| Citation: |
Gao Zhijie, Sun Fuchun, Min Haibo, Wang Shixing. STUDY ON ATTITUDE DISTURBANCE AND CONTROL OF MOTHER SATELLITE DURING SPACE NET PROJECTING[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(3): 434-441. DOI: 10.6052/0459-1879-12-249
|
|
Nakasuka S, Aoki T, Ikeda I, et al. "Furoshiki Satellite"——A large membrane structure as a novel space system. Acta Astronautica, 2001, 48(5-12): 461-468
|
|
Nakasuka S, Funase R, Nakada K, et al. Large membrane "Furoshiki Satellite" applied to phased array antenna and its sounding rocket experiment. Acta Astronautica, 2006, 58(8): 395-400
|
|
Nakasuka S, Funane T, Nakamura Y, et al. Sounding rocket flight experiment for demonstrating "Furoshiki Satellite" for large phased array antenna. Acta Astronautica, 2006, 59(1-5): 200-205
|
|
于绍华.航天飞行器相对运动动力学及其控制方法.宇航学报, 1995, 16(3): 1-7 (Yu Shaohua. The dynamics and control of spacecraft of relative motion. Journal of Astronautics, 1995, 16(3): 1-7 (in Chinese))
|
|
Mankala KK, Agrawal SK. Dynamic modeling and simulation of impact in tether net gripper systems. Mulitbody System Dynamics, 2003, 11(3): 235-250
|
|
Sorensen J, Kirk F. Conceptual design and analysis of an MXER tether boost station. In: Proceedings of Joint Propulsion Conference and Exhibit, 37th, Salt Lake City, UT, July 8-11, 2001, 391-402
|
|
Westerhoff J. Optimal configuration of MXER tether systems. In: Proceedings of 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, July 20-23, 2003, 522-531
|
|
Bishchof B, Starke J, Guenther H, et al. ROGER-robotic geostationary orbit restorer. In: Proceedings of the 8th ESA Workshop on Advanced Space Technologies for Robotics and Automation. The Netherlands, November 2-4, 2004, 1214-1218
|
|
Bonometti J, Sorensen K, Dankanich J. 2006 Status of the momentum exchange electrodynamic re-boost (MXER) tether development. In: Proceedings of 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, Alifornia, July 9-12, 2006, 451-468
|
|
Kassebom M, Koebel D, Tobehn C, et al. ROGER——An advanced solution for a geostationary service satellite. In: Proceedings of 54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law, Bremen, Germany, Sep. 29-30, 2003. 279-285
|
|
李俊峰, 蒋方华. 连续小推力航天器的深空探测轨道优化方法综述.力学与实践, 2011, 33(3): 1-6 (Li Junfeng, Jiang Fanghua. Summary of continuous low-thrust deep space exploration spacecraft orbit optimization method. Journal of Mechanics in Engineering, 2011, 33(3): 1-6 (in Chinese))
|
|
于洋, 宝音贺西, 李俊峰. 空间飞网抛射展开动力学建模与仿真.宇航学报, 2010, 31(5): 1289-1296 (Yu Yang, Baoyin Hexi, Li Junfeng. Modeling and simulation of projecting deployment dynamics of space webs. Journal of Astronautics, 2010, 31(5): 1289-1296 (in Chinese))
|
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