Abstract
A method of synthesizing control algorithms by using the concepts of inverse dynamic problems is presented. The problems of how to control the rotational motion and pitch angle of air-craft are solved. The dynamic problems are analyzed theoretically and it is shown that the synthesized algorithms give the natural properties of parametric adaptivity to the systems. The results of the mathematical simulation are presented.
Similar content being viewed by others
References
Pospelov, G.S., Avtomaticheskoe upravlenie poletom samoleta (Aircraft Flight Automatic Control), Moscow: VVIA im. Zhukovskogo, 1959.
Bodner, V.A., Teoriya avtomaticheskogo upravleniya poletom (Theory of Flight Automatic Control), Moscow: Nauka, 1964.
Krasovskii, A.A., Sistemy avtomaticheskogo upravleniya poletom i ikh analiticheskoe konstruirovanie (Automatic Systems of Flight Control and Their Analytical Design), Moscow: Nauka, 1973.
Krut’ko, P.D., Obratnye zadachi dinamiki upravlyemykh sistem. Nelineinye modeli (Inverse Problems of Control Systems Dynamics. Nonlinear Models), Moscow: Nauka, 1988.
Krut’ko, P.D., Obratnye zadachi dinamiki v teorii avtomaticheskogo upravleniya. Tsikl lekstii (Inverse Dynamic Problems in Automatic Control Theory. Lecture Course), Moscow: Mashinostroenie, 2004.
Tsypkin, Ya.Z., Osnovy teorii avtomaticheskikh sistem (Foundations of Automatic Control Systems), Moscow: Nauka, 1977.
Voronov, A.A., Ustoichivost’, upravlyaemost’, nablyudaemost’ (Stability, Controllability, Observability), Moscow: Nauka, 1979.
Author information
Authors and Affiliations
Additional information
Original Russian Text © P.D. Krut’ko, 2010, published in Problemy Mashinostroeniya i Nadezhnosti Mashin, 2010, No. 2, pp. 83–95.
About this article
Cite this article
Krut’ko, P.D. Algorithms of a nontraditional structure in the problems of the control of the longitudinal motion of aircraft. J. Mach. Manuf. Reliab. 39, 168–178 (2010). https://doi.org/10.3103/S1052618810020123
Received:
Published:
Issue Date:
DOI: https://doi.org/10.3103/S1052618810020123