Only feature point line-of-sight relative navigation in asteroid exploration descent stage-Reference-Cited by-同舟云学术

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Only feature point line-of-sight relative navigation in asteroid exploration descent stage

Published:2014-12 Issue: Volume:39 Page:628-638
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ma Hongliang^ORCID,Xu Shijie

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference22 articles.

1. Linear System Theory and Design;Chen,1999

2. Optimal Estimation of Dynamic Systems;Crassidis,2004

3. Autonomous optical navigation and guide method for soft landing on small bodies;Cui;J. Astronaut.,2009

4. A multi-sensors fusion filtering algorithm for small satellite attitude determination;Duan;J. Astronaut.,2006

5. Implementation of the first asteroid landing;Dunham;Icarus,2002

Cited by 11 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Optimization-based iterative and robust strategy for spacecraft relative navigation in elliptical orbit;Aerospace Science and Technology;2023-02

2. Visual navigation with fast landmark selection based on error analysis for asteroid descent stage;Advances in Space Research;2021-11

3. A Sensitivity Analysis of Satellite Navigation Using Landmarks;2021 IEEE Aerospace Conference (50100);2021-03-06

4. Visual navigation algorithm based on line geomorphic feature matching for Mars landing;Acta Astronautica;2020-08

5. Autonomous navigation for small body landing using optical and inter-spacecraft measurements;2020 IEEE Aerospace Conference;2020-03

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