近地卫星陨落期地球反照系数估计

李强; 张烨; 田凯; 祝俊淞; 段崇雯

doi:10.3788/OPE.20182604.0796

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近地卫星陨落期地球反照系数估计

现代应用光学 | 更新时间：2020-07-05

- 近地卫星陨落期地球反照系数估计
- Estimation of albedo coefficient of Earth during LEO satellite falling
- 光学精密工程 2018年26卷第4期页码：796-806
- 作者机构：
  
  1.宇航动力学国家重点实验室, 陕西西安 710043
  2.西安卫星测控中心, 陕西西安 710043
- 作者简介：
  
  [ "李强(1976-), 男, 湖北荆州人, 硕士, 工程师, 1998年于武汉测绘科技大学获得学士学位, 2007年于华中科技大学获得硕士学位, 主要从事卫星测控与在轨管理的研究。E-mail:buffalo126126@126.com" ]
- 基金信息：
  
  青年科学基金资助项目(61401515)
- DOI：10.3788/OPE.20182604.0796
  中图分类号： V556.1
- 收稿日期：2017-07-24，
  
  录用日期：2017-9-15，
  
  纸质出版日期：2018-04-25
- 稿件说明：
移动端阅览
李强, 张烨, 田凯, 等. 近地卫星陨落期地球反照系数估计[J]. 光学精密工程, 2018,26(4):796-806.

Qiang LI, Ye ZHANG, Kai TIAN, et al. Estimation of albedo coefficient of Earth during LEO satellite falling[J]. Optics and precision engineering, 2018, 26(4): 796-806.
李强, 张烨, 田凯, 等. 近地卫星陨落期地球反照系数估计[J]. 光学精密工程, 2018,26(4):796-806. DOI： 10.3788/OPE.20182604.0796.

Qiang LI, Ye ZHANG, Kai TIAN, et al. Estimation of albedo coefficient of Earth during LEO satellite falling[J]. Optics and precision engineering, 2018, 26(4): 796-806. DOI： 10.3788/OPE.20182604.0796.

摘要

为了研究地球反照的可见光对太阳电池阵电流在卫星陨落期间的影响程度，进行阵电流的地球反照系数估计。以运行在300 km高度、降交点地方时约10：30AM的某太阳同步轨道近地卫星陨落为例，在讨论卫星轨道半长轴、倾角、光照角、降交点地方时等参数漂移的基础上，重点分析卫星太阳电池阵电流和温度的变化，并对电流进行正弦曲线拟合，进而建立地球反照系数的估计模型，最后用卫星陨落期间的遥测数据进行检验。结果表明，卫星自300 km轨道高度向100 km轨道高度陨落期间，地球反照系数先由0.21逐渐变大，最大值接近0.40，后又逐渐变小至0.20附近；对估计值的二次曲线拟合结果表明，在轨道高度210~270 km这一区间，地球反照对于太阳电池阵的作用最强，对应的地球反照系数极大值约为0.28，作用最强的中心区域可能在250 km轨道高度附近。估计结果可应用于在轨航天器长期管理的遥测诊断、能源估计与预测、器件健康状态评估以及可见光载荷应用等方面。

Abstract

In order to estimate the albedo coefficient of the Earth

one needs to investigate the change in solar array output current of a low Earth orbit (LEO) satellite caused by the sunlight reflected from the Earth while the satellite is falling to the ground. An LEO satellite orbiting along a sun-synchronous orbit at an altitude of 300 km with a local time of descending node (LTDN) of 10:30 A.M. is selected as the sample. Details of the semi-major axis degradation

inclination perturbance

solar incidence variation

and LTDN shift are discussed

and the solar array output current and temperature are analyzed. Based on the sinusoidal fitting of the solar array output current data

a method for estimating the albedo coefficient of the Earth is developed. The results

validated by telemetry

indicate that when the satellite falls from an altitude of 300 km to 100 km

the albedo coefficient of the Earth increases gradually from 0.21 to 0.40

and then decreases to approximately 0.20. Parabolic fitting of the estimated results indicate that for orbits at altitudes in the range 210-270 km

the albedo coefficient of the Earth results in an enhanced solar array output current

with the maximum occurring for an orbit at an altitude of approximately 250 km when the albedo coefficient of the Earth is approximately 0.28. The results will be helpful for telemetry diagnosis

energy estimation and prediction

and device state of health evaluation for long-term management of satellites for tracking

telemetry

and command

and visible light payload applications.

关键词

Keywords

references

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