Abstract
In this paper we present a design of a fuzzy system for the longitudinal control of an F-14 airplane. The longitudinal control is carried out only by controlling the elevators of the airplane. To carry out such monitoring it is necessary to use the stick, the rate of elevation and the angle of attack. These 3 variables are input into the fuzzy inference system, which is of Mamdani type, and we obtain as output the value of the elevators. After designing the fuzzy inference system we turn to the simulation stage. Simulation results of the longitudinal control are obtained using a plant in Simulink and those results are compared against the PID controller.
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References
Abusleme, H., Angel, C.: Control difuso de un vehiculo volador no tripulado, Phd Thesis, Pontificia University of Chile (2000)
Blakelock, J.: Automatic Control of Aircraft and Missiles. Wiley, New York (1965)
Dorf, R.: Modern Control Systems. Addison-Wesley Pub. Co., Reading (1997)
Dwinnell, J.: Principles of Aerodynamics. McGraw-Hill Book Company, New York (1929)
Engelen, H., Babuska, R.: Fuzzy logic based full-envelope autonomous flight control for an atmospheric re-entry spacecraft Control Engineering Practice, vol. 11(1), pp. 11–25 (January 2003)
Federal Aviation Administration, Airplane Flying Handbook, Book (2007)
Federal Aviation Administration. Pilot’s Handbook of Aeronautical Knowledge, Book (2008)
Garcia, C.: ” Everything about airplane”. Paper (2009), http://los-aviones-y-su-his-toria.blogspot.com/2009/02/40-motor-de-combustion-interna-ano-1859.html
Gardner, A.: U.S Warplanes The F-14 Tomcat, Book (2003)
Gibbens, P., Boyle, D.: Introductory Flight Mechanics and Performance. University of Sydney, Australia (1999)
Holmes, T.: US Navy F-14 Tomcat Units of Operation Iraqi Freedom, Book (2005)
Jamshidi, M., Vadiee, N., Ross, T.: Fuzzy Logic and Control: Software and Hardware Applications, vol. 2. University of New Mexico
Kadmiry, B., Driankov, D.: A fuzzy flight controller combining linguistic and model-based fuzzy control. Fuzzy Sets and Systems 146(3), 313–347 (2004)
Keviczky, T., Balas, G.: Receding horizon control of an F-16 aircraft: A comparative study. Control Engineering Practice 14(9), 1023–1033 (2006)
Liu, M., Naadimuthu, G., Lee, E.S.: Trayectory tracking in aircraft landind operations management using the adaptive neural fuzzy inference system. Computers & Mathematics with Applications 56(5), 1322–1327 (2008)
McLean, D.: Automatic Flight Control System, Book, Prentice Hall, Englewood Cliffs (1990)
McRuer, D., Ashkenas, I., Graham, D.: Aircraft Dynamics and Automatic Control. Princeton University Press, Princeton (1973)
Morelli, E.A.: Global Nonlinear Parametric Modeling with Application to F-16 Aero-dynamics, NASA Langley Research Center, Hampton, Virginia (1995)
Nelson, R.: Flight Stability and automatic control. Department of Aerospace and Mechanical Engineering, University of Notre Dame, 2nd edn. McGraw Hill, New York (1998)
Rachman, E., Jaam, J., Hasnah, A.: Non-linear simulation of controller for longitudinal control augmentation system of F-16 using numerical approach Information Sciences, vol. 164(1-4), pp. 47–60 (August 2, 2004)
Reiner, J., Balas, G., Garrard, W.: Flight control design using robust dynamic inversion and time-scale separation. Automatic 32(11), 1493–1504 (1996)
Sanchez, E., Becerra, H., Velez, C.: Combining fuzzy, PID and regulation control for an autonomous mini-helicopter. Information Sciences 177(10), 1999–2022 (2007)
Sefer, K., Omer, C., Okyay, K.: Adaptive neuro-fuzzy inference system based autono-mous flight control of unmanned air vehicles. Expert Systems with Applications In Press, Corrected Proof (June 2009)
Song, Y., Wang, H.: Design of Flight Control System for a Small Unmanned Tilt. Rotor Aircraft Chinese Journal of Aeronautics, vol. 22(3), pp. 250–256 (2009)
Walker, D.J.: Multivariable control of the longitudinal and lateral dynamics of a fly-by-wire helicopter. Control Engineering Practice 11(7), 781–795 (2003)
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Cervantes, L., Castillo, O. (2010). Design of a Fuzzy System for the Longitudinal Control of an F-14 Airplane. In: Castillo, O., Kacprzyk, J., Pedrycz, W. (eds) Soft Computing for Intelligent Control and Mobile Robotics. Studies in Computational Intelligence, vol 318. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-15534-5_13
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DOI: https://doi.org/10.1007/978-3-642-15534-5_13
Publisher Name: Springer, Berlin, Heidelberg
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