Synthesis of stabilizing spacecraft control based on generalized Ackermann's formula

DOI10.1134/S1064230711010199zbMath1267.93050MaRDI QIDQ356984

V. N. Ryabchenko, E. A. Vorob'eva, M. Sh. Misrikhanov, N. E. Zubov, E. A. Mikrin, S. N. Timakov

Publication date: 29 July 2013

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

zbMATH Keywords

Ackermann's formulacomplex dynamic systemmodal synthesisstabilization of orbital orientation

Mathematics Subject Classification ID

Application models in control theory (93C95) Variable mass, rockets (70P05) Adaptive or robust stabilization (93D21) Synthesis problems (93B50) Control/observation systems governed by ordinary differential equations (93C15)

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Delayed feedback stabilization and the Huijberts-Michiels-Nijmeijer problem ⋮ Unnamed Item ⋮ Unnamed Item ⋮ The use of the exact pole placement algorithm for the control of spacecraft motion ⋮ Synthesis of spacecraft covariance controls ⋮ Unnamed Item ⋮ Asymptotic behavior of solutions of Lorenz-like systems: analytical results and computer error structures ⋮ Unnamed Item ⋮ Terminal synthesis of orbital orientation for a spacecraft ⋮ Synthesis of decoupling laws for attitude stabilization of a spacecraft ⋮ Identification of the position of an equilibrium attitude of the international space station as a problem of stable matrix completion ⋮ Modification of the exact pole placement method and its application for the control of spacecraft motion ⋮ Algorithms for the synthesis of observers for nonlinear dynamic systems

Cites Work

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