星载激光通信端机可重复锁紧/解锁机构设计
[1] 刘志全.航天器机构及其可靠性[M].北京: 中国宇航出版社,2012.
LIU ZH Q. Spacecraft Institutions and Their Reliability [M]. Beijing: China Aerospace Press, 2012. (in Chinese)
[2] 姜会林, 安岩, 张雅琳, 等. 空间激光通信现状、发展趋势及关键技术分析[J]. 飞行器测控学报, 2015, 34(3): 207-217.
JIANG H L, AN Y, ZHANG Y L, et al.. Analysis of the status quo, development trend and key technologies of space laser communication[J]. Journal of Spacecraft TT&C Technology, 2015, 34(3): 207-217. (in Chinese)
[3] 王忠素, 吴清文, 郭权峰, 等. 空间光学载荷探测器组件抗冲击隔振设计[J]. 光学 精密工程, 2017, 25(8): 2098-2105.
[4] 王书新, 李景林, 齐光, 等. 空间相机用爆炸螺栓防护装置[J]. 光学 精密工程, 2014, 22(12): 3318-3323.
[5] 宣明, 张道威, 谷松, 等. 微小卫星太阳帆板压紧释放机构的设计[J]. 光学 精密工程, 2017, 25(4): 447-454.
XUAN M, ZHANG D W, GU S, et al.. Design of hold-down and release mechanism for solar panel of micro-satellite[J]. Opt. Precision Eng., 2017, 25(4): 447-454. (in Chinese)
[6] 张佼龙, 周军. 立方星星箭分离机构运动系统的设计与验证[J]. 光学 精密工程, 2017, 25(4): 387-395.
ZHANG J L, ZHOU J. Design and verification of kinematic system in deploying mechanism for CubeSats[J]. Opt. Precision Eng., 2017, 25(4): 387-395. (in Chinese)
[7] 王玉鹏, 王凯, 贾瑞栋, 等. 精指向自解锁星载太阳指向器设计与应用[J]. 光学 精密工程, 2016, 24(1): 0065.
[8] ERIC D MILLERA, MICHAEL DESPENZAB, ILYA GAVRILYUKB, et al.. A prototype coarse pointing mechanism for laser communication[C]. Free-Space Laser Communication and Atmospheric Propagation XXIX. 2017
[9] 贺志荣, 周超, 刘琳, 等. 形状记忆合金及其应用研究进展[J]. 铸造技术, 2017, 38(2): 257-261.
HE Z R, ZHOU C, LIU L, et al.. Research progress of shape memory alloys and their applications[J]. Foundry Technology, 2017, 38(2): 257-261. (in Chinese)
[10] 张明德, 李雅格, 吴艳斌, 等. 形状记忆合金驱动器动态驱动性能研究[J]. 航空制造技术, 2017(17): 49-54.
ZHANG M D, LI Y G, WU Y B, et al.. Research on dynamic driving characteristic of shape memory alloy actuator[J]. Aeronautical Manufacturing Technology, 2017(17): 49-54. (in Chinese)
[11] 秦晓宇, 张小勇, 闫晓军, 等. 自锁式形状记忆合金馈源锁紧机构[J]. 宇航学报, 2016, 37(3): 357-363.
QIN X Y, ZHANG X Y, YAN X J, et al.. An SMA-actuated locking device for feed source structure based on self-locking principle[J]. Journal of Astronautics, 2016, 37(3): 357-363. (in Chinese)
[12] BUCKLEY S, FOSNESS E, GAMMILL W. Deployment and release devices efforts at the air force research laboratory space vehicles directorate[C]//AIAA Space 2001 Conference and Exposition, Albuquerque, NM, USA. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001.
[13] NAVA N, COLLADO M, CAB S R. REACT: resettable hold down and release actuator for space applications[J]. Journal of Materials Engineering and Performance, 2014, 23(7): 2704-2711.
[14] 王轩. 飞行环境下航天器结构的模态分析技术[D]. 上海: 复旦大学, 2008.
WANG X. Operational modal identification of spacecraft structures[D]. Shanghai: Fudan University, 2008. (in Chinese)
[15] 刘晨, 朱剑涛, 刘丽红, 等. 某平台卫星发射及在轨力学环境测量与分析[J]. 航天器环境工程, 2017, 34(3): 270-276.
LIU CH, ZHU J T, LIU L H, et al.. Dynamics parameter measurement and analysis of certain satellite platform during the launch and in orbit[J]. Spacecraft Environment Engineering, 2017, 34(3): 270-276. (in Chinese)
孟立新, 孟令臣, 李小明, 张家齐, 迟铁, 张立中. 星载激光通信端机可重复锁紧/解锁机构设计[J]. 光学 精密工程, 2019, 27(7): 1544. MENG Li-xin, MENG Ling-chen, LI Xiao-ming, ZHANG Jia-qi, CHI Tie, ZHANG Li-zhong. Design of repeatable locking/unlocking mechanism for spaceborne laser communication terminal[J]. Optics and Precision Engineering, 2019, 27(7): 1544.