• Optics and Precision Engineering
  • Vol. 20, Issue 12, 2812 (2012)
HUANG Qun-dong*, YANG Fang, and ZHAO Jiang
Author Affiliations
  • [in Chinese]
  • show less
    DOI: 10.3788/ope.20122012.2812 Cite this Article
    HUANG Qun-dong, YANG Fang, ZHAO Jiang. Calculation of image motion velocity for agile satellite dynamic imaging to changed continuously attitude point[J]. Optics and Precision Engineering, 2012, 20(12): 2812 Copy Citation Text show less
    References

    [1] HUANG Q L, LI X M. Application of TDICCD on real-time earth reconnaissance satellite[C]//Proc. Of SPIE, Automated Optical Inspection for Industry: Theory, Technology and Applications Ⅱ (3558) Washington, 1998:93-104.

    [2] HUANG Q D, YANG F, ZHAO J. Calculation and attitude compensation for the drift angle caused by the agile imaging and the velocity mismatch[C]. 2011, The Development Of Advanced Space Control Technologies Conference,Huangshan,2011:136-144.(in Chinese)

    [3] WANG J Q, YU P, YAN C X, et al.. Space optical remote sensor image motion velocity vector computational modeling[J]. Acta Optica Sinica, 2004,24(12):1585-1589.(in Chinese)

    [4] YAN C X, WANG J Q. Method of coordinate transformation for IM&IMC calculation in aerospace camera system[J]. Opt. Precision Eng., 2006,14(3):203-207.(in Chinese)

    [5] WANG Y, YAN C X. Computation of image motion velocity vector for space camera based on difference method[J].Opt. Precision Eng., 2011,19(5):1054-1060.(in Chinese)

    [6] YAN D J, HAN C S, LI W H. Optimization design of scroll and pitch and their control errors on aerocraft [J]. Opt. Precision Eng., 2009,17(9):2224-2229.(in Chinese)

    [7] YAN D J, XU S Y, HAN C S. Effect of aerocraft attitude on image motion compensation of space camera [J]. Opt. Precision Eng., 2008,16(11):2199-2203.(in Chinese)

    [8] JEAN J, ERIC J, GRARD L, et al.. Attitude guidance technics developed in CNES for earth observation and scientific missions[C]. The 28th Annual AAS Guidance and Control Conference, Breckenridge,2005:11-16.

    [9] PERRET L, BOUSSARIE E, LACHIVER J M, et al.. The Pléiades system high resolution optical satellite and its performances[C]. The 53rd International Astronautical Congress The World Space Congress, Houston,2002.

    [10] LIU Y W, ZHANG J. Agile satellite fast attitude maneuver control method research[C]. The Thirteenth National Conference On Space And Motion Control Technology Conference, Yichang, 2008:1-6.(in Chinese)

    [11] FAN C, LI Y C, YI H W. Influence of Velocity-Height ratio of satellite on the TDICCD camera[J]. Acta Armamentarii, 2007,28(7):817-821.(in Chinese)

    [12] MILLER B M, RUBINOVICH E Y. Image motion compensation at charge-coupled device photographing in delay Integration mode [J]. Automation and Remote Control, 2007, 68(3):564-571.

    [13] OLSON G. Image motion compensation with frame transfer CCD’s [J]. SPIE, 2002,4567:153-160.

    [14] SMITH S L ,TANTALO J M. Understanding image quality losses due to smear in high-resolution remote sensing imaging system [J].Opt Eng,1999,38(5):821-826.

    [15] ZHAI L P, LIU M, XIU J H. Calculation of image motion velocity considering airplane gesture angle in oblique aerial camera [J]. Opt. Precision Eng., 2006, 14(3):490-494.(in Chinese)

    [16] DAMILANO P. Pleiades high resolution satellite: a solution for military and civilian needs in metric-class optical observation[C]. The 15th Annual/USU Conference on Small Satellites, 2001.

    [17] ZHANG L, WU X Q, TANG G M. Analysis of synchronization error for time delayed integration (TDI) CCD imaging system based on MTF[J]. Journal of Applied Optics, 2006, 27(2):167-170.(in Chinese)

    CLP Journals

    [1] Zhao Jiaxin, Zhang Tao, Yang Yongming, Li Xinyang, Wang Dejiang. Image Motion Velocity Filed of TDI-CCD Aerial Panoramic Camera[J]. Acta Optica Sinica, 2014, 34(7): 728003

    [2] Han Xingzi. Analysis of Effect on Image Quality of TDICCD During Dynamic Imaging[J]. Chinese Journal of Lasers, 2014, 41(s1): 114004

    HUANG Qun-dong, YANG Fang, ZHAO Jiang. Calculation of image motion velocity for agile satellite dynamic imaging to changed continuously attitude point[J]. Optics and Precision Engineering, 2012, 20(12): 2812
    Download Citation