Development of a novel device for attitude control over small satellites

被引：3

作者：

Bakanauskas, Vytautas ^{[1
]}

Bansevičius, Ramutis ^{[2
]}

Bručas, Domantas ^{[3
]}

Domeika, Aurelijus ^{[2
]}

机构：

[1] Kaunas University of Technology, Space Science and Technology Institute, K. Donelaičio g. 73, LT-44029 Kaunas/Saulėtekio av. 15, Vilnius

[2] Kaunas University of Technology, K. Donelaičio g. 73, Kaunas

[3] Space Science and Technology Institute, Saulėtekio av. 15, Vilnius

来源：

Solid State Phenomena | 2015年 / 220-221卷

关键词：

Attitude control; Momentum of inertia; Nano-satellite; Piezoelectric actuator; Reaction-sphere;

D O I：

10.4028/www.scientific.net/SSP.220-221.561

中图分类号：

学科分类号：

摘要：

Recent years have faced a very modern trend for space exploration activities – constructing, launching and operating nano-satellites have become very popular. One of the major problems of implementing and taking control over the nano-satellite is ensuring accurate but simple and small dimension equipment for attitude control. Most of the equipment implemented for the introduced task was large and bulky in the past and could be hardly used on extremely small satellites. The paper describes equipment under development for attitude control over satellites. Equipment relies on the implementation of piezoelectric transducers for the rotation of a spherical body, i.e. reaction sphere, thus ensuring precise three-axis attitude control over the satellite by means of a single device. Further, the article focuses on the device under development with some calculations and examples of implementing such instruments. © (2015) Trans Tech Publications, Switzerland.

引用

页码：561 / 564

页数：3

共 9 条

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