一种再入机动的实时自适应滤波算法

Peng Dan, Tao Xi, Dan Wang
{"title":"一种再入机动的实时自适应滤波算法","authors":"Peng Dan, Tao Xi, Dan Wang","doi":"10.1109/CAC57257.2022.10055988","DOIUrl":null,"url":null,"abstract":"In order to solve the problem of the real-time reconstruction of the reentry trajectory with lift-to-drag controlling law during the spacecraft’s reentry flight, an adaptive UKF filtering algorithm was proposed by using external measurements and considering the actual engineering situations. The filter’s state model and observation model were given, and some adaptive processing methods were used, including the maneuver detection and model switching method, and the acceleration compensation method, which were used to deal with the real-time tracking of the maneuvering process of the return flight. The simulation results show that the proposed calculation method is feasible, and the proposed adaptive processing algorithm applying the acceleration compensation can do the robust estimation processing of the reentry trajectory. The research results have certain reference value for the real-time estimation of maneuvering reentry spacecraft.","PeriodicalId":287137,"journal":{"name":"2022 China Automation Congress (CAC)","volume":"136 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-11-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"A Real-time Adaptive Filtering Algorithm for Reentry Maneuvering\",\"authors\":\"Peng Dan, Tao Xi, Dan Wang\",\"doi\":\"10.1109/CAC57257.2022.10055988\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In order to solve the problem of the real-time reconstruction of the reentry trajectory with lift-to-drag controlling law during the spacecraft’s reentry flight, an adaptive UKF filtering algorithm was proposed by using external measurements and considering the actual engineering situations. The filter’s state model and observation model were given, and some adaptive processing methods were used, including the maneuver detection and model switching method, and the acceleration compensation method, which were used to deal with the real-time tracking of the maneuvering process of the return flight. The simulation results show that the proposed calculation method is feasible, and the proposed adaptive processing algorithm applying the acceleration compensation can do the robust estimation processing of the reentry trajectory. The research results have certain reference value for the real-time estimation of maneuvering reentry spacecraft.\",\"PeriodicalId\":287137,\"journal\":{\"name\":\"2022 China Automation Congress (CAC)\",\"volume\":\"136 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2022-11-25\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2022 China Automation Congress (CAC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CAC57257.2022.10055988\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2022 China Automation Congress (CAC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CAC57257.2022.10055988","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

摘要

为了解决航天器在再入飞行过程中具有升阻控制律的再入轨迹实时重建问题,结合实际工程情况,利用外部测量数据,提出了一种自适应UKF滤波算法。给出了滤波器的状态模型和观测模型,并采用机动检测和模型切换法、加速度补偿法等自适应处理方法对返航机动过程进行实时跟踪。仿真结果表明,所提出的计算方法是可行的,采用加速度补偿的自适应处理算法能够对再入弹道进行鲁棒估计处理。研究结果对机动再入航天器的实时估计具有一定的参考价值。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Real-time Adaptive Filtering Algorithm for Reentry Maneuvering
In order to solve the problem of the real-time reconstruction of the reentry trajectory with lift-to-drag controlling law during the spacecraft’s reentry flight, an adaptive UKF filtering algorithm was proposed by using external measurements and considering the actual engineering situations. The filter’s state model and observation model were given, and some adaptive processing methods were used, including the maneuver detection and model switching method, and the acceleration compensation method, which were used to deal with the real-time tracking of the maneuvering process of the return flight. The simulation results show that the proposed calculation method is feasible, and the proposed adaptive processing algorithm applying the acceleration compensation can do the robust estimation processing of the reentry trajectory. The research results have certain reference value for the real-time estimation of maneuvering reentry spacecraft.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信