Simulation and experiment on attitude tracking control of small TV satellite

SUN Zhi-yuan; ZHANG Liu; JIN Guang; XU Kai; CHEN Mao-sheng

doi:10.3788/OPE.20111911.2715

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Simulation and experiment on attitude tracking control of small TV satellite

Article | 更新时间：2020-08-12

- Simulation and experiment on attitude tracking control of small TV satellite
- Optics and Precision Engineering Vol. 19, Issue 11, Pages: 2715-2723(2011)
- 作者机构：
  
  1. 中国科学院长春光学精密机械与物理研究所,吉林长春,中国,130033
  2. 中国科学院研究生院,北京 100039
- 作者简介：
- 基金信息：
- DOI：10.3788/OPE.20111911.2715
  CLC： V474.262
- Received：01 March 2011，
  
  Revised：01 April 2011，
  
  Published Online：25 November 2011，
  
  Published：25 November 2011
- 稿件说明：
移动端阅览
孙志远, 张刘, 金光, 徐开, 陈茂胜. 视频小卫星凝视姿态跟踪的仿真与实验[J]. 光学精密工程, 2011,19(11): 2715-2723

SUN Zhi-yuan, ZHANG Liu, JIN Guang, XU Kai, CHEN Mao-sheng. Simulation and experiment on attitude tracking control of small TV satellite[J]. Editorial Office of Optics and Precision Engineering, 2011,19(11): 2715-2723
孙志远, 张刘, 金光, 徐开, 陈茂胜. 视频小卫星凝视姿态跟踪的仿真与实验[J]. 光学精密工程, 2011,19(11): 2715-2723 DOI： 10.3788/OPE.20111911.2715.

SUN Zhi-yuan, ZHANG Liu, JIN Guang, XU Kai, CHEN Mao-sheng. Simulation and experiment on attitude tracking control of small TV satellite[J]. Editorial Office of Optics and Precision Engineering, 2011,19(11): 2715-2723 DOI： 10.3788/OPE.20111911.2715.

摘要

对视频卫星实现对地凝视成像时的数学模型、姿态跟踪控制器设计和全物理仿真进行了研究。首先

根据卫星轨道运动与姿态运动相关理论

推导了对地凝视时视频小卫星相对轨道坐标系的期望四元数和期望姿态角速度的变化规律。设计了基于误差四元数和误差姿态角速度的PD控制器

并采用李雅普诺夫稳定性理论证明了所设计控制器的稳定性。然后

以在曝光时间内的面阵CCD成像偏差不超过0.3 pixel为要求

给出了姿态角控制精度和姿态角速度控制精度的最小极限值。最后

在设计的基于小型三轴气浮台的小卫星姿态控制系统全物理仿真平台上对视频小卫星凝视摄像进行了仿真验证。实验结果表明

小型三轴气浮台的姿态角控制精度优于0.1

姿态角速度控制精度优于0.01()/s

基本满足视频小卫星凝视时面阵CCD高质量成像的要求。

Abstract

This paper focuses mainly on the mathematical model of ground target tracking of a video satellite and the design of an attitude tracking controller. Firstly

the desired attitude quaternion and the desired attitude angular velocity are presented respectively according to the orbit kinematic and attitude kinematic. Then

a feedback PD controller based on the error quaternion and error attitude angular velocity is designed

and the stability of the designed controller is analyzed by using the Lyapunov stability theory. By setting the deviation of area CCD in the exposal time to be smaller than 0.3 pixel

the minimum attitude pointing error and attitude velocity error are induced. Finally

physical simulation of staring-imaging by a video camera is conducted on the minitype three-axis air bearing table. Simulation results suggest that the pointing error is less than 0.1

and that the attitude velocity error is less than 0.012()/s

which meets the requirements of staring-imaging of area CCDs.

关键词

Keywords

references

刘兆军,陈伟. 面阵凝视型成像空间应用技术[J]. 红外与激光工程,2006,35(5): 541-545. LIU Z J, CHEN W. Space applications of staring imaging technology with area FPA [J]. Infrared and Laser Engineering, 2006, 35(5): 541-545. (in Chinese)[2] ROBERTUR H T, AYOM W. Video camera system on LAPAN-TUBSAT micro-satellite . Proceeding of Asian Space Conference, Singapore, 2007: 1-5.[3] WILLEM H S. A view finder control system for an earth observation satellite [J]. Aerospace Science and Technology, 2006, 10: 248-255.[4] 李俊峰,徐敏,STEYN W H. 低轨道航天器姿态跟踪机动控制研究 [J]. 清华大学学报(自然科学版),2001,41(2):102-104. LI J F, XU M, STEYN W H. Attitude tracking maneuvers of a low earth orbit spacecraft[J]. Journal of Tsinghua University(Science & Technology), 2001,41(2):102-104.(in Chinese)[5] 邬树楠,孙兆伟,叶东. 低轨对地凝视卫星姿态控制[J]. 上海航天,2010,1(1): 15-20. WU S N, SUN Z W, YE D. Attitude control of a staring-imaging satellite in LEO[J]. Aerospace Shanghai, 2010,1(1): 15-20. (in Chinese)[6] SHINH C L, YON P C. Smooth sliding-mode control for spacecraft attitude tracking maneuvers[J].Journal of Guidance, Control, and Dynamics, 1995, 18(6):1345-1349.[7] 林壮,段广仁,宋申民, 刚体航天器姿态跟踪的高阶滑膜控制器设计[J]. 控制与决策,2009,24(11): 1753-1756. LIN Z, DUAN G R, SONG S M. Design of higher-order sliding mode controller for rapid spacecraft attitude tracking maneuver [J]. Control and Decision, 2009,24(11): 1753 -1756. (in Chinese)[8] 刘军,韩潮. 使用变速控制力矩陀螺的航天器鲁棒自适应姿态跟踪控制[J]. 航空学报,2008,29(1): 159-154. LIU J, HAN C. Spacecraft adaptive robust attitude tracking control with variable speed control moment gyroscopes [J]. Acta Aeronautica Et Astronautica Sinica, 2008, 29(1): 159-154.(in Chinese)[9] 汤亮,徐世杰. 采用变速控制力矩陀螺的航天器自适应姿态跟踪和稳定控制研究[J]. 航空学报,2006,27(4):663-669. TANG L, XU S J. Spacecraft adaptive attitude aracking and stable control with variable speed control moment gyroscopes [J]. Acta Aeronautica Et Astronautica Sinica, 2006, 27(4): 663-669. (in Chinese)[10] LI C, MA G F, SONG B. Spacecraft attitude tracking control based on nonlinear H control . Proceeding of 1st International Symposium on Systems and Control in Aerospace and Astronautics, Harbin, 2006: 395-399.[11] 王家骐,于平,颜昌翔,等. 航天光学遥感器像移速度矢计算数学模型[J]. 光学学报,2004,24(12): 1585-1589. 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)[12] 章仁为.卫星轨道姿态动力学与控制[M]. 北京:北京航空航天大学出版社 ,1998. ZHANG R W. Dynamics and Control of Satellite orbit And attitude [M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 1998.(in Chinese)[13] WIE B, WEISS H, ARAPOSTATHIS A. Quaternion feedback regulator for spacecraft eigenaxis rotations [J]. Journal of Guidance, Control and Dynamics, 1989, 12(3): 375-380.[14] 杨秀彬,贺小军,张刘,等. 偏流角误差对TDI CCD相机成像的影响与仿真[J]. 光电工程,2008,35(11):45-50. YANG X B, HE X J, ZHANG L, et al.. Effect and simulate of the deviant angle error on TDI CCD cameras image[J]. Opt. Precision Eng., 2008,35(11):45-50.(in Chinese)[15] 颜昌翔,王家骐. 航相机像移补偿计算的坐标变换方法[J]. 光学精密工程,2000,8(3):203-207. YAN C X, WANG J Q. Method of coordinate transformation for IM&IMC calculation in aerospace camera system [J]. Opt. Precision Eng., 2000, 8(3): 203-207.(in Chinese)[16] 黄猛,刘家燕,张葆,等. 小型面阵航空相机系统的像移补偿[J]. 电光与控制,2009,16(3):68-71. HUANG M, LIU J Y, ZHANG B. et al.. Image motion compensation of small aerial camera system with area array sensor [J]. Electronics Optics & Control, 2009, 16(3): 68-71.

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