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Journal of Automation and Information Sciences

Published 12 issues per year

ISSN Print: 1064-2315

ISSN Online: 2163-9337

SJR: 0.173 SNIP: 0.588 CiteScore™:: 2

Indexed in

Synthesis of Control Algorithms of the Spacecraft Spatial Reorientation with the Use of Dynamic Equations of a Solid Body Rotational Motion in Rodrigo-Hamilton Parameters

Volume 47, Issue 6, 2015, pp. 1-16
DOI: 10.1615/JAutomatInfScien.v47.i6.10
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ABSTRACT

An algorithm for SC spatial reorientation in a specified time interval is presented. In contrast to the classical formulation the traditional restrictions are not imposed on the class of spacecraft angular motions. The proposed approach based on the maximum principle allows one to obtain an analytical solution of the problem of optimal spatial reorientation of the spacecraft. On the basis of the proposed algorithm software for the mode of spacecraft "Egyptsat-l" and "Sich-2" rotations has been implemented.

CITED BY
  1. Khoroshylov S.V., Shamakhanov V.K., Vasyliev V.V., Modeling of centrifugal deployment of three-section minisatellite boom, Technical mechanics, 2021, 4, 2021. Crossref

  2. Sedelnikov A. V., Salmin V. V., Modeling the disturbing effect on the aist small spacecraft based on the measurements data, Scientific Reports, 12, 1, 2022. Crossref

  3. Yefymenko Nikolay, Kudermetov Ravil, Quaternion models of a rigid body rotation motion and their application for spacecraft attitude control, Acta Astronautica, 194, 2022. Crossref

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