Journal of Automation and Information Sciences
Erscheint 12 Ausgaben pro Jahr
ISSN Druckformat: 1064-2315
ISSN Online: 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
Volumen 49,
Ausgabe 6, 2017,
pp. 1-21
DOI: 10.1615/JAutomatInfScien.v49.i6.10
ABSTRAKT
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.
REFERENZIERT VON
-
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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