Amir H. Tavakoli, Seyyed M.M. Dehghan, Adel Abedian, and Hamed Arefkhani


  1. [1] M.A.H. Clarke, Cost effective attitude control validation test methods for CubeSats applied to PolarCube, Master’s Thesis, Delft University of Technology, 2016.
  2. [2] J.L. Schwartz, M.A. Peck, and C.D. Hall, Historical review of air-bearing spacecraft simulators, Journal of Guidance, Control, and Dynamics, 26(4), 2003, 513–522.
  3. [3] J. Prado, H. Hernández, D. Vera, J. Reyes, and J. Prado, Frictionless spacecraft simulator with unrestricted three-axis movement for nanosats, International Journal of Scientific & Technology Research, 7(8), 2018, 84–95.
  4. [4] S.J. Chung, Design, implementation and control of a sparse aperture imaging satellite, Ph.D. Diss., Massachusetts Institute of Technology, 2002.
  5. [5] B. Kim, E. Velenis, P. Kriengsiri, and P. Tsiotras, Designing a low-cost spacecraft simulator, IEEE Control Systems, 23(4), 2003, 26–37. 23
  6. [6] J. Prado, G. Bisiacchi, L. Reyes, E. Vicente, F. Contreras, M. Mesinas, and A. Juárez, Three-axis air-bearing based platform for small satellite attitude determination and control simulation, Journal of Applied Research and Technology, 3(3), 2005, 222–237.
  7. [7] V.S. Chernesky, Development and control of a three-axis satellite simulator for the bifocal relay mirror initiative, Ph.D. Diss., Monterey, California, Naval Postgraduate School, 2001.
  8. [8] H. Figueiredo and O. Saotome, Design of a set of reaction wheels for satellite attitude control simulation, 22nd International Congress, Brazil, 2013.
  9. [9] W.J. Larson and J.R. Wertz, Space mission analysis and design (No. DOE/NE/32145-T1) (Torrance, CA: Microcosm, Inc., 1992).
  10. [10] P. Jelinsky, SNAP reaction wheel size, bscw.cgi/S49d0b4a1/d118194/SNAP-TECH-04025.doc, 2004.
  11. [11] N.H. Hansen, Development of a computer balanced motion table, a ground testing facility for microsatellite attitude control systems, Ph.D. Diss., National Library of Canada, 2000.
  12. [12] R.C. da Silva, F.C. Guimarães, J.V.L. de Loiola, R.A. Borges, S. Battistini, and C. Cappelletti, Tabletop testbed for attitude determination and control of nanosatellites, Journal of Aerospace Engineering, 32(1), 2019, 04018122-1–04018122-10.
  13. [13] H. Yun and L. Liu, Rapid development of air bearing threeaxis stabilized satellite, IEEE 8th Int. Conf. on CIS & RAM, Ningbo, China, 2017.
  14. [14] J. Bhagatji, G. Mohankrishna, S. Nagabhusana, S.A. Asundi, and V.K. Agrawal, Design, simulation and testing of a reaction wheel system for pico/nano-class CubeSat systems, AIAA SPACE and Astronautics Forum and Exposition, Orlando, FL, 2018.
  15. [15] G.Q. Wu, B.J. Lin, and X.L. Chen, Robust adaptive back stepping fault-tolerant attitude control for small satellite, Mechatronic Systems and Control, 40(3), 2012, 177–185.
  16. [16] R.W. Johnson and S. Jayaram, A new real-time automated ground health monitoring system at a satellite ground control station, Mechatronic Systems and Control, 32(1), 2004, 27–34.
  17. [17] P.H. Zipfel, Modeling and simulation of aerospace vehicle dynamics (Reston, VA: American Institute of Aeronautics and Astronautics, 2007).
  18. [18] A.H. Tavakoli, A. Kalhor, and S.M.M. Dehghan, Implementation of three axis attitude controllers for evaluation of a micro-gravity satellite simulator, Journal of Space Science and Technology, 5(3), 2012, 59–68 (in Persian).
  19. [19] J. Dongwon and P. Tsiotras, A 3-dof experimental test-bed for integrated attitude dynamics and control research, AIAA Guidance, Navigation, and Control Conference and Exhibit, Austin, Texas, 2003
  20. [20] A.H. Tavakkoli, M. Kabganian, and M. Shahravi, Modeling of attitude control actuator for a flexible spacecraft using an extended simulation environment, ICCA’05. Int. Conf. on Control and Automation, Budapest, vol. 1, 2005, 147–152.
  21. [21] K.H. Decker and K. Kabus, Machine elements function, design and calculation (Munich: Hanser, 2007) (in German).

Important Links:

Go Back