欢迎访问中国科学院大学学报,今天是
论文

太阳同步轨道卫星上太阳方位的计算及精度分析

  • 张乾 ,
  • 叶新 ,
  • 方伟
展开
  • 1. 中国科学院长春光学精密机械与物理研究所, 长春 130033;
    2. 中国科学院研究生院, 北京 100049

收稿日期: 2010-06-24

  修回日期: 2010-08-03

  网络出版日期: 2011-05-15

基金资助

国家自然科学基金(61077080)资助 

Calculation of sun’s location on the sun synchronous orbit satellite and its precision analysis

  • ZHANG Qian ,
  • YE Xin ,
  • FANG Wei
Expand
  • 1. Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, China;
    2. Graduate University, Chinese Academy of Sciences, Beijing 100049, China

Received date: 2010-06-24

  Revised date: 2010-08-03

  Online published: 2011-05-15

摘要

为了在太阳同步轨道卫星上,实现太阳辐射监测仪对太阳辐射的跟踪测量,提出了一种卫星本体坐标系上太阳方位的计算方法.首先,采用巴黎天文台的VSOP87理论计算太阳在地心惯性坐标系下的太阳方位;然后,通过坐标变换转换到卫星本体坐标系上,实现了太阳方位的计算;最后,利用拟平均根数法生成卫星瞬时轨道根数,模拟计算太阳方位的计算精度.该方法对卫星本体坐标系上太阳方位的计算精度优于0.19°,满足实际跟踪精度的要求.

本文引用格式

张乾 , 叶新 , 方伟 . 太阳同步轨道卫星上太阳方位的计算及精度分析[J]. 中国科学院大学学报, 2011 , 28(3) : 310 -314 . DOI: 10.7523/j.issn.2095-6134.2011.3.005

Abstract

A method for calculation of the sun’s location in the satellite’s body coordinate system is proposed in order to measure the solar irradiance using solar irradiance absolute radiometer on the sun synchronous orbit satellite. First, the sun’s location in the inertial coordinate system is calculated using the VSOP87 theory. Then, the sun’s location in the satellite’s body coordinate system is obtained by coordinate transformation. Finally, the satellite’s instantaneous orbital elements of high accuracy are generated based on the mean orbital elements to simulate the precision for calculation of the sun’s location. The simulation shows that the accuracy for the calculation of the sun’s location is within 0.19°.

参考文献


[1] 王炳忠,莫月琴,杨云. 现代气象辐射测量技术
[M]. 北京:气象出版社,2008:1-20.

[2] Lü W H, He X L, Yu H J, et al. Development of full-automatic solar tracker and its application
[J]. Optics and Precision Engineering, 2008, 16(12): 2544-2550(in Chinese). 吕文华,贺晓雷,于贺军,等. 全自动太阳跟踪器的研制和应用
[J]. 光学精密工程,2008,16(12):2544-2550.

[3] Meeus J. Astronomical algorithms
[M]. USA:Willmann-Bell Inc,1998:157-159.

[4] 中国科学院紫金山天文台. 2006年中国天文年历
[M]. 北京:科学出版社,2005.

[5] 刘林. 航天器轨道理论
[M]. 北京:国防工业出版社,2000:99-308.

[6] 汤锡生,陈贻迎,朱民才. 载人飞船轨道确定和返回控制
[M]. 北京:国防工业出版社,2002:130-176.

[7] 杨颖,王琦. STK在计算机仿真中的应用
[M]. 北京:国防工业出版社,2005:153-162.

[8] Wei X G, Jiang J, Wen Z M, et al. Optical system design for MEMS based digital sun sensor
[J]. Optics and Precision Engineering, 2008, 16(8): 1361-1366(in Chinese). 魏新国,江洁,温志明,等. 基于MEMS的数字式太阳敏感器光学系统设计
[J]. 光学精密工程,2008,16(8):1361-1366.

文章导航

/