Synthesis of controls for a spacecraft that optimize the pole placement of the closed-loop control system

DOI10.1134/S1064230712020141zbMath1307.93171OpenAlexW2004162610MaRDI QIDQ2263427

M. Sh. Misrikhanov, V. N. Ryabchenko, E. A. Mikrin, N. E. Zubov

Publication date: 18 March 2015

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

Full work available at URL: https://doi.org/10.1134/s1064230712020141

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Pole and zero placement problems (93B55) Synthesis problems (93B50)

Related Items (11)

Delayed feedback stabilization and the Huijberts-Michiels-Nijmeijer problem ⋮ Unnamed Item ⋮ Pyragas stabilization of discrete systems with delayed feedback and pulse periodic gain ⋮ Synthesis of spacecraft covariance controls ⋮ Asymptotic behavior of solutions of Lorenz-like systems: analytical results and computer error structures ⋮ Output control of the longitudinal motion of a flying vehicle ⋮ Synthesis of linear postcompensators for signal processing of nonlinear systems of a special form ⋮ Electrodynamic stabilization of artificial Earth satellites in the König coordinate system ⋮ Terminal synthesis of orbital orientation for a spacecraft ⋮ Algorithms for the synthesis of observers for nonlinear dynamic systems ⋮ Finite eigenvalue assignment for a descriptor system

Cites Work

• Unnamed Item
• Pole placement in large dynamical systems with many inputs and outputs
• Linear multivariable control. A geometric approach
• Superstable linear control systems. II: Design
• Synthesis of decoupling laws for attitude stabilization of a spacecraft
• Synthesis of linear quadratic control laws on basis of linear matrix inequalities
• A simple solution to the optimal eigenvalue assignment problem

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