Testing of attitude control algorithms for microsatellite “Chibis-M” at laboratory facility

Author:

Ivanov D. S.,Karpenko S. O.,Ovchinnikov M. Yu.,Roldugin D. S.,Tkachev S. S.

Publisher

Pleiades Publishing Ltd

Subject

Applied Mathematics,Computer Networks and Communications,Computer Vision and Pattern Recognition,Information Systems,Theoretical Computer Science,Control and Systems Engineering,Software

Reference22 articles.

1. J. James and W. E. Howell, “Simulator Study of a Satellite Attitude Control System Using Inertia Wheels and a Magnet. Langley Station, Va”, NASA Technical Note, 63-21893 (Humpton, Langley Research Center, 1963).

2. “Research and Test Facilities for Development of Technologies and Experiments with Commercial Applications”, NASA Technical Report TM-101789 N90-10909 (Goddard Space Center, 1990).

3. B. N. Agrawal and R. E. Rasmussen, “Air Bearing Based Satellite Attitude Dynamics Simulator for Control Software Research and Development,” in Proceedings of SPIE Conference on Technologies for Synthetic Environments: Hardware-in-the-Loop Testing VI, Orlando, Florida, 2001, pp. 204–214.

4. B. Bruninga, “US Naval Academy LABsats”, AIAA JHU/APL Educational Seminar Materials, US Naval Academy (2006).

5. J. L. Schwartz and C. D. Hall, “The Distributed Spacecraft Attitude Control System Simulator: Development, Progress, Plans”, in Proceedings of Flight Mechanics Symposium, Greenbelt, Goddard Space Flight Center, Maryland, 2003.

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