Infrared and Laser Engineering, Volume. 44, Issue 2, 549(2015)

Analysis of symmetric sweep motion characteristic of satellite rigid loads

Chang Lin1,2、*, Jin Guang1, Yang Xiubin1, Qu Hongsong1, and Xu Kai1
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • show less
    References(16)

    [1] [1] He Hongyan, Wu Congde, Wang Xiaoyong. Study of influence of swinging on the systemic parameters of the satellite and CCD camera[J]. Spacecraft Recovery & Remote Sensing, 2003, 24(4): 14-18. (in Chinese)

    [4] [4] Geng Miao, Lu Shan, Xia Yongjiang. Fast maneuver of satellite by mixed control moment gyro and momentum wheel[J]. Aerospace Shanghai, 2013, 30(1): 8-14. (in Chinese)

    [5] [5] Xu Kai, Liu Chunyu, Zhou Meili, et al. Design of momentum compensation control for micro-small satellite with double swinging mechanism[J]. Optics Precision and Engineering, 2013, 21(S): 221-226. (in Chinese)

    [6] [6] Xue Yonghong, An Wei, Zhang Tao, et al. Real time line of sight calibration algorithm for high earth orbit infrared scanning sensor[J]. Acta Optica Sinica, 2013, 33(6): 0628003-1-0628003-6. (in Chinese)

    [7] [7] Shen Zhong. Dynamic interactions analysis of HJ-1B satellite platform and onboard infrared camera scanning mirror[D]. Wuhan: National University of Defense Technology, 2005: 21-33. (in Chinese)

    [8] [8] Yu Zhefeng, Yang Zhichun. Effects of scan mirror motion on the attitude of three-axis-stabilized geostationary satellite[J]. Journal of Northwestern Polytechnical University, 2003, 21(1): 87-90. (in Chinese)

    [9] [9] Li Yuan. Study on dynamic modeling and control system of satellite with multiple rotatable payloads[D]. Wuhan: National University of Defense Technology, 2005: 27-39. (in Chinese)

    [10] [10] Jia Yinghong, Xu Shijie. Scan mirror motion compensation of geostationary satellite[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(8): 873-877. (in Chinese)

    [11] [11] Qian Yong, Man Shunqiang. Influence analysis of spacecraft's attitude based on variable-structure control to decrease motion of scanning camera[J]. Aerospace Erospace Shanghai, 2012, 29(6): 7-11. (in Chinese)

    [12] [12] Markley F L, Bauer F H, Femiano M D. Attitude control system conceptual design for geostationary operational environmental satellite spacecraft series[J]. Journal of Guidance, Control and Dynamics, 1995, 18(2): 247-255.

    [13] [13] Lau Jimmy, Joshi Sanjay S, Agrawal Brij N, et al. Investigation of periodic-disturbance identification and rejection in spacecraft[J]. Journal of Guidance, Control, and Dynamics, 2006, 29(4): 792-798.

    [15] [15] Lei Jing, Liu Yingying, Zhou Fengqi, et al. A new method for identification of and compensation for periodically disturbing torques of on-orbit Satellite[J]. Journal of Northwestern Polytechnical University, 2009, 27(3): 396-400. (in Chinese)

    [16] [16] Liu Jun, Han Chao, Zhang Wei. Analysis on disturbance of mobile bodies and compensation control of satellite attitude[J]. Aerospace Shanghai, 2006(6): 22-26. (in Chinese)

    Tools

    Get Citation

    Copy Citation Text

    Chang Lin, Jin Guang, Yang Xiubin, Qu Hongsong, Xu Kai. Analysis of symmetric sweep motion characteristic of satellite rigid loads[J]. Infrared and Laser Engineering, 2015, 44(2): 549

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Category: 先进光学

    Received: Jun. 9, 2014

    Accepted: Jul. 10, 2014

    Published Online: Jan. 26, 2016

    The Author Email: Lin Chang (fanglinchang@aliyun.com)

    DOI:

    Topics