系统工程与电子技术 ›› 2019, Vol. 41 ›› Issue (12): 2827-2834.doi: 10.3969/j.issn.1001-506X.2019.12.22

• 制导、导航与控制 • 上一篇    下一篇

基于MSCMG的复合补偿控制提高图像配准方法

舒适1,2,3,4, 房建成1,2,3, 张伟4, 刘刚1,2,3, 钱勇4, 张健4, 崔培玲1,2,3   

  1. 1. 北京航空航天大学仪器科学与光电工程学院, 北京 100191; 2. 新型惯性仪表与导航系统技术国防重点学科实验室, 北京 100191;
    3. 惯性技术重点实验室, 北京 100191; 4. 上海卫星工程研究所, 上海 200240
  • 出版日期:2019-11-25 发布日期:2019-11-26

Composite compensation method to improve the image registration based on MSCMG

SHU Shi1,2,3,4, FANG Jiancheng1,2,3, ZHANG Wei4, LIU Gang1,2,3, QIAN Yong4, ZHANG Jian4, CUI Peiling1,2,3   

  1. 1. School of Instrument Science and Opto-electronics Engineering, Beiing University of Aeronautics and Astronautics, Beijing 100191, China; 2. Novel Inertial Instrument & Navigation System Technology Key Laboratory of Fundamental Science for National Defense, Beijing 100191, China; 3. Inertial Technology Key Laboratory, Beijing 100191, China; 4. Shanghai Institute of Satellite Engineering, Shanghai, 200240, China
  • Online:2019-11-25 Published:2019-11-26

摘要:

针对星上相机运动干扰影响遥感卫星图像配准精度控制难题,研究基于磁浮控制力矩陀螺(magnetically suspended control moment gyros, MSCMG)的复合补偿控制提高图像配准精度的方法。以基于MSCMG作为执行机构,采用姿态反馈补偿控制方法,避免复杂的控制系统前馈补偿及其自身干扰,姿态稳定精度达到5.8×10-5(°)/s。在此基础上,提出了MSCMG姿态补偿控制与相机运动补偿算法一体化的复合补偿控制方法。仿真结果表明:采用一体化复合补偿控制,跟踪相机步进角精度由补偿前的6 μrad提高到补偿后的0.36 μrad,提高了一个数量级以上;扫描角精度由补偿前的0.6 μrad提高到补偿后的0.45 μrad;显著提高了相机光轴指向的稳定性;研究结果可为甚高精度遥感卫星高精度图像配准设计提供参考。

关键词: 磁浮控制力矩陀螺, 姿态控制, 光轴指向, 复合补偿控制, 图像配准

Abstract:

Focusing on improving image registration precision of the high precise remote sensing satellite due to the camera motion disturbance. The composite compensation method to improve the image registration based on magnetically suspended control moment gyros (MSCMG) is proposed. Firstly, the traditional attitude feedback control system avoiding the complexity of the feed forward control method and its disturbance is used in terms of MSCMG actuators, and the control attitude precision of to 5.8×10-5 (°)/s can be achieved. Then, the integration compensation method is put forward according to attitude control and camera pointing control in order to compensate the attitude residual error due to the constriction of the control band width of the control system. Finally, the simulation is done and the results show that not only the precision of elevation is improved from 6 μrad before compensated to 0.36 μrad after compensated, but also the precision of the scanning angle enhances as well from 0.6 μrad to 0.45 μrad, which boosts the pointing stability of bore sight evidently. Research results can be used as a reference for image registration design for the very high precised remote sensing satellites.

Key words: magnetically suspended control moment gyros, attitude control, bore-sight pointing, composite compensation control, image registration