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Journal of Automation and Information Sciences

Publication de 12  numéros par an

ISSN Imprimer: 1064-2315

ISSN En ligne: 2163-9337

SJR: 0.173 SNIP: 0.588 CiteScore™:: 2

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Synthesis of Time Optimal Spatial Slewing of Spacecraft Using Dynamic Equation of Rigid Body Rotational Motion at Rodrigues−Hamilton Parameters

Volume 49, Numéro 6, 2017, pp. 1-21
DOI: 10.1615/JAutomatInfScien.v49.i6.10
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RÉSUMÉ

Algorithm of spacecraft spatial reorientation over a minimum time is proposed. Unlike known solutions, the proposed approach does not impose any restrictions on the character of spacecraft motion. The results of computational modeling of the proposed algorithm operation are presented.

CITÉ PAR
  1. 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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