The use of the exact pole placement algorithm for the control of spacecraft motion

DOI10.1134/S1064230713010127zbMath1279.93060OpenAlexW2063552705MaRDI QIDQ394076

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

Publication date: 24 January 2014

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

Full work available at URL: https://doi.org/10.1134/s1064230713010127

zbMATH Keywords

motion controlLuenberger observerexact pole placement algorithmlinear steady modelmethod for practical observationsimultaneous observationspacecraft motion

Mathematics Subject Classification ID

System identification (93B30) Variable mass, rockets (70P05) Pole and zero placement problems (93B55) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (8)

Delayed feedback stabilization and the Huijberts-Michiels-Nijmeijer problem ⋮ Asymptotic behavior of solutions of Lorenz-like systems: analytical results and computer error structures ⋮ Output control of the longitudinal motion of a flying vehicle ⋮ Electrodynamic stabilization of artificial Earth satellites in the König coordinate system ⋮ Methods for the vibration determination and parameter identification of spacecraft with flexible structures ⋮ Terminal synthesis of orbital orientation for a spacecraft ⋮ Terminal bang-bang impulsive control of linear time invariant dynamic systems ⋮ Algorithms for the synthesis of observers for nonlinear dynamic systems

Cites Work

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• Synthesis of stabilizing spacecraft control based on generalized Ackermann's formula
• The use of an adaptive bandpass filter as an observer in the control loop of the international space station
• The band formula for A.N. Krylov's problem
• Linear multivariable control. A geometric approach
• Superstable linear control systems. II: Design
• Identification of the position of an equilibrium attitude of the international space station as a problem of stable matrix completion
• Synthesis of linear quadratic control laws on basis of linear matrix inequalities
• Robust pole assignment in linear state feedback

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