Identification of the position of an equilibrium attitude of the international space station as a problem of stable matrix completion
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Publication:2263414
DOI10.1134/S1064230712010133zbMath1307.93120OpenAlexW1995168164MaRDI QIDQ2263414
V. N. Ryabchenko, N. E. Zubov, M. Sh. Misrikhanov, E. A. Mikrin, E. A. Cheremnykh, S. N. Timakov
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/s1064230712010133
System identification (93B30) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)
Related Items (8)
The use of an adaptive bandpass filter as an observer in the control loop of the international space station ⋮ The use of the exact pole placement algorithm for the control of spacecraft motion ⋮ Methods for the vibration determination and parameter identification of spacecraft with flexible structures ⋮ Terminal synthesis of orbital orientation for a spacecraft ⋮ 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 ⋮ An efficient method for convex constrained rank minimization problems based on DC programming ⋮ Application of generalized Butterworth polynomials for stabilization of the equilibrium position of a space station
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- Synthesis of stabilizing spacecraft control based on generalized Ackermann's formula
- \(D\)-decomposition technique state-of-the-art
- Randomized algorithms for analysis and control of uncertain systems. With a foreword by M. Vidyasagar
- Hard problems in linear control theory: possible approaches to their solution
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