Abstract
For nonlinear dynamic systems, an approach based on cycle-by-cycle linearization is proposed to construct algorithms for state observers based on linear estimation theory. This approach makes it possible to analytically synthesize a full-rank and a reduced observer of the angular velocity of a spacecraft rotation relative to the body reference frame given the measurements of three angles determining the position of this reference frame in the inertial space. Simulation results are presented.
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N. E. Zubov, E. A. Mikrin, M. Sh. Misrikhanov, V. N. Ryabchenko, S. N. Timakov, and E. A. Cheremnykh, “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).
N. E. Zubov, E. A. Mikrin, V. N. Ryabchenko, and S. N. Timakov, “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).
N. E. Zubov, E. A. Mikrin, M. Sh. Misrikhanov, V. N. Ryabchenko, and S. N. Timakov, “The use of the exact pole placement algorithm for the control of spacecraft motion,” J. Comput. Syst. Sci. Int. 52, 129–144 (2013).
Handbook of Automatic Control Theory, Ed. by A. A. Krasovskii (Nauka, Moscow, 1987) [in Russian].
N. E. Zubov, E. A. Vorob’eva, E. A. Mikrin, M. Sh. Misrikhanov, V. N. Ryabchenko, and S. N. Timakov, “Synthesis of stabilizing spacecraft control based on generalized Ackermann’s formula,” J. Comput. Syst. Sci. Int. 50, 93–103 (2011).
A. V. Bogachev, E. A. Vorob’eva, N. E. Zubov, E. A. Mikrin, M. Sh. Misrikhanov, V. N. Ryabchenko, and S. N. Timakov, “Unloading angular momentum for inertial actuators of a spacecraft in the pitch channel,” J. Comput. Syst. Sci. Int. 50, 483–490 (2011).
N. E. Zubov, E. A. Mikrin, M. Sh. Misriknanov, and V. N. Ryabchenko, “Synthesis of decoupling laws for attitude stabilization of a spacecraft,” J. Comput. Syst. Sci. Int. 51, 80–96 (2012).
N. E. Zubov, E. A. Mikrin, M. Sh. Misrikhanov, and V. N. Ryabchenko, “Modification of the exact pole placement method and its application for the control of spacecraft motion,” J. Comput. Syst. Sci. Int. 52, 279–292 (2013).
N. E. Zubov, E. A. Mikrin, M. Sh. Misriknanov, and V. N. Ryabchenko, “Synthesis of controls for a spacecraft that optimize the pole placement of the closed-loop control system,” J. Comput. Syst. Sci. Int. 51, 431–444 (2012).
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Original Russian Text © N.E. Zubov, E.A. Mikrin, A.S. Oleinik, V.N. Ryabchenko, 2014, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2014, No. 5, pp. 3–16.
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Zubov, N.E., Mikrin, E.A., Oleinik, A.S. et al. Algorithms for the synthesis of observers for nonlinear dynamic systems. J. Comput. Syst. Sci. Int. 53, 623–635 (2014). https://doi.org/10.1134/S1064230714050153
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DOI: https://doi.org/10.1134/S1064230714050153