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

Hybrid gravitational orientation system of small spacecraft

Detalles Bibliográficos
Parent link:MATEC Web of Conferences
Vol. 48 : Space Engineering.— 2016.— [01002, 6 p.]
Autor Principal: Dmitriev V. S. Viktor Stepanovich
Autor Corporativo: Национальный исследовательский Томский политехнический университет
Outros autores: Frolov R. A. Ruslan Andreevich, Bekasova A. G. Anastasiya Gennadievna
Summary: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.
Idioma:inglés
Publicado: 2016
Series:Spacecrafts and Devices
Subjects:
электронный ресурс
труды учёных ТПУ
гибридные системы
гравитация
ориентация
космические аппараты
гравитационные системы
угловое управление
Acceso en liña:http://dx.doi.org/10.1051/matecconf/20164801002
http://earchive.tpu.ru/handle/11683/33700
Formato: Electrónico Capítulo de libro
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=648897

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