Hybrid gravitational orientation system of small spacecraft; MATEC Web of Conferences; Vol. 48 : Space Engineering

書誌詳細
Parent link:MATEC Web of Conferences
Vol. 48 : Space Engineering.— 2016.— [01002, 6 p.]
第一著者: Dmitriev V. S. Viktor Stepanovich
団体著者: Томский политехнический университет
その他の著者: Frolov R. A. Ruslan Andreevich, Bekasova A. G. Anastasiya Gennadievna
要約:Title screen
In this article is considered the problem of small satellite's angular position control. This problem is solved by some improvement. The authors offer to use active control element, in the form of gyrodyne, which to fix on the end of gravitational rod. This improvement transforms the gravitational system of orientation into a control system along three axes of orientation: yaw, roll and pitch.
言語:英語
出版事項: 2016
シリーズ:Spacecrafts and Devices
主題:
オンライン・アクセス:http://dx.doi.org/10.1051/matecconf/20164801002
http://earchive.tpu.ru/handle/11683/33700
フォーマット: 電子媒体 図書の章
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=648897

MARC

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330 |a In this article is considered the problem of small satellite's angular position control. This problem is solved by some improvement. The authors offer to use active control element, in the form of gyrodyne, which to fix on the end of gravitational rod. This improvement transforms the gravitational system of orientation into a control system along three axes of orientation: yaw, roll and pitch. 
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