小行星撞击探测自主导航与制导控制方法

Jing Liu; Shengying Zhu; Yuhua Tang; Rui Xu

doi:10.15982/j.issn.2096-9287.2023.20230110

小行星撞击探测自主导航与制导控制方法

Jing Liu^*
, Shengying Zhu^*
, Yuhua Tang
, Rui Xu

^*此作品的通讯作者

空天科学与技术学院

Beijing Institute of Technology
Ministry of Industry and Information Technology
Deep Space Exploration Laboratory

科研成果: 期刊稿件 › 文章 › 同行评审

3 引用（Scopus）

摘要

Based on the working mode of the autonomous navigation guidance and control system of the impactor，the autonomous optical information processing algorithm，autonomous optical navigation algorithm and trajectory correction guidance law were designed. Based on the research work of autonomous navigation guidance and control system，a comprehensive test system of autonomous navigation guidance and control for small body impact detection was built. Semi-physical ground simulation test of autonomous navigation guidance and control for small body impact was carried out. The simulation results show that the proposed method can effectively achieve high precision asteroid impact.

投稿的翻译标题	Research on Autonomous Guidance Navigation and Control Methods for Small Body Impact Detection
源语言	繁体中文
页（从-至）	405-412
页数	8
期刊	Journal of Deep Space Exploration
卷	10
期	4
DOI	https://doi.org/10.15982/j.issn.2096-9287.2023.20230110
出版状态	已出版 - 8月 2023

关键词

autonomous guidance navigation and control
impact detection
small body

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10.15982/j.issn.2096-9287.2023.20230110

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title = "小行星撞击探测自主导航与制导控制方法",

abstract = "Based on the working mode of the autonomous navigation guidance and control system of the impactor，the autonomous optical information processing algorithm，autonomous optical navigation algorithm and trajectory correction guidance law were designed. Based on the research work of autonomous navigation guidance and control system，a comprehensive test system of autonomous navigation guidance and control for small body impact detection was built. Semi-physical ground simulation test of autonomous navigation guidance and control for small body impact was carried out. The simulation results show that the proposed method can effectively achieve high precision asteroid impact.",

keywords = "autonomous guidance navigation and control, impact detection, small body",

author = "Jing Liu and Shengying Zhu and Yuhua Tang and Rui Xu",

year = "2023",

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doi = "10.15982/j.issn.2096-9287.2023.20230110",

language = "繁体中文",

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T1 - 小行星撞击探测自主导航与制导控制方法

AU - Liu, Jing

AU - Zhu, Shengying

AU - Tang, Yuhua

AU - Xu, Rui

PY - 2023/8

Y1 - 2023/8

N2 - Based on the working mode of the autonomous navigation guidance and control system of the impactor，the autonomous optical information processing algorithm，autonomous optical navigation algorithm and trajectory correction guidance law were designed. Based on the research work of autonomous navigation guidance and control system，a comprehensive test system of autonomous navigation guidance and control for small body impact detection was built. Semi-physical ground simulation test of autonomous navigation guidance and control for small body impact was carried out. The simulation results show that the proposed method can effectively achieve high precision asteroid impact.

AB - Based on the working mode of the autonomous navigation guidance and control system of the impactor，the autonomous optical information processing algorithm，autonomous optical navigation algorithm and trajectory correction guidance law were designed. Based on the research work of autonomous navigation guidance and control system，a comprehensive test system of autonomous navigation guidance and control for small body impact detection was built. Semi-physical ground simulation test of autonomous navigation guidance and control for small body impact was carried out. The simulation results show that the proposed method can effectively achieve high precision asteroid impact.

KW - autonomous guidance navigation and control

KW - impact detection

KW - small body

UR - https://www.scopus.com/pages/publications/105017135368

U2 - 10.15982/j.issn.2096-9287.2023.20230110

DO - 10.15982/j.issn.2096-9287.2023.20230110

M3 - 文章

AN - SCOPUS:105017135368

SN - 2096-9287

VL - 10

SP - 405

EP - 412

JO - Journal of Deep Space Exploration

JF - Journal of Deep Space Exploration

IS - 4

ER -

小行星撞击探测自主导航与制导控制方法

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