[1] GLASER P E. Power from the sun:Its future[J]. Science, 1968, 162(3856):857-861.[2] MANKINS J, KAYA N, VASILE M. SPS-ALPHA:The first practical solar power satellite via arbitrarily large phased array:AIAA-2012-3978[R]. Reston, VA:AIAA, 2012.[3] SASAKI S, TANAKA K, HIGUCHI K, et al. A new concept of solar power satellite:Tethered-SPS[J]. Acta Astronautica, 2007, 60(3):153-165.[4] SEBOLDT W, KLIMKE M, LEIPOLD M, et al. European sail tower SPS concept[J]. Acta Astronautica, 2001, 48(5):785-792.[5] 侯欣宾, 王立, 张兴华, 等. 多旋转关节空间太阳能电站概念方案设计[J]. 宇航学报, 2015, 36(11):1332-1338. HOU X B, WANG L, ZHANG X H, et al. Concept design on multi-rotary joints SPS[J]. Journal of Astronautics, 2015, 36(11):1332-1338(in Chinese).[6] YANG Y, ZHANG Y Q, DUAN B Y, et al. A novel design project for space solar power station (SSPS-OMEGA)[J]. Acta Astronautica, 2016, 121:51-58.[7] 王立, 侯欣宾. 空间太阳能电站的关键技术及发展建议[J]. 航天器环境工程, 2014, 31(4):343-350. WANG L, HOU X B. Key technologies and some suggestions for the development of space solar power station[J]. Spacecraft Environment Engineering, 2014, 31(4):343-350(in Chinese).[8] GRAF O F, Jr. Orbital motion of the solar power satellite:NASA-CP-151603[R]. Washington, D.C.:NASA, 1978.[9] MCNALLY I, SCHEERES D, RADICE G. Locating large solar power satellites in the geosynchronous Laplace plane[J]. Journal of Guidance, Control, and Dynamics, 2015, 38(3):489-505.[10] 刘玉亮, 邬树楠, 吴志刚, 等. 空间太阳能电站地球同步拉普拉斯轨道动力学特性[J]. 中国空间科学技术, 2016, 36(5):1-8. LIU Y L, WU S N, WU Z G, et al. Dynamic characteristics of geosynchronous Laplace orbit for space solar power station[J]. Chinese Space Science and Technology, 2016, 36(5):1-8(in Chinese).[11] MCNALLY I, SCHEERES D, RADICE G. Attitude dynamics of large geosynchronous solar power satellites[C]//AIAA/AAS Astrodynamics Specialist Conference. Reston, VA:AIAA, 2014:1-13.[12] WIE B, ROITHMAYR C M. Attitude and orbit control of a very large geostationary solar power satellite[J]. Journal of Guidance, Control, and Dynamics, 2005, 28(3):439-451.[13] ISHIMURA K, NATORI M, WADA M. Stability analysis and decentralized system design of large space structures based on potential field[C]//13th International Conferenc on Adaptive Structures and Technologies. Boca Raton, FL:CRC Press, 2003:413-422.[14] ISHIMURA K, HIGUCHI K. Coupling between structural deformation and attitude motion of large planar space structures suspended by multi-tethers[J]. Acta Astronautica, 2007, 60(8):691-710.[15] GLAESE J R, MCDONALD E J. Space solar power multi-body dynamics and controls, concepts for the integrated symmetrical concentrator configuration:TCD20000222A[R]. Washington, D.C.:NASA, 2000.[16] 周荻, 范继祥. 绳系太阳能发电卫星姿态机动的主动振动控制[J]. 宇航学报, 2012, 33(5):605-611. ZHOU D, FAN J X. Boundary control in the attitude maneuvering of tethered space solar power satellite[J]. Journal of Astronautics, 2012, 33(5):605-611(in Chinese).[17] 魏乙, 邓子辰, 李庆军, 等. 绳系空间太阳能电站动力学响应分析[J]. 宇航学报, 2016, 37(9):1041-1048. WEI Y, DENG Z C, LI Q J, et al. Analysis of dynamic response of tethered space solar power station[J]. Journal of Astronautics, 2016, 37(9):1041-1048(in Chinese).[18] DUBOSHIN G N. The differential equations of translational-rotational motion of mutally attracting rigid bodies[J]. Soviet Astronomy, 1958, 2:239-250.[19] LANGE B. Linear coupling between orbital and attitude motions of a rigid body[J]. Journal of the Astronautical Sciences, 1970, 18:150-167.[20] SINCARSIN G B, HUGHES P C. Gravitational orbit-attitude coupling for very large spacecraft[J]. Celestial Mechanics, 1983, 31(2):143-161.[21] ASHENBERG J. Mutual gravitational potential and torque of solid bodies via inertia integrals[J]. Celestial Mechanics and Dynamical Astronomy, 2007, 99(2):149-159.[22] WANG Y, XU S. Gravitational orbit-rotation coupling of a rigid satellite around a spheroid planet[J]. Journal of Aerospace Engineering, 2012, 27(1):140-150.[23] 吴志刚, 刘玉亮, 张开明, 等. 高阶重力和力矩对空间太阳能电站运动的影响[J]. 空间控制技术与应用, 2016, 42(4):1-5. WU Z G, LIU Y L, ZHANG K M, et al. The influences of higher order gravitational force and torque to the motion of space solar power station[J]. Aerospace Control and Application, 2016, 42(4):1-5(in Chinese).[24] LIU Y L, WU S N, ZHANG K G, et al. Gravitational orbit-attitude coupling dynamics of a large solar power satellite[J]. Aerospace Science and Technology, 2017, 62:46-54.[25] 刘暾, 赵钧. 空间飞行器动力学[M]. 哈尔滨:哈尔滨工业大学出版社, 2003:153-154. LIU D, ZHAO J. Dynamics of spacecraft[M]. Harbin:Harbin Institute of Technology Press, 2003:153-154(in Chinese).[26] ASHLEY H. Observations on the dynamic behavior of large flexible bodies in orbit[J]. AIAA Journal, 1967, 5(3):460-469.[27] BAINUM P M, KUMAR V K, JAMES P K. The dynamics and control of large flexible space structures, Part B:Development of continuum model and computer simulation:NASA-CR-l63612[R]. Washington,D.C.:NASA, 1978.[28] KANE T R, RYAN R, BANERJEE A K. Dynamics of a cantilever beam attached to a moving base[J]. Journal of Guidance, Control, and Dynamics, 1987, 10(2):139-151.[29] 杨辉, 洪嘉振, 余征跃. 两种刚柔耦合动力学模型的对比研究[J]. 上海交通大学学报, 2002, 36(11):1591-1595. YANG H, HONG J Z, YU Z Y. Study on two dynamic models for a rigid-flexible coupling system[J]. Journal of Shanghai Jiaotong University, 2002, 36(11):1591-1595(in Chinese).[30] ASHLEY H. Observations on the dynamic behavior of large flexible bodies in orbit[J]. AIAA Journal, 1967, 5(3):460-469.
CJA