Abstract
For a discrete model of the angular motion of the International Space Station, using an onboard identification model, the problem of identification of the equilibrium attitude position is solved under the action of aerodynamic, gravitational, gyroscopic moments. It is shown that the convergence of the iteration process is determined by a choice of weight coefficients in the equations of the identification onboard model. In this paper, the possibility of finding numerical values of the weight coefficients by solving the problem of stable matrix completion is addressed. A symbolic method for solving the problem of stable matrix completion is proposed. Using this method, numerical values of the weight coefficients that provide fast convergence of the iteration search of an equilibrium attitude of the International Space Station are obtained.
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