Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators
A method is proposed for solving the problem of controlling finite eigenvalues of a descriptor linear dynamic system, which is based on the original decomposition of the model of the initial system that is unsolved for the derivatives and is defined in the space of states. This method has no restric...
|Published in:||Journal of computer and systems sciences international, Vol. 54, No. 4 (2015), p. 621-628|
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|Item Description:||Original Russian Text © N.E. Zubov, E.A. Mikrin, M.Sh. Misrikhanov, V.N. Ryabchenko, 2015, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2015, No. 4, pp. 124–131.|
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