[ 1 ] Duan B. The state-of-the-art and development trend of large space-borne deployable antenna. Electro Mech Eng 2017;33(1):1–14. Chinese. link1

[ 2 ] Deng ZQ. Design of space deployable and foldable mechanisms. Harbin: Harbin Institute of Technology Press; 2013. Chinese. link1

[ 3 ] Hu H, Tian Q, Zhang W, Jin D, Hu G, Song Y. Nonlinear dynamics and control of large deployable space structures composed of trusses and meshes. Adv Mech 2013;43(4):390–414. Chinese. link1

[ 4 ] Ma X, Li Y, Xiao Y, Zheng S, Huang Z, Feng T. Development and tendency of large space deployable antenna reflector. Space Electron Technol 2018;2:16–26. Chinese. link1

[ 5 ] Ma XF. Structure and mechanism of space mesh antenna. Beijing: China Machine Press; 2021. Chinese. link1

[ 6 ] Li P, Liu C, Tian Q, Hu H, Song Y. Dynamics of a deployable mesh reflector of satellite antenna: form-finding and modal analysis. J Comput Nonlinear Dynam 2016;11(4):041017. link1

[ 7 ] Xu Y, Guan FL. Structure–electronic synthesis design of deployable truss antenna. Aerosp Sci Technol 2013;26(1):259–67. link1

[ 8 ] Tang Y, Li T, Ma X. Pillow distortion analysis for a space mesh reflector antenna. AIAA J 2017;55(9):3206–13. link1

[ 9 ] Guo H, Shi C, Li M, Deng Z, Liu R. Design and dynamic equivalent modeling of double-layer hoop deployable antenna. Int J Aerosp Eng 2018;2018:1–15. link1

[10] Nie R, He B, Yan S, Ma X. Design optimization of mesh antennas for on-orbit thermal effects. Int J Mech Sci 2020;175:105547. link1

[11] Peng Y, Zhao Z, Zhou M, He J, Yang J, Xiao Y. Flexible multibody model and the dynamics of the deployment of mesh antennas. J Guid Control Dyn 2017;40(6): 1499–510. link1

[12] Du B, Wu Y, Zhang Y, Liu G. Overview of large reflector antenna technology. Radio Commun Technol 2016;42(1):1–8. Chinese. link1

[13] Li WJ, Cheng DY, Liu XG, Wang YB, Shi WH, Tang ZX, et al. On-orbit service (OOS) of spacecraft: a review of engineering developments. Prog Aerosp Sci 2019;108:32–120. link1

[14] Liu J, Fan Q, Deng T, Wang Y, Huang Q. Mechanical analysis and design of a light weight and high stiffness space manipulator. In: Proceedings of 2016 IEEE International Conference on Mechatronics and Automation; 2016 Aug 7–10; Harbin, China. IEEE; 2016. p. 1495–500.

[15] Ma X, Gao B, Li H, Liu F, Li T. Design and implementation of large space radio telescope antenna. Int J Comput Mater Sci Eng 2018;7(1–2):1850008. link1

[16] Wang M, Luo J, Fang J, Yuan J. Optimal trajectory planning of free-floating space manipulator using differential evolution algorithm. Adv Space Res 2018;61(6):1525–36. link1

[17] Meng D, She Y, Xu W, Lu W, Liang B. Dynamic modeling and vibration characteristics analysis of flexible-link and flexible-joint space manipulator. Multibody Syst Dyn 2018;43(4):321–47. link1

[18] Ma S, Liang B, Wang T. Dynamic analysis of a hyper-redundant space manipulator with a complex rope network. Aerosp Sci Technol 2020;100:105768. link1

[19] Ni Z, Liu J, Wu Z, Shen X. Identification of the state-space model and payload mass parameter of a flexible space manipulator using a recursive subspace tracking method. Chin J Aeronauti 2019;32(2):513–30. link1

[20] Li Y, Wang C, Huang W. Dynamics analysis of planar rigid-flexible coupling deployable solar array system with multiple revolute clearance joints. Mech Syst Signal Process 2019;117:188–209. link1

[21] Xu J, Fang H, Zhou T, Chen YH, Guo H, Zeng F. Optimal robust position control with input shaping for flexible solar array drive system: a fuzzy-set theoretic approach. IEEE Trans Fuzzy Syst 2019;27(9):1807–17. link1

[22] Lan X, Liu LW, Zhang FH, Liu ZX, Wang LL, Li QF, et al. World’s first spaceflight on-orbit demonstration of a flexible solar array system based on shape memory polymer composites. Sci China Technol Sci 2020;63(8):1436–51. link1

[23] Cao Y, Cao D, Wei J, Huang W. Modeling for solar array drive assembly system and compensating for the rotating speed fluctuation. Aerosp Sci Technol 2019;84:131–42. link1

[24] Zhu S, Li D, Lei Y. Disturbance mechanism of the solar array drive system on spacecraft. Mech Syst Signal Process 2022;165:108306. link1

[25] Song K, Ma B, Yang G, Jiang J, Wei R, Zhang H, et al. A rotation-lightweight wireless power transfer system for solar wing driving. IEEE Trans Power Electron 2019;34(9):8816–30. link1

[26] Wu M, Shi Z, Xiao T, Chen ZLJ, Ang H. Effect of solar cell efficiency and flight condition on optimal flight control and energy performance for Z-shaped wing stratospheric solar aircraft. Acta Astronaut 2019;164:366–75. link1

[27] Gong S, Macdonald M. Review on solar sail technology. Astrodynamics 2019;3(2): 93–125. link1

[28] Zeng X, Gong S, Li J, Alfriend KT. Solar sail body-fixed hovering over elongated asteroids. J Guid Control Dyn 2016;39(6):1223–31. link1

[29] Zhang J, Qi R, Jiang B. Modeling and analysis of flexible solar sail. In: Proceedings of 2018 IEEE CSAA Guidance, Navigation and Control Conference; 2018 Aug 10–12; Xiamen, China. IEEE; 2018. p. 1–6.

[30] Song Y, Gong S. Solar sail trajectory optimization of multi-asteroid rendezvous mission. Acta Astronaut 2019;157:111–22. link1

[31] Zhang J, Wu N, Tong A, Liu Y. Structural dynamic responses of a stripped solar sail subjected to solar radiation pressure. Chin J Aeronauti 2020;33(8): 2204–11. link1

[32] Zhang P, Li Y, Hu H. Modeling and simulation active vibration control of flexible solar wing support structure. In: Proceedings of 2019 5th International Conference on Energy Equipment Science and Engineering; 2019 Nov 29–Dec 1; Harbin, China. IOP Publishing; 2020. p. 012024.

[33] Zheng J, Gao H, Yuan B, Liu Z, Yu H, Ding L, et al. Design and terramechanics analysis of a Mars rover utilising active suspension. Mechanism Mach Theory 2018;128:125–49. link1

[34] Zhou B, Shen SX, Lu W, Li YX, Liu Q, Tang CJ, et al. The Mars rover subsurface penetrating radar onboard China’s Mars 2020 mission. Earth Planet Phys 2020;4(4):345–54. link1

[35] Du AM, Zhang Y, Li HY, Qiao DH, Yi Z, Zhang TL, et al. The Chinese mars rover fluxgate magnetometers. Space Sci Rev 2020;216(8):1–15. link1

[36] Li R, Di K, Howard AB, Matthies L, Wang J, Agarwal S. Rock modeling and matching for autonomous long-range Mars rover localization. J Field Robot 2007;24(3):187–203. link1

[37] Zhao W, Wang C. China’s lunar and deep space exploration: touching the moon and exploring the universe. Natl Sci Rev 2019;6(6):1274–8. link1

[38] Liang Z, Chen J, Wang Y. Equivalent acceleration imitation for single wheel of manned lunar rover by varying torque on earth. IEEE/ASME Trans Mechatron 2020;25(1):282–93. link1

[39] Jia Y, Zou Y, Xue C, Ping J, Yan J, Ning Y. Scientific objectives and payloads of Chang’e-4 mission. Chin J Space Sci 2018;38(1):118–30. Chinese. link1

[40] Zhang D, Liu L, Leng J, Liu Y. Ultra-light release device integrated with screenprinted heaters for CubeSat’s deployable solar arrays. Compos Struct 2020;232:111561. link1

[41] Zhang D, Liu L, Lan X, Leng J, Liu Y. Synchronous deployed design concept triggered by carbon fiber reinforced shape memory polymer composites. Compos Struct 2022;290:115513. link1

[42] Shi C, Guo H, Zhang S, Liu R, Deng Z. Configuration synthesis of linear foldable over-constrained deployable unit based on screw theory. Mechanism Mach Theory 2021;156:104163. link1

[43] Ding X, Yang Y, Dai JS. Design and kinematic analysis of a novel prism deployable mechanism. Mechanism Mach Theory 2013;63:35–49. link1

[44] Chen Y, Feng J, Liu Y. A group-theoretic approach to the mobility and kinematic of symmetric over-constrained structures. Mechanism Mach Theory 2016;105:91–107. link1

[45] Chen Y, You Z. Square deployable frames for space applications. Part 1: theory. Proc Inst Mech Eng 2006;220(4):347–54. link1

[46] Sareh P, Chermprayong P, Emmanuelli M, Nadeem H, Kovac M. A rotary origami protective system for robotic rotorcraft. Sci Robot 2018;3(22): eaah5228. link1

[47] Yang Y, Liu Li, Li J, Yang Y, Zhang T, Mao Y, et al. Featured services and performance of BDS-3. Sci Bull 2021;66(20):2135–43. link1

[48] Ye PJ, Sun ZZ, Zhang H, Li F. An overview of the mission and technical characteristics of Change’4 Lunar Probe. Sci China Technol Sci 2017;60(5): 658–67. link1

[49] Li X, Meng Q, Gu X, Jancso T, Yu T, Wang K, et al. A hybrid method combining pixel-based and object-oriented methods and its application in Hungary using Chinese HJ-1 satellite images. Int J Remote Sens 2013;34(13):4655–68. link1

[50] Liu Z, Wu Y, Ma J. Design and verification of high-stiffness solar wing on agile satellites. J Astronaut 2019;40(6):621–7. Chinese. link1

[51] Wu Z, Liu Z, Rong J, Wu Y, Xin P, Luo Q. Modal simulation and experimental research on circular solar arrays. J Astronaut 2020;41(12):1516–24. Chinese. link1

[52] Xin P, Liu Z, Rong J, Liu C, Wu Z, Liu B. Modeling and analysis of deployment dynamics for UltraFlex solar array. J Astronaut 2020;41(3):262–9. Chinese. link1

[53] Li F, Liu L, Lan X, Pan C, Liu Y, Leng J, et al. Ground and geostationary orbital qualification of a sunlight-stimulated substrate based on shape memory polymer composite. Smart Mater Struct 2019;28(7):075023. link1

[54] Pan Y, Wang C. Developing the planetary science research for the sustainable deep space exploration of China. Bull Natl Nat Sci Found China 2021;35(2): 181–5. Chinese. link1

[55] Wu W, Yu D, Huang J, Zong Q, Wang C, Yu G, et al. Exploring the solar system boundary. Sci Sin Inf 2019;49(1):1. link1

[56] Shen Z, Zhang W, Jia Y, Sun Z. System design and technical characteristics analysis of Chang’e-3 lunar rover. Spacecr Eng 2015;24(5):8–13. Chinese. link1

[57] Dang Z, Li H, Peng S, Wen B, Shen Z, Jia Y. System design and verification of Chang’e-4 rover. Spacecr Eng 2019;28(4):37–42. Chinese. link1

[58] Chen M, Ma JN. China’s five-star red flag flies proudly on red planet [Internet]. Beijing: China Daily; 2021 Jul 20 [cited 2021 Nov 21]. Available from: http:// english.www.gov.cn/news/topnews/202107/20/content_WS60f622b4c6d0df5 7f98dd427.html. link1

[59] China National Space Administration. The first scientific images of Tianwen-1 probe landing on Mars unveiled [Internet]. Beijing: CNSA; 2021 Jun 11 [cited 2021 Nov 21]. Available from: http://www.cnsa.gov.cn/n6758823/n6758838/ c6812123/content.html. Chinese. link1

[60] Li C, Angeles J, Guo H, Yan H, Tang D, Liu R, et al. Mobility and singularity analyses of a symmetric multi-loop mechanism for space applications. Proc Inst Mech Eng 2021;235(22):6205–18. link1

[61] Yang Y, Ding X. Kinematic analysis of a plane deployable mechanism assembled by four pyramid cells. J Aeronaut Astronaut 2010;31(6):1257–65. Chinese. link1

[62] Wei G, Chen Y, Dai JS. Synthesis, mobility, and multifurcation of deployable polyhedral mechanisms with radially reciprocating motion. J Mech Des 2014;136(9):091003. link1

[63] Chen Y, Feng J, Sun Q. Lower-order symmetric mechanism modes and bifurcation behavior of deployable bar structures with cyclic symmetry. Int J Solids Struct 2018;139–140:1–14. link1

[64] Agrawal P, Anderson M, Card M. Preliminary design of large reflectors with flat facets. IEEE Trans Antennas Propag 1981;29(4):688–94. link1

[65] Ma X, Li T. Surface reconstruction of deformable reflectors by combining Zernike polynomials with radio holography. AIAA J 2019;57(6): 2544–52. link1

[66] Wang Z, Li T, Ma X. Method for generating statically determinate cable net topology configurations of deployable mesh antennas. J Struct Eng 2015;141(7): 04014182. link1

[67] Tang Y, Li T. Equivalent-force density method as a shape-finding tool for cablemembrane structures. Eng Struct 2017;151:11–9. link1

[68] Ma XF, Li TJ. Dynamic analysis of uncertain structures using an interval-wave approach. Int J Appl Mech 2018;10(2):1850021. link1

[69] Ma XF, Li TJ, Wang ZW. Hybrid active wave/mode control of space prestressed taut cable net structures. Int J Appl Mech 2018;10(6):1850062. link1

[70] Tian Q, Liu C, Li P, Hu H. Advances and challenges in dynamics of flexible multibody systems. J Dyn Control 2017;15(5):385–405. Chinese. link1

[71] Zhou ZC, Dong FX. Multi-body dynamics analysis of large antennas in space. Beijing: China Astronautic Publishing House; 2014. Chinese. link1

[72] Ma XF, Yang JG, Hu JF, Zhang X, Xiao Y, Zhao ZH. Deployment dynamical numerical simulation on large elliptical truss antenna. Sci Sin Phys Mech Astron 2019;49(2):024516. link1

[73] Feng Y, Ma X, Li Y. Review of thermally-induced dynamic responses of large space structures. Space Electron Technol 2020;17(6):13–21. Chinese. link1

[74] Chen GH, Wang B, Hua Y, Zhang X, Zhao J, Zheng SK. The key technologies for radial rib deployable antenna of Chang’e-4 relay satellite. Sci Sin Technol 2019;49(2):166–74. Chinese. link1

[75] Lin F, Chen C, Zhou J, Dai Y. Hanger forces optimization of ground test device on deployable struct. Int J Space Struct 2021;36(2):127–36. link1

[76] Liu ZQ, Qiu H, Li X, Yang SL. Review of large spacecraft deployable membrane antenna structures. Chin J Mech Eng 2017;30(6):1447–59. link1

[77] Zhao Z, Fu K, Li M, Li J, Xiao Y. Gravity compensation system of mesh antennas for in-orbit prediction of deployment dynamics. Acta Astronaut 2020;167:1–13. link1

[78] Mihora DJ, Redmond PJ. Electrostatically formed antennas. J Spacecr Rockets 1980;17(5):465–73. link1

[79] Duan B, Zhang Y, Du J. Electrostatic forming membrane reflector antenna. In: Large deployable satellite antennas. Singapore: Springer; 2020. p. 241–71. link1