analysis / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Herman E. Thomason and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A two-impulse plan for performing rendezvous on a once-a-day basis / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by John D. Bird, David F. Thomas, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A study of guidance sensitivity for various low-thrust transfers from Earth to Mars/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Alan L. Friedlander and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Servo loop design for air bearing inertial components / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Herman E. Thomason and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Conceptual design study of a multipurpose aerospace test facility. George C. Marshall. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by George C. Marshall and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analytical study of orbital rendezvous for least fuel and least energy / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Harold Hornby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Optimal filtering and linear prediction applied to a midcourse navigation system for the circumlunar mission / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by John D. McLean, Leonard A. McGee, Stanley F. Schmidt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Simple solar orientation control system for space vehicles. Seymour Salmirs, S. Lawrence Kessler and Otis J. Parker. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Seymour Salmirs, Otis J. Parker, S. Lawrence Kessler, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Instrumentation of the ionosphere direct measurements satellite (explorer VIII). / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by R. E. Bourdeau, E. C. Whipple, J. L. Donley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of the effects of the time lag due to long transmission distance upon remote control: Phase II - Vehicle experiments, Phase III - Conclusions / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by James L. Adams and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Angular motion of the spin axis of the Tiros I meteorological satellite due to magnetic and gravitational torques / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by W. R. Bandeen, W. P. Manger, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An automatic terminal guidance system for rendezvous with a satellite / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Terrance M. Carney and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lunar trajectories / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Richard J. Weber, Richard R. Burley, Werner M. Pauson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Rotational Magnetodynamics and sterring of space vehicles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Raymond H. Wilson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theory of artificial stabilization of missiles and space vehicles with exposition of four control principles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Rudolf Franz Hoelker and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of the use of a terminal controller technique for reentry guidance of a capsule-type vehicle / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Edwin C. Foudriat and United States National Aeronautics and Space Administration (page images at HathiTrust)

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