##[1] D. Kamran, A. Maziar, and S. Hossein, "FARAGAM algorithm in satellite layout," in Proceedings of the Sixth Asia-Pacific Conference on Multilateral Cooperation in Space Technology and Applications, Beijing, 2001, pp. 120-127.##
##[2] J. Cagan, K. Shimada, and S. Yin, "A survey of computational approaches to three-dimensional layout problems," Computer-Aided Design, vol. 34, no. 8, pp. 597-611, 2002.##
##[3] Z. Sun, H. Teng, and Z. Liu, "Several key problems in automatic layout design of spacecraft modules," Progress In Natural Science, vol. 13, no. 11, pp. 801-808, 2003.##
##[4] M. O. Kahraman, E. D. Swenson, and J. T. Black, "A constraint based approach for building operationally responsive space satellites," in 2009 4th International Conference on Recent Advances in Space Technologies, 2009, pp. 506-511: IEEE.##
##[5] m. fakoor, "Review of method for optimal layout of satellite components," (in eng), Modares Mechanical Engineering, vol. 13, no. 9, pp. 126-137, 2013.##
##[6] M. Fakoor, S. M. N. Ghoreishi, and H. Sabaghzadeh, "Spacecraft component adaptive layout environment (SCALE): an efficient optimization tool," Advances in Space Research, vol. 58, no. 9, pp. 1654-1670, 2016.##
##[7] Z.-G. Sun and H.-F. Teng, "Optimal layout design of a satellite module," Engineering optimization, vol. 35, no. 5, pp. 513-529, 2003.##
##[8] B. Zhang, H.-F. Teng, and Y.-J. Shi, "Layout optimization of satellite module using soft computing techniques," Applied Soft Computing, vol. 8, no. 1, pp. 507-521, 2008.##
##[9] H.-f. Teng, S.-l. Sun, D.-q. Liu, and Y.-z. Li, "Layout optimization for the objects located within a rotating vessel—a three-dimensional packing problem with behavioral constraints," Computers & Operations Research, vol. 28, no. 6, pp. 521-535, 2001.##
##[10] J.-Z. Huo and H.-F. Teng, "Optimal layout design of a satellite module using a coevolutionary method with heuristic rules," Journal of Aerospace Engineering, vol. 22, no. 2, pp. 101-111, 2009.##
##[11] A. Salehi, M. Fakoor, A. Kosari, and S. M. N. Ghoreishi, "Conceptual Design Process for LEO Satellite Constellations Based on System Engineering Disciplines," CMES-COMPUTER MODELING IN ENGINEERING & SCIENCES, vol. 131, no. 2, pp. 599-618, 2022.##
##]12[ م. باقر بهرامی، "طراحی بهینه سازه یک میکروماهواره با قیود ارتعاشی"، علوم، فناوری و کاربردهای فضایی، جلد 1، شماره 1، صفحات 80-65، 1400.##
## [13] T. P. Sarafin and W. J. Larson, "Spacecraft structures and mechanisms: from concept to launch," 1995.##
##[14] W. J. Larson and J. Wertz, "Space Mission Analysis and Design, Space Technology Library," Published jointly by Microcosm Press and Kluwer Academic Publishers, 2005.##
##[15] M. Aliha, S. Ghoreishi, D. Imani, Y. Fotoohi, and F. Berto, "Mechanical and fracture properties of aluminium cylinders manufactured by orbital friction stir welding," Fatigue & Fracture of Engineering Materials & Structures, vol. 43, no. 7, pp. 1514-1528, 2020.##
##[16] J. Guo, J. Zhang, Y. Feng, F. Wang, and C. Li, "Lightweight implementation of natural vibration frequency adjustment of satellite structures by varying the structural stiffness," Aerospace Science and Technology, vol. 118, p. 107061, 2021.##
##[17] A. Boudjemai, M. Bouanane, L. Merad, and A. S. Mohammed, "Small satellite structural optimisation using genetic algorithm approach," in 2007 3rd International Conference on Recent Advances in Space Technologies, 2007, pp. 398-406: IEEE.##
##[18] A. Aborehab, M. Kassem, A. Nemnem, M. Kamel, and H. Kamel, "Configuration design and modeling of an efficient small satellite structure," Engineering Solid Mechanics, vol. 8, no. 1, pp. 7-20, 2020.##
##[19] M. Safarabadi, H. Haghshenas, and H. Kelardeh, "Design of micro-vibration isolation system for a remote-sensing satellite payload using viscoelastic Materials," Engineering Solid Mechanics, vol. 8, no. 1, pp. 69-76, 2020.##
##]20[ م. صفرآبادی، ح. امامی، "بررسی میزان اعتبار به روز کردن مدل اجزا محدود سازه یک ماهواره میکرو با استفاده از نتایج آزمون ارتعاشات اتفاقی"، هفتمین همایش انجمن هوافضای ایران، تهران، 1386.##
##[21] H. Emami, F. Farhani, and M. Safarabadi, "Influence of modal effective mass distribution on the static and dynamic behavior of a satellite structure under base excitations," Material Science Research of India, vol. 5, no. 2, pp. 209-218, 2008.##
##[22] M. R. Roosta and M. Safarabadi, "Study of mass reduction possibility of a cubic microsatellite by replacing isogrid structure with sandwich panel structure using finite element analysis," Modares Mechanical Engineering, vol. 16, no. 9, pp. 241-248, 2016.##
##[23] M. R. Roosta and M. Safarabadi, " Investigation of a micro satellite structural properties on its effective vibration modes," 5th International Conference on Acoustics and Vibration, 2015.##
##]24[ ح. امامی، م. صفرآبادی، "بررسی تاثیر هندسه و صلبیت صفحات جانبی یک ماهواره مکعبی در رفتار سازه تحت بارگذاری دینامیک حاصل از شرایط محیطی پرتاب"، ششمین کنفرانس سراسری انجمن هوافضای ایران، دانشگاه صنعتی خواجه نصیرالدین طوسی، 1385.##
##]25[ م. صفرآبادی، ح. امامی، "تاثیر نحوه توزیع جرم موثر مودهای ارتعاشی و رفتار محلی صفحات جانبی یک ماهواره مکعبی در طراحی سازه تحت بارگذاری دینامیک حاصل از شرایط محیطی پرتاب"، پانزدهمین کنفرانس سالانه مهندسی مکانیک، دانشگاه صنعتی امیرکبیر، 1386.##
[26] ##Testing, ECSS-E-ST-10-03C, 2022.##
[27] ## A. Arianespace, "User's Manual (Issue 2-Revision 0)," E. Perez (Ed.), 2012.##
[28] ##M. Safarabadi and S. Bazargan, "Prediction of equivalent static loads act on a micro satellite via modal analysis," Engineering Solid Mechanics, vol. 3, no. 2, pp. 75-84, 2015.##
)