NDLI: Influence of disturbances on the angular motion of a spacecraft in the powered section of its descent

Content Provider	Semantic Scholar
Author	Aslanov, Vladimir S. Doroshin, Anton V.
Copyright Year	2008
Abstract	The motion of a variable-mass spacecraft is considered in the powered section of a descending trajectory. Approximate analytical solutions are obtained for the angles of spatial orientation of the spacecraft, which allows one to analyze the nutation motion and to develop recommendations on the spacecraft's mass configuration, providing the smallest possible deviations of the longitudinal axis and thrust vector from specified directions. The errors of stabilization of the spacecraft's longitudinal axis are calculated by means of numerical integration of complete models and using the obtained analytical solutions, the results being in good agreement.
Starting Page	166
Ending Page	171
Page Count	6
File Format	PDF HTM / HTML
DOI	10.1134/S001095250802007X
Volume Number	46
Alternate Webpage(s)	http://termech.ru/sites/default/files/papers/CosRes2_08AslanovLO.pdf
Alternate Webpage(s)	https://doi.org/10.1134/S001095250802007X
Language	English
Access Restriction	Open
Content Type	Text
Resource Type	Article

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