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

Nikolay V. Yefimenko

doi:10.1615/JAutomatInfScien.v49.i6.10

Journal of Automation and Information Sciences

Editor chefe: Arkadiy A. Chikriy (open in a new tab)

Editor associados: Vyacheslav F. Gubarev (open in a new tab) Yuriy P. Kondratenko (open in a new tab) Nonna V. Turovyerova (open in a new tab)

Publicou 12 edições por ano

ISSN Imprimir: 1064-2315

ISSN On-line: 2163-9337

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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, Edição 6, 2017, pp. 1-21

DOI: 10.1615/JAutomatInfScien.v49.i6.10

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Nikolay V. Yefimenko
Research and Production Enterprise "Hartron-UCOM", Zaporozhye

RESUMO

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.

Palavras-chave: spatial slewing, spatial reorientation, spacecraft motion, computational modeling

CITADO POR

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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