MATEC Web of Conferences
Volume 48, 2016IV Russian Forum for Young Scientists with International Participation “Space Engineering”
|Number of page(s)||10|
|Section||1. Spacecrafts and Devices|
|Published online||04 April 2016|
Design and analysis of power supply and information transfer to three-axis gyroscope stabilizer platform
1 National Research Tomsk Polytechnic University, 634050 Tomsk, Russia
2 Science and Technology Institute of Military, No. 17 Hoang Sam, Nghia Do, Cau Giay District, Hanoi, Viet Nam
a Corresponding author : firstname.lastname@example.org
The paper focuses on problems of the engineering implementation of 3-axis gyrostabilizer of the camera for orthophotography performed from light and ultralight aircrafts. The functional diagram of gyrostabilizer is characterized by a lighter ball-bearing having a large inner diameter used for the platform suspension on its internal (vertical) axis. The problem is to transfer the supply voltage to the platform and the electric signals to and from the platform. Design solutions concerning the power supply and information transfer are supported by the experimental techniques suggested in this paper, namely: the use of the rolling contact; three-phase gyro motor power supply replaced by that from the single-phase network; signal transmission from the precession angle sensor using the air transformer; current and voltage frequency division; DC mode selection for the torquer. The results obtained prove the efficiency of the suggested design solutions.
© 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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