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自动化与信息科学期刊

每年出版 12 

ISSN 打印: 1064-2315

ISSN 在线: 2163-9337

SJR: 0.173 SNIP: 0.588 CiteScore™:: 2

Indexed in

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

卷 49, 册 6, 2017, pp. 1-21
DOI: 10.1615/JAutomatInfScien.v49.i6.10
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摘要

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.

对本文的引用
  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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