Ultra-High Accurate Attitude Determination and Control of Microsatellite Formation Flight

Öz

Nowadays, technology and space science are developing rapidly, providing new possibilities for multi-segment missions to become a frequent practice. This relates to small satellites, which could be used to organize a formation, in order to solve complex scientific and applied problems. A formation could serve as distributed instruments for atmospheric sampling, construct a large distributed antenna platform, or make a large distributed aperture for imaging and other applications what only a big satellite can achieve. Small satellite’s formation flying is low cost space project compared to one big satellite. However, to develop satellite formation a lot of problems should be solved depending on its mission.

One of the important tasks in small satellite formation is an accurate determination and control of position and attitude.  This paper provides a mathematical modelling of a small satellite’s formation motion, which is essential to realize a synthetic aperture telescope. Furthermore, the paper describes the principle of formation configuration and its design. 

Anahtar Kelimeler

• geostationary orbit,formation flight,formation flying control,microsatellite

Kaynakça

1. Jesse Leitner. Formation Flying: The Future of Remote Sensing from Space. Proceedings of the International Symposium on Space Flight Dynamics, Munich, Oct., 2004, 11–15.
2. Saptashi Bandyopadhyay, Rebecca Foust, Giri P. Subramanian, Soon-Jo Chung, and Fred Y. Hadaegh. Review of Formation Flying and Constellation Missions Using Nanosatellites. Journal of spacecrafts and Rockets, Vol. 53, No.3,1-12 (2016).
3. D. C. Folta, L. K. Newman and T. Gardner. Foundations of Formation Flying for Mission to Planet Earth and New Millennium. AIAA, 1996, 656–666.
4. Gokhan Inalhan, Franz D.Busse and Jonathan P.How. Precise formation flying control of multiple spacecraft using carrier-phase differential GPS. Proc. of AAS/AIAA Space Flight Mechanics Conference, Clearwater, FL, Paper No. AAS 00-109, January 23-26, 2000.
5. Kun Liu, Yanfeng Qiao, Xiangyong Duan. Optical remote imaging using Fizeau synthetic aperture telescope. Proc. of Lasers & Electro Optics & The Pacific Rim Conference on Lasers and Electro-Optics, Shanghai China, August 31 – September 3, 2009.
6. http://www.keyence.com/
7. Journals William J Weber, Antonella Cavalleri, Rita Dolesi, Giorgio Fontana, Mauro Hueller, and Stefano Vitale. Position sensors for LISA drag-free control. Classical and Quantum Gravity, Vol.19, No.7, 1751-1752 (2002).
8. Proceedings (Transactions, Book of abstracts, Proceedings on CD, etc.) John K. Ziemer and Stephen M. Merkowitz. Microthrust propulsion of the LISA mission. Proc. of 40th AIAA joint propulsion conference. Fort Lauderdale, Florida, July 12-14, 2004

9. Yablonskiy A.A., Nikiforova V.M., Kurs teoreticheskoy mehaniki. – SPb.: «Lan», 2001. – 504 p.
10. Markeev A.P., Teoreticheskaya mehanika, M.: «CheRo», 1999. – 96 p.
11. Beletskiy V.V., Dvizhenie sputnika otnositelno tsentra mass v gravitatsionnom pole, M.: 1975, 17 p.