行星着陆自主导航地形特征综合优化方法

Sheng Ying Zhu; Xi Zhen Gao; Ping Yuan Cui; Wen Long Yao

doi:10.3873/j.issn.1000-1328.2021.02.007

行星着陆自主导航地形特征综合优化方法

Translated title of the contribution: Integrated Optimization of Navigation Features for Planetary Landing

Sheng Ying Zhu
, Xi Zhen Gao^*
, Ping Yuan Cui
, Wen Long Yao

^*Corresponding author for this work

School of Aerospace Engineering

Ministry of Industry and Information Technology
Beijing Institute of Technology
CAS - Beijing Institute of Control Engineering

Research output: Contribution to journal › Article › peer-review

6 Citations (Scopus)

Abstract

Aiming at the optimization of optical navigation scheme for planetary landing, this paper proposes an integrated optimization method based on observability. Firstly, the measurement equations of different geometric characteristics are established by using the image information of landmarks. Based on the observability matrix and Fisher information matrix, the observability and the lower limit of estimation error of navigation system are analyzed, and the relationship between the location and quantity of characteristics and the performance of navigation system is revealed. Then, the observability and the lower limit of estimation error of navigation system are used as the evaluation indexes respectively. At last, the influence of different feature points, lines and curves on the performance of navigation scheme is analyzed, and the relevant conclusions are verified by simulation.

Translated title of the contribution	Integrated Optimization of Navigation Features for Planetary Landing
Original language	Chinese (Traditional)
Pages (from-to)	192-201
Number of pages	10
Journal	Yuhang Xuebao/Journal of Astronautics
Volume	42
Issue number	2
DOIs	https://doi.org/10.3873/j.issn.1000-1328.2021.02.007
Publication status	Published - 28 Feb 2021

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10.3873/j.issn.1000-1328.2021.02.007

Cite this

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title = "行星着陆自主导航地形特征综合优化方法",

abstract = "Aiming at the optimization of optical navigation scheme for planetary landing, this paper proposes an integrated optimization method based on observability. Firstly, the measurement equations of different geometric characteristics are established by using the image information of landmarks. Based on the observability matrix and Fisher information matrix, the observability and the lower limit of estimation error of navigation system are analyzed, and the relationship between the location and quantity of characteristics and the performance of navigation system is revealed. Then, the observability and the lower limit of estimation error of navigation system are used as the evaluation indexes respectively. At last, the influence of different feature points, lines and curves on the performance of navigation scheme is analyzed, and the relevant conclusions are verified by simulation.",

keywords = "Autonomous navigation, Feature optimization, Fisher information matrix, Observability analysis, Planetary landing",

author = "Zhu, \{Sheng Ying\} and Gao, \{Xi Zhen\} and Cui, \{Ping Yuan\} and Yao, \{Wen Long\}",

year = "2021",

month = feb,

day = "28",

doi = "10.3873/j.issn.1000-1328.2021.02.007",

language = "繁体中文",

volume = "42",

pages = "192--201",

journal = "Yuhang Xuebao/Journal of Astronautics",

issn = "1000-1328",

publisher = "Chinese Society of Astronautics",

number = "2",

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TY - JOUR

T1 - 行星着陆自主导航地形特征综合优化方法

AU - Zhu, Sheng Ying

AU - Gao, Xi Zhen

AU - Cui, Ping Yuan

AU - Yao, Wen Long

PY - 2021/2/28

Y1 - 2021/2/28

N2 - Aiming at the optimization of optical navigation scheme for planetary landing, this paper proposes an integrated optimization method based on observability. Firstly, the measurement equations of different geometric characteristics are established by using the image information of landmarks. Based on the observability matrix and Fisher information matrix, the observability and the lower limit of estimation error of navigation system are analyzed, and the relationship between the location and quantity of characteristics and the performance of navigation system is revealed. Then, the observability and the lower limit of estimation error of navigation system are used as the evaluation indexes respectively. At last, the influence of different feature points, lines and curves on the performance of navigation scheme is analyzed, and the relevant conclusions are verified by simulation.

AB - Aiming at the optimization of optical navigation scheme for planetary landing, this paper proposes an integrated optimization method based on observability. Firstly, the measurement equations of different geometric characteristics are established by using the image information of landmarks. Based on the observability matrix and Fisher information matrix, the observability and the lower limit of estimation error of navigation system are analyzed, and the relationship between the location and quantity of characteristics and the performance of navigation system is revealed. Then, the observability and the lower limit of estimation error of navigation system are used as the evaluation indexes respectively. At last, the influence of different feature points, lines and curves on the performance of navigation scheme is analyzed, and the relevant conclusions are verified by simulation.

KW - Autonomous navigation

KW - Feature optimization

KW - Fisher information matrix

KW - Observability analysis

KW - Planetary landing

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U2 - 10.3873/j.issn.1000-1328.2021.02.007

DO - 10.3873/j.issn.1000-1328.2021.02.007

M3 - 文章

AN - SCOPUS:85103176593

SN - 1000-1328

VL - 42

SP - 192

EP - 201

JO - Yuhang Xuebao/Journal of Astronautics

JF - Yuhang Xuebao/Journal of Astronautics

IS - 2

ER -

行星着陆自主导航地形特征综合优化方法

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