Digital Control Systems
Modern Control Systems
The band formula for A.N. Krylov's problem
Automation and Remote Control
Synthesis of decoupling laws for attitude stabilization of a spacecraft
Journal of Computer and Systems Sciences International
Journal of Computer and Systems Sciences International
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For a linear steady model of spacecraft motion, a method for the simultaneous observation and identification in the process of motion control is proposed. The method is based on the exact pole placement algorithm and the mathematical model of the Luenberger observer. Examples illustrating the advantages of this method for practical observation and identification problems in controlling a spacecraft motion are discussed.