首页 | 本学科首页   官方微博 | 高级检索  
     

多航天器协同探测效能影响参数不确定性分析
引用本文:高辰,杨震,张玉珠,牛文龙. 多航天器协同探测效能影响参数不确定性分析[J]. 宇航学报, 2020, 41(4): 499-506. DOI: 10.3873/j.issn.1000-1328.2020.04.014
作者姓名:高辰  杨震  张玉珠  牛文龙
作者单位:1. 中国科学院国家空间科学中心,北京 100190;2. 中国科学院大学,北京 100049
基金项目:空间科学先导专项(XDA1502070202)
摘    要:为解决传统基于蒙特卡洛仿真的探测效能不确定性分析评价方法中时间效率低,参数关系映射单一的问题,提出一种基于神经网络的不确定性分析方法,利用人工神经网络在拟合回归分析上的非线性特性,设计了能够替代复杂系统的神经网络结构,能够通过少量仿真计算结果作为训练样本实现模型的收敛并能有效反映被替代系统的原有特性。选择以一个多航天器的天文观测任务作为典型用例,建立了仿真分析模型,并与蒙特卡洛仿真方法结果进行了对比,验证了此方法的准确性和计算效率。

关 键 词:不确定性分析  空间科学任务分析  蒙特卡洛仿真  神经网络模型  
收稿时间:2019-03-20

Performance Uncertainty Analysis of Multi Spacecraft Mission
GAO Chen,YANG Zhen,ZHANG Yu zhu,NIU Wen long. Performance Uncertainty Analysis of Multi Spacecraft Mission[J]. Journal of Astronautics, 2020, 41(4): 499-506. DOI: 10.3873/j.issn.1000-1328.2020.04.014
Authors:GAO Chen  YANG Zhen  ZHANG Yu zhu  NIU Wen long
Affiliation:1. National Space Science Center, Chinese Academy of Sciences, Beijing 100190, China; 2. University of Chinese Academy of Sciences, Beijing 100049, China
Abstract:Uncertainty analysis plays an important role in early phases of a space mission. The uncertainty of parameters, such as the accuracy of positioning, timing and error in payloads, broadly exists in space mission. When it comes to a distributed satellite system, this problem turns to be more complicated. Traditional method is Monte Carlo simulation, which is time consuming and hard to recognize the coupling relationship between parameters. In this paper, we propose a method which uses a neural network as the model to replace the MCS process. By training the network model using small number of samples, this method can build a model and have advantages in time consuming. We use a multi-spacecraft astronomical observation mission as the use case, And the comparison results between the two methods verify the feasibility of the proposed method.
Keywords:Uncertainty analysis  Space science mission analysis  Monte Carlo simulation  Artificial neural network  
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航学报》浏览原始摘要信息
点击此处可从《宇航学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号