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

Problem of modal synthesis of controllers and observers using the generalized Ackermann’s formula is solved for a spacecraft as a complex dynamic system with high interconnections. All possible controller matrices (the whole set of controllers) are obtained for solution of the problem of stabilizati...

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Bibliographic Details
Published in:Journal of computer & systems sciences international 2011-02, Vol.50 (1), p.93-103
Main Authors: Zubov, N. E., Vorob’eva, E. A., Mikrin, E. A., Misrikhanov, M. Sh, Ryabchenko, V. N., Timakov, S. N.
Format: Article
Language:English
Subjects:
Channels
Computer science
Control
Control algorithms
Control systems
Control Systems of Moving Objects
Controllers
Dynamical systems
Dynamics
Engineering
Mathematical analysis
Matrices
Mechatronics
Orbitals
Robotics
Spacecraft
Studies
Synthesis
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Summary:Problem of modal synthesis of controllers and observers using the generalized Ackermann’s formula is solved for a spacecraft as a complex dynamic system with high interconnections. All possible controller matrices (the whole set of controllers) are obtained for solution of the problem of stabilization of orbital orientation of the spacecraft in inseparable channels of bank and yaw angles.
ISSN:1064-2307
1555-6530
DOI:10.1134/S1064230711010199