Abstract
For a parametrically uncertain model of the International Space Station (ISS), an algorithm using an adjustable model is proposed; on the basis of this algorithm, a self-tuning discrete bandpass filter is designed. The asymptotic stability of the proposed algorithm is ensured using the novel method for solving the matrix completion problem where the completed matrix is required to be stable. The use of the symbolic method for solving the matrix completion problem makes it possible to obtain a universal solution of the self-tuning bandpass filter design problem.
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Theoretical Foundations of the Design of Information and Control Systems of Spacecraft, Ed. by E. A. Mikrin (Nauka, Moscow, 1975) [in Russian].
P. Eykhoff, System Identification: Parameter and State Estimation (Wiley-Interscience, London, 1974; Mir, Moscow, 1975).
N. E. Zubov, E. A. Mikrin, M. Sh. Misriknanov, V. N. Ryabchenko, S. N. Timakov, and E. A. Chernykh, “Identification of the Position of an Equilibrium Attitude of the International Space Station as a Problem of Stable Matrix Completion,” J. Comput. Syst. Sci. Int. 51, 291–305 (2012).
K. A. Abgaryan and N. M. Rapoport, Dynamics of Rockets (Mashinostroenie, Moscow, 1969) [in Russian].
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Original Russian Text © N.E. Zubov, E.A. Mikrin, V.N. Ryabchenko, S.N. Timakov, 2012, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2012, No. 4, pp. 88–100.
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Zubov, N.E., Mikrin, E.A., Ryabchenko, V.N. et al. The use of an adaptive bandpass filter as an observer in the control loop of the international space station. J. Comput. Syst. Sci. Int. 51, 560–572 (2012). https://doi.org/10.1134/S1064230712030124
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DOI: https://doi.org/10.1134/S1064230712030124