[1] R. S. Maynard, Fluid Momentum Control, U.S. Patent, 4,776,541, 1998.
[2] B. J. Lurie, J. A. Schier, Liquid-ring attitude-control system for spacecraft, NASA Tech Briefs, Vol. 14, No. 9, 1990.
[3] D. R. Laughlin, H. R. Sebesta, D. E. Ckelkamp-Baker, A dual function magnetohydrodynamic (MHD) device for angular motion measurement and control, Advances in the Astronautical Science, Vol. 111, pp. 335-348, 2002.
[4] A. C. Kelly, C. Mc Chesney, P. Z. Smith, S. Waltena, A performance test of a fluidic momentum controller in three axes, NASA Report, 2004.
[5] K. D. Kumar, Satellite attitude stabilization using fluid rings, Acta Mechanica, Vol. 208, pp. 117-131, 2009.
[6] Sh. Xiao-wei, Ch. Xue-qin, G. Yan-hai, Zh. Shi-jie, Small satellite attitude control based on mechanically-pumped fluid loops, 6 th IEEE Conference on Industrial Electronics and Applications, Beijing, China, June 21-23, 2011.
[7] R. Varatharajoo, R. Kahle, S. Fasoulas, Approach for combining spacecraft attitude and thermal control systems, Journal of Spacecraft and Rocket, Vol. 40, No. 5, pp. 657-664, 2003.
[8] S. B. Alkhodari, R. Varatharajoo, H2 and H∞ control options for the combined attitude and thermal control system (CATCS), Journal of Advances in Space Research, Vol. 43, pp. 1897-1903, 2009.
[9] N. A. Nobari, A. K. Misra, Satellite attitude stabilization using four fluid rings in a pyramidal configuration, AIAA/AAS Astrodynamics Specialist Conference, Toronto, Canada, August 2-5, 2010.
[10] N. A. Nobari, A. K. Misra, Attitude Dynamics and Control of Satellite with Fluid Ring Actuators, PhD Thesis, Department of Mechanical Engineering, McGill University, Canada, 2013.
[11] N. A. Nobari, A. K. Misra, Attitude dynamics and control of satellites with fluid ring actuators, Journal of Guidance, Control and Dynamics, Vol. 35, No. 6, pp. 1855-1864, Nov-Dec 2012.
[12] J. Tayebi, A. Soleymani, A comparative study of CMG and FMC actuators for nano satellite attitude control system - pyramidal configuration, 7th International Conference on Recent Advances in Space Technologies (IEEE), Istanbul, Turkey, June 16-19, 2015.
[13] S. R. Vadali, Variable-structure control of spacecraft large-angle maneuvers, Journal of Guidance, Control and Dynamics, Vol. 9, No. 2, pp. 235-239, 1986.
[14] T. A. W. Dwyer, H. Sira-RBmirez, Variable-structure control of spacecraft attitude maneuvers, The Journal of Guidance, Control and Dynamics, Vol. 11, No. 3, pp. 262-270, 1988.
[15] R. D. Roeinett, G. G. Parker, Least squares sliding mode control tracking of spacecraft large angle maneuvers, The Journal of the Astronautical Sciences, Vol. 45, No. 4, pp. 433-450, 1997.
[16] J. L. Crassidis, S. R. Vadali, F. L. Markley, Optimal variable-structure control tracking of spacecraft maneuvers, Journal of Guidance, Control and Dynamics, Vol. 23, No. 3, pp. 564-566, 2000.
[17] C. Binglong, L. Xiangdong, C. Zhen, Exponential time-varying sliding mode control for large angle attitude eigenaxis maneuver of rigid spacecraft, Chinese Journal of Aeronautics, Vol. 23, pp. 447-453, 2010.
[18] R. L. Akau, V. L. Behr, R. Whitaker, Thermal design of the fast-on-orbit recording of transient events (FORTE) satellite, 8th Annual AIAA/USU Conference on Small Satellites, Utah State University, USA, 1994.
[19] N. Sozbir, M. Bulut, M.F. Oktem, A. Kahriman, A. Chaix, Design of thermal control subsystem for TUSAT telecommunication satellite, World academy of science, engineering and technology, International Journal of Electrical, Computer, Energetic, Electronic and Communication Engineering, Vol. 2, No. 7, pp. 1370-1373, 2008.
[20] G. Tsuyuki, D. Thunnissen, Margin determination in the design and development of a thermal control system, SAE Technical Paper, 2004-01- 2416, 2004.
[21] C. Struble, E. Bascaran, R.B. Bannerot, F. Mistree, Compromise: A multiobjective hierarchical approach to the design of spacecraft thermal control systems, ASME Computers in Engineering Conference, Anaheim, CA, USA, July 30-Augest 3, 1989.
[22] W. Cheng, N. LiuZhi, L. ZhongAiMing, W. ZhiMin, Z. ZongBo He, Application study of a correction method for a spacecraft thermal model with a monte-carlo hybrid algorithm, Chinese Science Bulletin, Vol. 56, No. 13, pp. 1407-1412, 2011.
[23] G. Charlotte, University nanosat system thermal design, analysis, and testing, SPIE Defense & Security Symposium, Orlando, Florida, USA, April 18-20, 2006.
[24] D. Roos, A. Diner, Thermal design analysis of a satellite with articulating solar panels, 1st Worldwide MSC Aerospace Users' Conference, Long Beach, CA, USA, June 7–10, 1999.
[25] K. Daryabeigi, Thermal analysis and design optimization of multilayer insulation for reentry aerodynamic heating, Journal of Spacecraft and Rockets, Vol. 39, No. 4, pp. 509-514, 2002.
[26] A. Corey Bolduc Chahe, Rapid thermal analysis of rigid three-dimensional bodies with the use of modelica physical modelling language, MSDL 2009 Summer Presentations for Canadian Space Agency, Department of Space Technologies, Quebec, Canada, 2009.
[27] A. Corey Bolduc Chahé, Rapid Thermal Analysis of Rigid ThreeDimensional Bodies with the Use of Modelica Physical Modelling Language, PhD Thesis, McConnell University, USA, 2009.
[28] G. Jose, G. Fernandez-Rico, Linear approach to the orbiting spacecraft thermal problem, Journal of Thermophysics and Heat Transfer, Vol. 26, No. 3, pp. 511-522, 2012.
[29] V. Chandrasekaran, E. R. Subramanian, Transient thermal analysis of a nanosatellite in low earth orbit, Proceedings of The Eighth International Conference on Engineering Computational Technology, Civil-Comp Press, Stirlingshire, UK, September 4-7, 2012.
[30] R. Katarzyna, K. Dariusz, Fuzzy TOPSIS method with ordered fuzzy numbers for flow control in a manufacturing system, Journal Applied Soft Computing, Vol. 52, Issue C, pp. 1020-1041, 2016.
[31] M. Sabaghi, M. Christian, Application of DOE-TOPSIS technique in decision-making problems, IFAC-Papers Online, Vol. 48, No. 3, pp. 773– 777, 2015.
[32] A. Hatami-Marbini, F. Kangi, An extension of fuzzy TOPSIS for a group decision making with an application to Tehran stock exchange, Applied Soft Computing, Vol. 52, pp. 1084-1097, 2016.
[33] G. T. Tumer, A novel multi attribute decision making approach for location decision under high uncertainty, Applied Soft Computing, Vol. 40, pp. 674- 682, 2016.
[34]B. Wie, Space Vehicle Dynamics and Control, pp. 180-196, Reston, Virginia, AIAA Education Series (AIAA Publisher), 1998.