Chernesky, V. S., “Development and Control of a Three-Axis Satellite Simulator for the Bifocal Relay Mirror Initiative,” (M. Sc. thesis), Naval Postgraduate School Monterey, California, 2001.
 Roemer, S., Terzibaschian, T., Wiener, A. and Bärwald, W., “Experiences with the BIRD ACS Test Facility and the Resulting Design of a State of the Art Mini-and Micro-Satellite ACS Test Facility,” Small Satellites for Earth Observation - Digest of the 6th International Symposium of the International Academy of Astronautics, Berlin, VI, 2007, pp. 165-168.
 Kato, T., Heidecker, A., Dumke, M. and Theil, S., “Three-Axis Disturbance-Free Attitude Control Experiment Platform : FACE
,” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan
, Vol. 12, No. ists29, 2014.
 Raschke, C., Roemer, S. and Grossekatthoefer, K., “Test bed for Verification of Attitude Control System,” url:http:/ /www.astrofein.com/2728/dwnld/admin/Paper_TestBed.pdf.
 Somanathan, A., Lakkoju, S., Bhagavan, M.K. and Natarajan, P., “Designing and Evaluation of an Experimental Attitude Determination system Using Sun Sensor and Magnetometer,” Spacecraft Motion Simulator and associated Modeling for Realistic Hardware-In-Loop Simulation,” 16th National Conference on Machines and Mechanisms (iNaCoMM2013), IIT Roorkee, India, Dec 18-20 2013
 Chesi, S., Perez, O. and Romano, M., “A Dynamic, Hardware-in-the-Loop, Three-Axis Simulator of Spacecraft Attitude Maneuvering with Nanosatellite Dimensions,” Journal of Small Satellites (JoSS), Vol. 4, No. 1, 2015, pp. 315–328.
 Tavakkoli, A.H., Yazdanian, M., Koolivand, Y., Shahravi, M., Momeni, M. and Dehghan, S.M.M., “Designing and Evaluation of an Experimental Attitude Determination System Using Sun Sensor and Magnetometer,” Journal of Space Science and Technology, Vol. 5, No. 4, 2013, pp.69-78 (In Persian).
 Mousavi, S.M.S. and Mortazavi, M., “Functional Tests of the prototype of Earth Magnetic Field Simulator,” 16th Geophysic Confrence of Iran, 2014 (In Persian).
 Mousavi, S.M.S. and Mortazavi, M., “Design, Construction, test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite,” Journal of Space Science and Technology, Vol. 9, No. 2, 2016, pp. 25-34 (In Persian).
 Bolandi, H., Ghahremani, M., Alinaghi, S.M., Ghorbani, B. and Esmaeelzadeh, S.M., “Helmholtz Coil and Calibration Table Design,” 13th Iranian Iranian Aerospace Society Conference, Tehran University, 2014 (In Persian).
 Kermanshahi, F., Mohajerani, M.H., Babini, M.H. and Mortazavi, M. “Design and Manufacturing of Sun Motion Simulator Applied to Satellites Attitude Determination,” Applied Mechanics and Materials, Switzerland, 2012.
 Bolandi, H., Esmaeelzadeh, S.M., Ghorbani, B., Ghahremani, M., Hasanian, M., and Abedi, M.,“ Satellite Solar Sensor Performance Testing in Thermal Vacuum Conditions,” 10th Iranian Iranian Aerospace Society Conference, Tarbiat Modares University, 2011 (In Persian).
 Wertz, J.R., Spacecraft Attitude Determination and Control, Kluwer Academic Publishers,1999
 Vallado, D.A., Fundamentals of Astrodynamics and Applications, McGraw-Hill, 1997.
 IAGA, Available, [Online]: https://www.ngdc. noaa. gov/IAGA/vmod/igrf11coeff.txt. [Accessed 2015].
 Products," Optical Energy, Available, [Online]: http:// www.opticalenergy.com/s13-solar-simulator/. [Accessed 2015].
 Products," Honeywell, Available, [Online]: https:// aerospace.honeywell.com/en/~/media/aerospace/files/datasheet/3-axismagneticsensorhybridhmc2003_ds.pdf. [Accessed 2015].
 Wie, B., Space Vehicle Dynamics and Control, AIAA Education Series, 1998.