High-Precision Angle Prediction of Sun for Space Remote Sensing Instrument
Y. Wang; Z. Li; G. Lin and Y. Huang
刊名International Journal of Aerospace Engineering
2021
卷号2021
ISSN号16875966
DOI10.1155/2021/8733478
英文摘要In order to grasp the timing of sun calibration in advance, this paper introduces a high-precision method to predict the solar angle by using the current broadcast time and orbital instantaneous root of the satellite platform. By calculating the sun's apparent right ascension and apparent declination, the conversion matrix from the geocentric inertial coordinate system to the orbital coordinate system, and the satellite attitude correction matrix, the sun vector in the satellite body coordinate system is obtained. This method is used to predict the sun angle of a sun synchronous orbit in the satellite coordinate system, and the prediction results are compared with the STK simulation results. The results show that the sun angle prediction error of this method is less than 0.003. It can meet the requirements of on-orbit solar calibration. The main error sources in the prediction method are analysed. 2021 Yan Wang et al.
URL标识查看原文
内容类型期刊论文
源URL[http://ir.ciomp.ac.cn/handle/181722/65302]  
专题中国科学院长春光学精密机械与物理研究所
推荐引用方式
GB/T 7714
Y. Wang,Z. Li,G. Lin and Y. Huang. High-Precision Angle Prediction of Sun for Space Remote Sensing Instrument[J]. International Journal of Aerospace Engineering,2021,2021.
APA Y. Wang,Z. Li,&G. Lin and Y. Huang.(2021).High-Precision Angle Prediction of Sun for Space Remote Sensing Instrument.International Journal of Aerospace Engineering,2021.
MLA Y. Wang,et al."High-Precision Angle Prediction of Sun for Space Remote Sensing Instrument".International Journal of Aerospace Engineering 2021(2021).
个性服务
查看访问统计
相关权益政策
暂无数据
收藏/分享
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。


©版权所有 ©2017 CSpace - Powered by CSpace