Attitude Control of Micro- and Nanosatellites Using Multi-degree-of-Freedom Piezoelectric Actuators

Author:

Bansevicius Ramutis,Kargaudas V.

Publisher

Springer Netherlands

Reference8 articles.

1. Samir A.R.: Passive attitude stabilization for small satellites. Thesis, The Graduate School University of Kentucky, Lexington (2009)

2. Ortega, P., et al.: Miniaturized two axis sun sensor for attitude control of nano-satellites. Sens. J. IEEE 10(10), 1623–1632 (2010) (ISSN: 1530-37X)

3. Kundu, P., Bhattacharyya, T.K., Das, S.: A monopropellant hydrazine MEMS thruster for attitude control of nanosatellites. In: Students’ Technology Symposium (TechSym), 2010 IEEE, IEEE Explore Digital Library (IEEE Xplore), 3–4 April 2010, pp. 137–141. ISBN: 978-1-4244-5975-9

4. Iai, M., Durali, M., Hatsuzawa, T.: Attitude control of nanosatellites by paddle motion using elastic hinges actuated by shape memory alloy. J. Space Eng. 3(1), 38–51 (2010)

5. Bansevicius R., Ahmed S.: Bearings and support. US Patent 6,262,514 (2001)

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