[1] Conley, P.L., Space Vehicle Mechanisms: Elements of Successful Design, John Wiley & Sons, New York, USA, 1998.
[2] Jones, P.A. and Spence, B.R., "Spacecraft Solar Array Technology Trends", IEEE Aerospace and Electronic Systems Magazine, Vol. 26, pp. 17-28, 2011.
[3] Fowler, R., Howell, L., and Magleby, S., "Compliant Space Mechanisms: A New Frontier for Compliant Mechanisms", Mech. Sci, Vol. 2, pp. 205-215, 2011.
[4] Wertz, J.R., Spacecraft Attitude Determination and Control, Springer Science&Business Media, Vol. 73, 2012.
[5] Sarafin, T.P. and Larson, W.J., Spacecraft Structures and Mechanisms-From Concept To Launch, Springer, Netherlands, 1995.
[6] Kanji, S., Mechanical Aspects of Design, Analysis, and Testing for the NORSAT-1 Microsatellite, (M.Sc. Thesis), University of Toronto, 2015.
[7] Stevens, C. L., Design, Analysis, Fabrication, and Testing of a Nanosatellite Structure, (M.Sc. Thesis), Virginia Polytechnic Institute and State University, 2002.
[8] Morozov, E. and Lopatin, A., "Design and Analysis of the Composite Lattice Frame of a Spacecraft Solar Array", Composite Structures, Vol. 93, pp. 1640-1648, 2011.
[9] Zhang, L.X., Bai, Z.F., Zhao, Y., and Cao, X.B., "Dynamic Response of Solar Panel Deployment on Spacecraft System Considering Joint Clearance", Acta Astronautica, Vol. 81, pp. 174-185, 2012.
[10] Pellegrino, S., Kukathasan, S., Tibert, G., and Watt, A., Small Satellite Deployment Mechanisms, Department of Engineering, University of Cambridge, 2000.
[11] Cadogan D.P. and Grahne, M.S., "Deployment Control Mechanisms for Inflatable Space Structures", The 33rd Aerospace Mechanisms Conference, Pasadena: NASA, pp. 1-12, 1999.
[12] Katsumata, M., Natori,
M.C., and Yamakawa, H. "Analysis of Dynamic Behaviour of Inflatable Booms in Zigzag and Modified Zigzag Folding Patterns",
Acta Astron.
, Vol. 93, pp. 45-54, 2014.
[13] Szyszkowski, W. and, Glockner, P.,"Inflatable Booms And Pneumatic Hinges: An Application In Deployment of Satellite Sensors", Engineering Structures, Vol. 13, pp. 357-365, 1991.
[14] Freeland, R., Bilyeu, G., Veal, G., and Mikulas, M.,"Inflatable Deployable Space Structures Technology Summary", IAF-98-I.5.01 presented at 49th Congress of the International Astronautical Federation, Melbourne, Australia, Sept. 28-Oct. 2, 1998.
[15] Cassapakis C. and Thomas, M., "Inflatable Structures Technology Development Overview", in Space Programs and Technologies Conference, pp. 3738, Huntsville, AL, USA 1995.
[16] Herzl, G.G., Tubular Spacecraft Booms: Extendible, Reel Stored: Lockheed Missiles & Space Company, 1970.
[17] Meyers, S. and Sturm, J., "Development of a Strain Energy Deployable Boom for the Space Technology, 5 Mission", Proceedings of the 37th Aerospace Mechanisms Symposium, Johnson Space Center, May 19-21, 2004.
[18] Thomson, M., "AstroMesh™ Deployable Reflectors For Ku And Ka Band Commercial Satellites", The 20th AIAA International Communication Satellite Systems Conference and Exhibit., pp. 2032, 2002.
[19] Hoyt, R.P., "Spiderfab: An Architecture for Self-Fabricating Space Systems", in AIAA Space 2013 Conference and Exposition, pp. 5509, 2013.
[20] Christian, J., Jayaram, S., and Swartwout, M., "Feasibility of A Deployable Boom Aboard Picosatellites for Instrumentation and Control Purposes", in 2012 IEEE Aerospace Conference, , pp. 1-9, 2012.
[21] Straubel, M., Block, J., Sinapius, M., and Hühne, C., "Deployable Composite Booms for Various Gossamer Space Structures", in 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 19th AIAA/ASME/AHS Adaptive Structures Conference 13th, pp. 2023, 2011.
[22] Miyazaki, H.I.Y., Kodama, T., Uchiki, M., and Hinuma, S.,"AIAA/USU annual Conference on Small Satellite," 15th utah university, Logan, 2001.
[23] Lake, M.S., Peterson, L.D., Mikulas, M.M., Hinkle, J.D., Hardaway, L.R., and Heald, J., "Structural Concepts and Mechanics Issues for Ultra-Large Optical Systems," The 1999 Ultra Lightweight Space Optics Workshop, 1999.
[24] Tibert, G., "Deployable Tensegrity Structures for Space Applications", (Ph.D. Thesis) Kungliga Tekniska H¨ogskolan, Stockholm, Sweden, 2002.
[25] Mikulas, M.M., "State-Of-The-Art and Technology Needs for Large Space Structures," ASME Monograph on Flight-Vehicle Materials, Structures, and Dynamics Technologies, 1993.
[26] Chandra, A., "Inflatable Parabolic Reflectors for Small Satellite Communication", (M.Sc. Thesis), Arizona State University, USA, 2015.
[27] Guan, F.L., Shou, J.J., Hou, G.Y., and Zhang, J.J., "Static Analysis of Synchronism Deployable Antenna", Journal of Zhejiang University-SCIENCE A, Vol. 7, pp. 1365-1371, 2006.
[28] Onoda, J., "Two-dimensional Deployable Truss Structures for Space Applications", Journal of Spacecraft and Rockets, Vol. 25, pp. 109-116, 1988.
[29] You, Z., "Deployable structure of Curved Profile for Space Antennas", Journal of Aerospace Engineering, Vol. 13, pp. 139-143, 2000.
[30] Barrett, R., Taylor, R., Keller, P., Codell, D., and Adams, L., "Deployable Reflectors for Small Satellites", 21th Annual Conf. Smart Satellites, Logan. UT, 2007.
[31] Kiper, G., Söylemez, E., and Kişisel, A. Ö., "A Family of Deployable Polygons and Polyhedra", Mechanism and Machine Theory, Vol. 43, pp. 627-640, 2008.
[32] You, Z., "Motion Structures Extend Their Reach", Materials Today, Vol. 10, pp. 52-57, 2007.
[33] Hedgepeth, J.M., "Structures for Remotely Deployable Precision Antennas", NASA Contractor Report 182065, 1989.
[34] Freeland, R., Bilyeu, G. and Veal, G. , "Validation of A Unique Concept for A Low-Cost, Lightweight Space-Deployable Antenna Structure", Acta Astronautica, Vol. 35, pp. 565-572, 1995.
[36] Vyvyan, W.W., "Self-Actuating, Self-Locking Hinge," ed: Google Patents, 1968.
[37] Greenbelt, S.C.M.,"AIAA/USU Annual Conference On Small satellite", 10th Utah state University, Logan., 1996.
[38] Nagaraj, B., Nataraju, B., and Ghosal, A., "Dynamics of A Two-Link Flexible System Undergoing Locking: Mathematical Modelling and Comparison with Experiments", Journal of sound and vibration, Vol. 207, pp. 567-589, 1997.
[39] Bieler, T., "Handbuch Der Raumfahrttechnik", Aufl., Munich: Hanser, S. 238, 2008.
[40] Pellegrino, S., "Large Retractable Appendages in Spacecraft", Journal of Spacecraft and Rockets, Vol. 32, pp. 1006-1014, 1995.
[41] Wiegand, M., and Konigsmann, H., "A Small Re-Entry Capsule-BREM-SAT 2," 10th AIAA/USU Small Satellite Conference, Logan., Volume 1, 1996.
[42] Miyashita, N. and et al., "Development Of Nano-Satellite Cute-1.7+ APD And Its Current Status," in 56th International Astronautical Congress, Fukuoka, pp. 17-21, 2005.
[43] Nagaraj, B., Pandiyan, R., and Ghosal, A., "Kinematics of Pantograph Masts," Mechanism and Machine Theory, Vol. 44, pp. 822-834, 2009.
[44] Stoeckle, W.D.I.S., "Satellite Solar Generator Panel Deployment Device," Patent: DE19610297 (C1), 1997.
[45] M. L. u. a., "AIAA/USU annual conference on small satellite", 10th Utah state University, Logan., 1996.
[46] Zimmerman, W. H.,"Servomechanisms Responsive to A Heat Source," Patent: US3311322A, 1967-03-28
[47] http://spaceflight101.com/insight/insight-spacecraft/.
[48] Yu, W., Ang, L., Guan, X., and Zhang, Z., "Application of MSC Adams/View Technology in Spacecraft Solar Array Dynamic Analysis," Computer Aided Engineering, p. S1, 2006.
[49] https: //space.skyrocket.de/ doc_sdat/gals-1.htm.
[50] Plaza, J.M.E., Vilán Vilán, J.A., Agelet, F.A., Mancheño, J.B., Estévez, M.L., Fernández, C.M., and Ares, F.S., "Xatcobeo: Small Mechanisms for CubeSat Satellites-Antenna and Solar Array Deployment", Proceedings of the 40th Aerospace Mechanisms Symposium, NASA Kennedy Space Center, May 12-14, 2010.
[51] Fong, C.J., Yen, N.L., and Chi, S., "Space-Based Global Weather Monitoring System: FORMOSAT-3/COSMIC Constellation and Its Follow-On Mission," Journal of Spacecraft and Rockets, Vol. 46, pp. 883-891, 2009.
[52] Sugawara, Y. and et al., "A satellite for Demonstration of Panel Extension Satellite (PETSAT)," Acta Astronautica, Vol. 63, pp. 228-237, 2008.
)
