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References
Blakelock, J.H.: Automatic Control of Aircraft and Missiles, John Wiley & Sons, Inc., New York, NY, second edition, 1991.
Etkin, B.: Dynamics of Atmospheric Flight, John Wiley & Sons, Inc., New York, 1972.
Garnell, P.: Guided Weapon Control Systems, Pergamon Press, Oxford, New York, second edition, 1980.
Li, Y.T. and Whitaker, H.P.: Performance Characterization for Adaptive Control Systems, paper presented at the Symposium on Self-Adjusting System Theory sponsored by the International Federation of Automatic Control and the Italian Commission on Automation, Rome, Italy, April 1962.
Lin, C.F.: Modern Navigation, Guidance, and Control Processing, Vol. II, Prentice Hall, Englewood Cliffs, New Jersey, 1991.
Nicolai, L.M.: Fundamentals of Aircraft Design, METS, Inc., San Jose, CA., 1984.
Osborn, P., Whitaker, H.P., and Kezer, A.: New Developments in the Design of Model Reference Adaptive Control Systems, Institute of Aeronautical Sciences, paper No. 61-39, presented at the IAS 29th annual meeting, January 1961.
Roskam, J.: Airplane Flight Dynamics and Automatic Flight Control, Part I, Roskam Aviation and Engineering Corporation, Ottawa, Kansas, second printing, 1982.
Siouris, G.M.: Aerospace Avionics Systems: A Modern Synthesis, Academic Press, Inc., San Diego, CA., 1993.
Skolnik, M.I.: Introduction to Radar Systems, McGraw-Hill, New York, second ed., 1980.
Whitaker, H.P., Yarmon, J., and Kezer, A.: Design of Model-Reference Adaptive Control Systems for Aircraft, Instrumentation Laboratory, M.I.T., Report R-164, September 1958.
Zarchan, P.: Tactical and Strategic Missile Guidance, “Progress In Astronautics and Aeronautics,” Published by the American Institute of Aeronautics and Astronautics, Inc., third edition, 1998.
A Study to Determine an Automatic Flight Control Configuration to Provide a Stability Augmentation Capability for a High-Performance Supersonic Aircraft, Minneapolis-Honeywell Regulator Company, Aeronautical Division, WADC-TR-349 (Final), May 1958.
Final Technical Report Feasibility Study Automatic Optimizing Stabilization System, Part 1, Sperry Gyroscope Company, WADC-TR-243, June 1958.
Proceedings of the Self-Adaptive Flight Control Systems Symposium, WADC-TR-59-49, March 1959.
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(2004). Aerodynamic Forces and Coefficients. In: Missile Guidance and Control Systems. Springer, New York, NY. https://doi.org/10.1007/0-387-21816-5_3
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DOI: https://doi.org/10.1007/0-387-21816-5_3
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