西安电子科技大学学报 ›› 2019, Vol. 46 ›› Issue (2): 23-28.doi: 10.19665/j.issn1001-2400.2019.02.005

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星载相控阵热变形误差估计与校正方法

霍立寰1,廖桂生1,2,杨志伟1,2,辛金龙1   

  1. 1. 西安电子科技大学 雷达信号处理国家重点实验室,陕西 西安 710071
    2. 西安电子科技大学 信息感知技术协同创新中心,陕西 西安 710071
  • 收稿日期:2018-08-12 出版日期:2019-04-20 发布日期:2019-04-20
  • 作者简介:霍立寰(1992-),男,西安电子科技大学博士研究生,E-mail:huolihuan@163.com.
  • 基金资助:
    国家自然科学基金(61621005);国家自然科学基金(61671352)

Array thermal deformation error calibration method for spaceborne radar

HUO Lihuan1,LIAO Guisheng1,2,YANG Zhiwei1,2,XIN Jinlong1   

  1. 1. National Key Lab. of Radar Signal Processing, Xidian Univ., Xi’an 710071, China
    2. Collaborative Innovation Center of Information Sensing and Understanding, Xidian Univ., Xi’an 710071, China
  • Received:2018-08-12 Online:2019-04-20 Published:2019-04-20

摘要:

为提高星载相控阵天线热变形误差估计精度,提出一种结合机械测量和信号处理的误差估计方法。该方法利用测量传感器的测量数据,能够快速地拟合得到形变阶数和阵元初始位置;根据星-地几何关系,提取已知来波角度的模糊地块回波作为校正源数据,进而结合形变特性建立优化模型,在迭代中计算得到更加精确的阵元位置估计值。仿真结果表明,该方法能够获得优于1/15波长的热变形误差估计结果,并且在较大变形误差的情况下仍具有良好的稳健性,最终获得了良好的方向图校正结果。

关键词: 星载雷达, 热变形, 误差校正

Abstract:

In order to improve the accuracy of the thermal deformation error estimation for spaceborne phased arrays, an array error estimation method is proposed which combines the measurement and the signal processing. In the proposed method, the deformation order and initial positions are obtained from the measurement. Then the echo data can be obtained from the range-Doppler images. The optimization model is established based on the deformation characteristics. The sensor positions can be corrected with high accuracy in the iteration. Several simulated results show that the proposed method can obtain estimation better than one-fifteenth the wavelength and is still robust under the large deformation error condition. The array pattern is compensated well in the simulation.

Key words: spaceborne radar, thermal deformation, calibration.

中图分类号: 

  • TN958.92