MATEC Web of Conferences
Volume 48, 2016IV Russian Forum for Young Scientists with International Participation “Space Engineering”
|Number of page(s)||6|
|Section||1. Spacecrafts and Devices|
|Published online||04 April 2016|
Hybrid gravitational orientation system of small spacecraft
National Research Tomsk Polytechnic University, 634050 Tomsk, Russia
a Corresponding author : email@example.com
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.
© Owned by the authors, published by EDP Sciences, 2016
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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