[1] Saghari, A, “Satellite Conceptual Design Algorithmsunder Uncertainty,” (Thesis M.Sc.) K. N. Toosi University of Technology, 2012, pp.17-87 (in persian).
[2] Gilmore, D.G., Spacecraft Thermal Control Handbook Volume I, 2nd ed., David G. Gilmore, Ed. Virginia, U.S.A, American Institute of Aeronautics and Astronautics, 2002, pp. 22-47.
[3] Wertzand, J.R. and Everett,D.F., Space Mission Engineering: The New SMAD, Microcosm Press, Hawthorne, CA, 2011, pp. 641-663.
[4] Taylor, E.R., Evaluation of Multidisciplinary Design Optimization Techniques as Applied to the Spacecraft Design Process, U.S.A, University of Colorado Department of Aerospace Engineering Sciences, 1999, pp.18-29.
[5] Saghari, S., Mirshams, M. and Jafarsalehi, A., “Comprehensive Algorithm and Code for Conceptual Design of an Earth Observation Satellite,” Journal of Space Science and Technology (JSST), Vol. 7, No. 2, Summer 2014, (in persia).
[6] Brown, C.B., Elements of Spacecraft Design, J. S. Przemlenleckl, Ed. Colorado, U.S.A, AIAA, 2002, pp. 315-369.
[7] Fortescue, P., Spacecraft Systems Engineering, 4th ed., Graham Swinerd,John Stark Peter Fortescue, Ed. UK, John Wiley & Sons, Ltd, 2011:351-355
[8] Anderson, B.J, Guidelins for the Selection of Near-Earth Thermal Environment Parameters for Spacecraft Design, NASA, 2001
[9] Rickman, S.L., A Simplified, Closed-Form Method for Screening Spacecraft Orbital Heating Variations, NASA-Lyndon B. Johnson Space Center, Houston, Texas, 2002.
[10] Jacques, L., Thermal Design of the Oufti-1nanosatellite, (Thesis M.Sc.), University of Liège, 2009, pp.1-37
Nejati, M.,
Particle Swarm Optimization (PSO), Research,
Isfahan University of Technology, May 2015.