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大角速度条件下星像运动轨迹建模及误差评估

何贻洋 王宏力 冯磊 由四海 陈志侃

何贻洋, 王宏力, 冯磊, 等 . 大角速度条件下星像运动轨迹建模及误差评估[J]. 北京航空航天大学学报, 2019, 45(8): 1653-1662. doi: 10.13700/j.bh.1001-5965.2018.0762
引用本文: 何贻洋, 王宏力, 冯磊, 等 . 大角速度条件下星像运动轨迹建模及误差评估[J]. 北京航空航天大学学报, 2019, 45(8): 1653-1662. doi: 10.13700/j.bh.1001-5965.2018.0762
HE Yiyang, WANG Hongli, FENG Lei, et al. Star spot motion trajectory modeling and error evaluation under large angular velocity[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(8): 1653-1662. doi: 10.13700/j.bh.1001-5965.2018.0762(in Chinese)
Citation: HE Yiyang, WANG Hongli, FENG Lei, et al. Star spot motion trajectory modeling and error evaluation under large angular velocity[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(8): 1653-1662. doi: 10.13700/j.bh.1001-5965.2018.0762(in Chinese)

大角速度条件下星像运动轨迹建模及误差评估

doi: 10.13700/j.bh.1001-5965.2018.0762
基金项目: 

国家自然科学基金 61503391

中国博士后科学基金 2017M613372

详细信息
    作者简介:

    何贻洋  男, 博士研究生。主要研究方向:星光导航、星图处理

    王宏力  男, 博士, 教授, 博士生导师。主要研究方向:复合制导以及故障诊断

    冯磊  男, 博士, 讲师。主要研究方向:图像处理、故障诊断和寿命预测

    通讯作者:

    冯磊, E-mail: fengl1983@126.com

  • 中图分类号: TP391.4;V448.22+4

Star spot motion trajectory modeling and error evaluation under large angular velocity

Funds: 

National Natural Science Foundation of China 61503391

China Postdoctoral Science Foundation 2017M613372

More Information
  • 摘要:

    在大角速度条件下星敏感器成像平面上的星像会产生严重拖尾,影响星敏感器性能。为了全面认识星敏感器的星像运动轨迹形式,并定量评估星像运动对星点提取过程的影响,首先研究建立了星敏感器成像平面上星像运动轨迹的数学模型,推导出在成像平面上星像运动轨迹为一段圆弧;然后建立了星像运动时的能量分布模型,并对大角速度条件下基于质心法的星点坐标误差进行了评估,分析得到星点坐标误差的模近似可用星像运动轨迹长度的二分之一来衡量。仿真实验结果验证了所得结论的正确性。

     

  • 图 1  绕任意轴方向转动时的星像运动示意图

    Figure 1.  Schematic diagram of star spot motion when rotating around any axis

    图 2  模糊星图上星像能量分布仿真示意图

    Figure 2.  Schematic diagram of star spot energy distribution simulation on blurred star image

    图 3  静态无噪声条件的理想星图

    Figure 3.  Ideal star image under static noise-free conditions

    图 4  静态有噪声条件的星图

    Figure 4.  Star image under static and noisy conditions

    图 5  Osxs轴转动时star1、star2和star3的运动轨迹

    Figure 5.  Motion trajectory of star1, star2 and star3 when rotating around Osxs axis

    图 6  Osys轴转动时star1、star2和star3的运动轨迹

    Figure 6.  Motion trajectory of star1, star2 and star3 when rotating around Osys axis

    图 7  Oszs轴转动时star1、star2和star3的运动轨迹

    Figure 7.  Motion trajectory of star1, star2 and star3 when rotating around Oszs axis

    图 8  OsxsOsysOszs轴转动时star1、star2和star3的运动轨迹

    Figure 8.  Motion trajectory of star1, star2 and star3 when rotating around Osxs, Osys and Oszs axis

    图 9  仿真条件下的角速度变化曲线

    Figure 9.  Angular velocity curves under simulation conditions

    图 10  仿真条件1)的星点坐标误差

    Figure 10.  Star spot coordinate error under simulation condition 1)

    图 11  仿真条件1)的星点坐标误差的模与星像运动轨迹长度二分之一的对比

    Figure 11.  Comparison of modulus of star spot coordinate error and one half of star spot motion trajectory length under simulation condition 1)

    图 12  仿真条件2)的星点坐标误差

    Figure 12.  Star spot coordinate error under simulation condition 2)

    图 13  仿真条件2)的星点坐标误差的模与星像运动轨迹长度二分之一的对比

    Figure 13.  Comparison of modulus of star spot coordinate error and one half of star spot motion trajectory length under simulation condition 2)

    图 14  仿真条件3)的星点坐标误差

    Figure 14.  Star spot coordinate error under simulation condition 3)

    图 15  仿真条件3)的星点坐标误差的模与星像运动轨迹长度二分之一的对比

    Figure 15.  Comparison of modulus of star spot coordinate error and one half of star spot motion trajectory length under simulation condition 3)

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出版历程
  • 收稿日期:  2018-12-25
  • 录用日期:  2019-02-22
  • 网络出版日期:  2019-08-20

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