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Journal of Automation and Information Sciences

Publicou 12 edições por ano

ISSN Imprimir: 1064-2315

ISSN On-line: 2163-9337

SJR: 0.173 SNIP: 0.588 CiteScore™:: 2

Indexed in

Attitude Control of a Spacecraft in the Orbital Coordinate System Using Ellipsoidal Estimates of its State Vector

Volume 31, Edição 4-5, 1999, pp. 24-32
DOI: 10.1615/JAutomatInfScien.v31.i4-5.230
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RESUMO

The problem of attitude control of a rigid body in the orbital coordinate system is considered. Algorithms for ellipsoidal estimation of the state vector of the control object (CO) are used in the control loop. As distinct from the well-know algorithms, these algorithms are characterized by robustness relative to violations of a priory assumptions as to CO. The control algorithms are synthesized based on the direct Lyapunov method and its generalizations. The efficiency of the adaptive control algorithms is illustrated by results of computer simulation.

CITADO POR
  1. Volosov V.V., Shevchenko V.M., Synthesis of control of the angular motion of a spacecraft on the basis of generalization of the direct Lyapunov method, Kosmìčna nauka ì tehnologìâ, 24, 4, 2018. Crossref

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