Launch vehicles (Astronautics) -- Automatic control -- Mathematical models

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• Launch vehicles (Astronautics) -- Automatic control
• Launch vehicles (Astronautics) -- Mathematical models
• Automatic control -- Mathematical models

• Control of a large launch vehicle with limited thrust vectoring in the presence of winds / by Dennis F. Collins, Jr., and Homer G. Morgan. (Washington : National Aeronautics and Space Administration, [1963]), by Dennis F. Collins (page images at HathiTrust)

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

• NASA Scout ST-1 flight-test results and analyses, launch operations and test vehicle description / compiled by Robert J. Mayhue. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]) (page images at HathiTrust)

• The development of a pseudo-Nyquist analysis technique for hybrid sampled-data control systems / by Milford G. Burnitt and Charles W. Davis. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by National Technical Information Service], 1973), by Milford G. Burnitt (page images at HathiTrust)

• Launch vehicle error sensitivity study / by Richard C. Rosenbaum and Robert E. Willwerth. ([Washington, D.C.] : National Aeronautics and Space Administration, [1970]), by Richard C. Rosenbaum (page images at HathiTrust)
• A describing-function analysis of the stability of a launch vehicle with nonlinear thrust vectoring / by Harold C. Lester. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by Harold C. Lester (page images at HathiTrust)
• Longitudinal mass-spring modeling of launch vehicles / by Rudolf F. Glaser. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by Rudolf F. Glaser (page images at HathiTrust)

• Rendezvous capability of horizontal-take-off launch vehicle with air-breathing propulsion / by Charlie M. Jackson. (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Charlie M. Jackson (page images at HathiTrust)

• Numerical integration in a rigid-body trajectory program / by John Edd Moore. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by John Edd Moore (page images at HathiTrust)

• Trajectory simulation applicable to stability and control studies of large multi-engine vehicles / by Ronald J. Harris. (Washington : National Aeronautics and Space Administration, [1963]), by Ronald J. Harris (page images at HathiTrust)

• Optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraints / by Fred Teren and Omer F. Spurlock. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Fred Teren (page images at HathiTrust)
• Rendezvous capability of horizontal-take-off launch vehicle with air-breathing propulsion / by Charlie M. Jackson. (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Charlie M. Jackson (page images at HathiTrust)
• Trajectory simulation applicable to stability and control studies of large multi-engine vehicles / by Ronald J. Harris. (Washington : National Aeronautics and Space Administration, [1963]), by Ronald J. Harris (page images at HathiTrust)
• Performance charts for multistage rocket boosters / by John S. MacKay and Richard J. Weber. (Washington : National Aeronautics and Space Administration, [1961]), by John S. MacKay (page images at HathiTrust)

• Modeling digital control systems with MA-prefiltered measurements / Michael E. Polites. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by National Technical Information Service, 1987), by Michael E. Polites (page images at HathiTrust)
• Further developments in exact state reconstruction in deterministic digital control systems / Michael E. Polites. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Michael E. Polites (page images at HathiTrust)

• Servomechanisms with force feedback / by Robert C. Arzbaecher. (Argonne, Ill. : Argonne National Laboratory, 1960), by Robert C. Arzbaecher (page images at HathiTrust)
• Principles of control systems engineering [by] Vincent Del Toro [and] Sydney R. Parker. (New York, McGraw-Hill, 1960), by Vincent Del Toro (page images at HathiTrust)
• Analytical design of linear feedback controls (New York, Wiley, [1957]), by George C. Newton (page images at HathiTrust)
• Executive-controlled adaptive systems, by Robert Staffin and John G. Truxal. (Brooklyn, 1958), by Robert Staffin (page images at HathiTrust)
• A method for analyzing nonlinear closed-loop control systems with stationary stochastic inputs / by Wilfred J. Minkus. (Washington, D.C. : National Aeronautics and Space Administration, [1963]), by Wilfred J. Minkus (page images at HathiTrust)
• Decoupling in the design and the synthesis of multivariable control systems / by Peter L. Falb and William A. Wolovich. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Peter L. Falb (page images at HathiTrust)
• Studies of second- and third-order contactor control systems / by Irmgard Flügge-Lotz and Herbert E. Lindberg. (Washington : National Aeronautics and Space Administration, [1959]), by Irmgard Flügge-Lotz (page images at HathiTrust)
• Dynamic optimization and control; a variational approach. ([Cambridge] M.I.T. Press, Massachusetts Institute of Technology, [1961]), by Walerian Kipiniak (page images at HathiTrust)

• Investigation of third-order contactor control systems with two complex poles without zeros / by Irmgard Flügge-Lotz and Tomo Ishikawa. (Washington : National Aeronautics and Space Administration, [1960]), by Irmgard Flügge-Lotz (page images at HathiTrust)

• The absolute stability of nonlinear automatic control systems / B. Zh. Maygarin. (Washington, D.C. : National Aeronautics and Space Administration, [1965]), by B. Zh Maygarin (page images at HathiTrust)
• Analysis of dynamic performance limitations of fast response (150 to 200 Hz) electrohydraulic servos / by John R. Zeller. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by John R. Zeller (page images at HathiTrust)

• Active Control for the Total-In-Flight Simulator (ACTIFS) / E.G. Rynaski, D. Andrisani II, and N. Weingarten. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by E. G. Rynaski (page images at HathiTrust)

• Linearized aerodynamic and control law models of the X-29A airplane and comparison with flight data / John T. Bosworth. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by John T. Bosworth (page images at HathiTrust)

• The absolute stability of nonlinear automatic control systems / B. Zh. Maygarin. (Washington, D.C. : National Aeronautics and Space Administration, [1965]), by B. Zh Maygarin (page images at HathiTrust)

• The effect of digital computing on the performance of a closed-loop control-loading system / Russell V. Parrish and Billy R. Ashworth. (Washington : National Aeronautics and Space Administration : Springfield, Va. : For sale by the National Technical Information Service, 1976), by Russell V. Parrish (page images at HathiTrust)

• Analysis of dynamic performance limitations of fast response (150 to 200 Hz) electrohydraulic servos / by John R. Zeller. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by John R. Zeller (page images at HathiTrust)

• Analytic determination of camera operability status considering dynamic solar conflict for the Radio Astronomy Explorer satellite / by Harvey Walden. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970]), by Harvey Walden (page images at HathiTrust)

• Analytic determination of camera operability status considering dynamic solar conflict for the Radio Astronomy Explorer satellite / by Harvey Walden. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970]), by Harvey Walden (page images at HathiTrust)

• A study of the effect of measurement errors upon a range controller for an entry vehicle / by Jack A. White. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Jack A. White (page images at HathiTrust)

• Minimum thrust for correcting Keplerian orbits with application to interplanetary guidance / by Frederick W. Boltz. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Frederick W. Boltz (page images at HathiTrust)
• Control of a large launch vehicle with limited thrust vectoring in the presence of winds / by Dennis F. Collins, Jr., and Homer G. Morgan. (Washington : National Aeronautics and Space Administration, [1963]), by Dennis F. Collins (page images at HathiTrust)

• Control of a large launch vehicle with limited thrust vectoring in the presence of winds / by Dennis F. Collins, Jr., and Homer G. Morgan. (Washington : National Aeronautics and Space Administration, [1963]), by Dennis F. Collins (page images at HathiTrust)

• Magnetic attitude and spin control of the small scientific satellite S³-A by Thomas W. Flatley. (Washington, D.C. : National Aeronautics and Space Administration, [1970]), by Thomas W. Flatley (page images at HathiTrust)

• Magnetic attitude and spin control of the small scientific satellite S³-A by Thomas W. Flatley. (Washington, D.C. : National Aeronautics and Space Administration, [1970]), by Thomas W. Flatley (page images at HathiTrust)

• Minimum thrust for correcting Keplerian orbits with application to interplanetary guidance / by Frederick W. Boltz. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Frederick W. Boltz (page images at HathiTrust)

• Analytic determination of camera operability status considering dynamic solar conflict for the Radio Astronomy Explorer satellite / by Harvey Walden. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970]), by Harvey Walden (page images at HathiTrust)