[1] H. Taei, Optimal Design Layout for a Tri-axial Satellite Attitude Dynamics Simulator with Combinatorial Actuators, Ph.D. Thesis, Aeospace Engineering Faculty, K. N. Toosi University of Technology, I.R. Iran, 2015 (In Persian فارسی).
[2] M. Mirshams, H. Taei, M. Ghobadi, H. Haghi, G. Sharifi, using air-bearing based platform and cold gas thruster actuator for satellite attitude dynamics simulation, Modares Mechanical Engineering Journal, vol. 14, no. 12, pp. 1-12, 2015 (In Persian فارسی).
[3] M. Mirshams, H. Taei, V. Rezvani, E. Taheri, Deriving the Dynamic Equation and Design of an Optimal Controller for a Satellite Attitude Motion Simulator and Comparison with PID Controller, 9th Iranian Aerospace Association Conference, I.R. Iran, 2010 (In Persian فارسی).
[4] B. Kim, E. Velenis, P. Kriengsiri, P. Tsiotras, Designing a low-cost spacecraft simulator, Control Systems, IEEE, vol. 23, no. 4, pp. 26-37, 2003.
[5] M. Mirshams, A. Nahvi, M. Khosrojerdi, H. Taei, M. Vahid, a 6-DoF Satellite Virtual Simulator Design and Development, Applied Mechanics and Materials, vol. 186, pp. 70-74, 2013.
[6] J. E. Colebank, R. D. Jones, G. R. Nagy, R. D. Pollak, D. R. Mannebach, SIMSAT: a satellite system simulator and experimental test bed for air force research, M. Sc. Thesis, Department of Aeronautics and Astronautics, Air Force Institute of Technology, USA, 1999.
[7] J. L. Schwartz, the distributed spacecraft attitude control system simulator: from design concept to decentralized control, Ph.D. Thesis, Aerospace Engineering Faculty, Virginia Polytechnic Institute and State University, USA, 2004.
[8] D. Gallardo, R. Bevilacqua, Six Degrees of Freedom Experimental Platform for Testing Autonomous Satellites Operations, Proceedings of the 8th International ESA GNC Conference, Czech Republic, 2011.
[9] M. Mirshams, H. Taei, M. Vahid, A Systems Engineering for Satellite Simulator Design, ASME Conference on Systems Engineering, Turkey, 2010.
[10] J. E. Smith, Attitude model of a reaction wheel/fixed thruster based satellite using telemetry data, M. Sc. Thesis, Departmentof Aeronautics and Astronautics, Air Force Institute of Technology, USA, 2005.
[11] M. Mirshams, H. Taei, M. Ghobadi, H. Haghi, E. Zabihian, Spacecraft Attitude Dynamics Simulator with Combinatorial Actuators, Electronics Industries Quarterly, vol. 4, no. 4, pp. 13-27, 2013. (In Persian فارسی).
[12] J. L. Schwartz, C. D. Hall, System identification of a spherical air-bearing spacecraft simulator, AAS Paper, vol. 122, 2004.
[13] M. Mirshams, H. Taei, A. Novin-zadeh, A 3-DoF Satellite Simulator Design & Development, 60th International Aerospace Congress, South Korea, 2000.
[14] M. Mirshams, H. Taei, M. Ghobadi, H. Haghi, Spacecraft Attitude Dynamics Simulator Actuated by Cold Gas Propulsion System, Proceeding of the Institution of Mechanical Engineering, Part G: Journal of Aerospace Engineering, vol. 5, no. 3, pp. 1510-1530, 2015.
[15] C. G. McChesney, Design of attitude control actuators for a simulated spacecraft, M. Sc. Thesis, Department of Aeronautics and Astronautics, Air Force Institute of Technology, USA, 2011.
[16] J. L. Schwartz, M. A. Peck, C. D. Hall, Historical review of air-bearing spacecraft simulators, Journal of Guidance, Control, and Dynamics, vol. 26, no. 4, pp. 513-522, 2003.
[17] M. Mirshams, H. Taei, H. Haghi, V. Rezvani, Design and Manufacturing of a Tri-axial Spacecraft Attitude Motion Simulator, 1st Conference on Flight Simulation, I.R. Iran, 2009 (In Persian فارسی).
[18] M. Mirshams, M. Ghobadi, H. Taei, Design, Development and Test of an Engineering Sample of Cold Gas Thruster for Using in a Tria-axialSatellite Attitude Dynamics Simulator, Sharif Mechanical Engineering Journal, vol. 8, no. 2, pp. 150-165, 2013 (In Persian فارسی).
[19] H. C. Schubert, J. P. How, Space Construction: An Experimental Testbed to Develop Enabling Technologies, Proceedings of the Conference on Telemanipulator and Telepresence Technologies IV, USA, 1997.
[20] S. Matunaga, K. Yoshihara, T. Takahashi, S. Tsurumi, K. Ui, Ground Experiment System for Dual-Manipulator-Based Capture of Damaged Satellites, Proceedings of the IEEE/RSJ International Conference on Intelligent Robots and Systems, Japan, 2000.
[21] B. Pond, I. Sharf, Experimental Demonstration of Flexible Manipulator Trajectory Optimization, Proceedings of the AIAA Guidance, Navigation and Control Conference, USA, 1999.
[22] M. G. Spencer, Development of a servicing satellite simulator, Proceedings of the AIAA space conference and exposition, USA, 2001.
[23] R. L. Kinnett, System Integration and Control of a Low-Cost SpacecraftAttitude Dynamics Simulator, MSc. Thesis, Aerospace Engineering, California Polytechnic State University, 2010.
[24] D. M. Meller, J. Reiter, M. Terry, K. F. Böhringer, M. Campbell, A docking system for microsatellites based on MEMS actuator arrays, Proceedings of the AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference and Exhibit, USA, 2001.
[25] W. R. Wilson, L. L. Jones, M. A. Peck, A Multimodule Planar Air Bearing Testbed for CubeSat-Scale Spacecraft, Journal of Dynamic Systems, Measurement, and Control, vol. 135, no. 4, pp. 1-10, 2013.
[26] B. H. Dishman, F. J. Moran, Air bearing table mechanization and verification of a spacecraft wide angle attitude control system, Journal of Spacecraft and Rockets, vol. 7, no. 7, pp. 819-825, 1970.
[27] H. Taei, Optimal Design of a Satellite Attitude Motion Simulator, MSc. Thesis, Aeospace Engineering Faculty, K. N. Toosi University of Technology, 2009 (In Persian فارسی).
[28] S. Sanz Fernandez de Cordova, D. Debra, Mass center estimation of a drag-free satellite, international Federation of Automatic Control, 6th Triennial World Congress, USA, 1975.
[29] D. C. Fosth, The Lunar Orbiter Attitude Control Simulator, Aerospace and Electronic Systems, IEEE Transactions on, no. 3, pp. 417-423, 1967.
[30] B. N. Agrawal, Acquisition, tracking and pointing of bifocal relay mirror spacecraft, Advances in the Astronautical Sciences, vol. 114, pp. 783-800, 2003.
[31] B. N. Agrawal, R. Mcclelland, G. Song, Attitude control of flexible spacecraft using pulse-width pulse-frequency modulated thrusters, Space Technology-Kedlington, vol. 17, no. 1, pp. 15-34, 1997.
[32] B. N. Agrawal, R. E. Rasmussen, Air-bearing-based satellite attitude dynamics simulator for control software research and development, Aerospace/Defense Sensing, Simulation, and Controls, USA, 2001.
[33] G. Song, B. N. Agrawal, Vibration suppression of flexible spacecraft during attitude control, Acta Astronautica, vol. 49, no. 2, pp. 73-83, 2001.
[34] J. Lau, S. S. Joshi, B. N. Agrawal, J.-W. Kim, Disturbance filtering and identification on the naval postgraduate school 3-axis spacecraft simulator, Proceedings of the AIAA guidance, navigation, and control conference and exhibit, USA, 2005.
[35] R. R. Fullmer, Dynamic Ground Testing of the Skipper Attitude Control System, Proceedings of the 34th AIAA Aerospace Sciences Meeting & Exhibit, USA, 1996.
[36] B. Kim, E. Velenis, P. Kriengsiri, P. Tsiotras, A spacecraft simulator for research and education, Proceedings of the AIAA/AAS Astrodynamics Specialists Conference, USA, 2001.
[37] D. Jung, P. Tsiotras, A 3-dof experimental test-bed for integrated attitude dynamics and control research, AIAA Guidance, Navigation & Control Conference, USA, 2003.
[38] J. Li, M. A. Post, R. Lee, Nanosatellite attitude air bearing system using variable structure control, 25th IEEE Canadian Conference on Electrical & Computer Engineering, 2008.
[39] M. A. Peck, L. Miller, A. R. Cavender, M. Gonzalez, T. Hintz, An airbearing-based testbed for momentum control systems and spacecraft line of sight, Advances in the Astronautical Sciences, vol. 114, pp. 427-446, 2003.
[40] J. Prado, G. Bisiacchi, L. Reyes, E. Vicente, F. Contreras, M. Mesinas, A. Juárez, Three-axis air-bearing based platform for small satellite attitude determination and control simulation, Journal of Applied Research and Technology, vol. 3, no. 3, pp. 222-237, 2005.
[41] A. Das, J. L. Berg, G. A. Norris, D. F. Cossey, T. J. Strange III, W. T. Schlaegel, Astrex-a unique test bed for CSI research, in Decision and Control, Proceedings of the 29th IEEE Conference on Decision and Control, USA, 1990.
[42] N. G. Creamer, G. C. Kirby, R. E. Weber, A. B. Bosse, S. Fisher, An integrated gps/gyro/smart structures architecture for attitude determination and baseline metrology, Proceedings of the AIAA Guidance, Navigation, and Control Conference, USA, 1997, pp. 1945-1955.
[43] D. Halsmer, W. Bair, P. Ng, The Spinning Rocket Simulator: An Experimental DesignProject for Teaching and Research, ASEE Annual Conference & Exposition, USA, 1996.
[44] B. J. Kim, H. Lee, Spacecraft attitude dynamics analysis using three-axis air bearing, Space Technology, vol. 17, no. 1, pp. 45-50, 1997.
[45] H. Figueiredo, O. Saotome, Design of a Set of Reaction Wheels for Satellite Attitude Control Simulation, 22nd International Congress of Mechanical Engineering, Brazil, 2013.
[46] L. C. de Souza, V. M. Arena, Design of Satellite AttitudeControl Algorithm Based on the SDRE Method Using Gas Jets and Reaction Wheels, Journal of Engineering, vol. 2013, 2013.
[47] L. C. G. de Souza, Experimental Parameters Estimation of Satellite Attitude Control Simulator, Journal of Aerospace Engineering, vol. 1, no. 2, pp. 14, 2008.
[48] J. S. Young, Development of an automatic balancing system for a small satellite attitude control simulator, MSc. Thesis, Mechanical Engineering, Utah University, USA, 1998.
[49] A. Aghalari, S. A. Kalhor, M. M. Dehghan, S. H. Cheheltani, Manufacturing and Test of an Attitude Dynamics Simulator for Microsatellites Based on CMG, Journal of Aerospace Science and Technology, vol. 7, no. 3, pp. 51-67, 2013 (In Persian فارسی).
[50] D. S. Bernstein, N. H. McClamroch, A. Bloch, Development of air spindle and triaxial air bearing testbeds for spacecraft dynamics and control experiments, Proceedings of the American Control Conference, USA, 2001.
[51] S. Cho, J. Shen, N. McClamroch, D. Bernstein, Equations of motion for the triaxial attitude control testbed, Proceedings of the 40th IEEE Conference on Decision and Control, USA, 2001.
[52] S. Cho, N. H. McClamroch, Feedback control of triaxial attitude control testbed actuated by two proof mass devices, Proceedings of the Conference on Decision and Control, USA, 2002.
[53] D. B. French, Hybrid control strategies for rapid, large angle satellite slew maneuvers, M. Sc. Thesis, Department of Aeronautical and Astronautical Engineering, Air Force Institute of Technology, USA, 2003.
[54] V. J. Dabrowski, Experimental demonstration of an algorithm to detect the presence of a parasitic satellite, MSc. Thesis, Department of Aeronautics and Astronautics, Air Force Institute of Technology, USA, 2003.
[55] P. Wang, J. Yee, F. Hadaegh, Synchronized rotation of multiple autonomous spacecraft with rule-based controls: experimental study, Journal of Guidance, Control, and Dynamics, vol. 24, no. 2, pp. 352-359, 2001.
[56] J. J. Kim, B. N. Agrawal, Automatic mass balancing of air-bearing-based three-axis rotational spacecraft simulator, Journal of Guidance, Control, and Dynamics, vol. 32, no. 3, pp. 1005-1017, 2009.
[57] R. Bevilacqua, A. Caprari, J. Hall, M. Romano, Laboratory Experimentation of Multiple Spacecraft Autonomous Assembly, AIAA Guidance, Navigation and Control Conference and Exhibit, USA, 2009.
[58] J. S. Hall, Design and integration of a three degrees-of-freedom robotic vehicle with control moment gyro for the Autonomous Multiagent Physically Interacting Spacecraft (AMPHIS) testbed, M. Sc. Thesis, Astronautical Engineering Faculty, Naval Postgraduate School, USA, 2006.
[59] W. D. Price, Control system of a three dof spacecraft simulator by vectorable thrusters and control moment gyros, MSc. Thesis, Astronautical Engineering Faculty, Naval Postgraduate School, USA, 2006.
[60] D. M. Cho, D. Jung, P. Tsiotras, A 5-dof Experimental Platform for Autonomous Spacecraft Rendezvous & Docking, Proceedings of AIAA Infotech@ Aerospace Conference, USA, 2009.
[61] K. Saulnier, D. Pérez, G. Tilton, D. Gallardo, C. Shake, R. Huang, R. Bevilacqua, Operational Capabilities of a Six Degrees of Freedom Spacecraft Simulator, AIAA Guidance, Navigation, and Control (GNC) Conference, USA, 2013.
[62] K. Saulnier, D. Pérez, R. Huang, D. Gallardo, G. Tilton, R. Bevilacqua, A six-degree-of-freedom hardware-in-the-loop simulator for small spacecraft, Acta Astronautica, Vol. 105, No. 2, pp. 444-462, 2014.
[63] K. Omagari, T. Usuda, S. Matunaga, Research of controlmomentum gyros for micro-satellites and 3-DOF attitude dynamics simulator experiments, Proceedings of the Int’l Symposium on Artificial Intelligence, Robotics and Automation in Space, Germany, 2005.
[64] W. Whitacre, An autonomous underwater vehicle as aspacecraft attitude control simulator, 43rd AIAA Aerospace Sciences Meeting and Exhibit, USA, 2005.
[65] F. Aghili, M. Namvar, G. Vukovich, Satellite simulator with a hydraulic manipulator, Proceedings of IEEE International Conference on Robotics and Automation, USA, 2006.
[66] T. Boge, O. Ma, using advanced industrial robotics for spacecraft rendezvous and docking simulation, Proceedings of IEEE International Conference on Robotics and Automation, China, 2011.
[67] O. Ma, K. Ruble, R. Tessier, E. Krecher, A New Technology for Physically Simulating 3D Free Floating and Rotating of an Object in Zero-Gravity Environment, AIAA Modeling and Simulation Technologies (MST) Conference, USA, 2013.