Abstract
A new adaptative algorithm for the system with reference model is proposed. Its operation does not depend on the intensity and spectral composition of the input actions and its realization does not require external disturbances estimation. The proposed algorithm functioning is illustrated in the example of large space structure (LSS) control. It is a new type of large-size spacecraft (space energy stations and large orbiting reflectors). Such an object cannot be inserted into orbit in assembled condition because of its big size. LSS, therefore, is assembled in orbit and it is a discretely evolving structure. As the control object, it is a multi-frequency oscillating system with discretely time-varying parameters and a number of freedom degrees. In the case of large space structure control proposed algorithm was simplified. Nevertheless, the control system of LSS realizes high precision.
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References
Donalson, D.D., Leondes, C.T.: A model referenced parameter tracking technique for adaptive control systems. IEEE Trans. Appl. Ind. 82, 241–262 (1963)
Hiza, J.G., Li, C.C.: Analytical synthesis of class model reference time-varying control systems. IEEE Trans. Ind. Appl. 9, 432–441 (1963)
Whitaker, H.P., Jarom, J., Kezer, A.: Design of Model Reference Adaptive Control Systems for Aircraft. Massachusetts Institute of Technology, Lab. Report R-164, Sept 1958
Parks, P.C.: Lyapunov redesign of model reference adaptive control systems. IEEE Trans. Automat. Control AC 11(3), 362–367 (1966)
Zemlyakov, S.D., Rutkovsky, V.Y.: On the synthesis of self-adjusting control systems with reference model. Avtomatika i Telemechanika 3, 70–77 (1966)
Morgan, A.P., Narendra, K.S.: On the stability of non-autonomous differential equations dx/dt = [A + B(t)]x with skew symmetric matrix. SIAM J. Control Optim. 15(1), 163–176 (1977)
Yuan, J.S.C., Wonham, W.M.: Probing Signals for Model Reference Identification. University of Toronto, Systems Control Report No 7613 (1976)
Emel’yanov, S.V.: Automatic Control Systems with Variable Structure. Nauka, Moscow (1967)
Zemlyakov, S.D., Rutkovsky, V.Y.: Precision control algorithm for a dynamic system under uncertainty based on an adaptive system with reference model. Dokladi Rossiyskoy Akademii Nauk 429(2), 176–179 (2009)
Nurre, G.S., Ryan, R.S., Skofield, H.N., Sims, J.I.: Dynamics and control of large space structures. J. Guidance 77(5), 514–526 (1984)
Rutkovsky, V.Y., Sukhanov, V.M.: Large space structure: models, methods of study and control, parts I and II. Autom. Remote Control Part 1 in 57(7), 953–963; Part 2 in 57(8), 1108–1117 (1996)
Glumov, V.M., Zemlyakov, S.D., Rutkovsky, V.Y., Sukhanov, V.M.: Spatial angular motion of flexible spacecraft. the modal physical model and its characteristics part 1. Autom. Remote Control 59(12), 1728–1738 (1998)
Acknowledgments
The work reported in this paper is a contribution to Project 14-08-01091 funded by the Russian Foundation for Basic Research, for which the authors remain grateful.
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Rutkovsky, V.Y., Glumov, V.M., Sukhanov, V.M. (2016). New Adaptive Algorithm of Flexible Spacecraft Control. In: Dimirovski, G. (eds) Complex Systems. Studies in Systems, Decision and Control, vol 55. Springer, Cham. https://doi.org/10.1007/978-3-319-28860-4_14
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DOI: https://doi.org/10.1007/978-3-319-28860-4_14
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