Autonomous navigation and guidance for landing on asteroids

Shuang Li; Pingyuan Cui; Hutao Cui

doi:10.1016/j.ast.2005.12.003

Autonomous navigation and guidance for landing on asteroids

Shuang Li^*
, Pingyuan Cui
, Hutao Cui

^*Corresponding author for this work

Harbin Institute of Technology

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

70 Citations (Scopus)

Abstract

This paper presents an autonomous landing navigation and guidance scheme for future asteroid sample return mission. An autonomous navigation scheme based on feature tracking technology is brought out firstly; secondly, desired descent landing trajectories with the initial and terminal constraints are planned in order to achieve arrive-at-time landing on an asteroid; then, two guidance control laws, based on error phase analysis method and PD plus PWPF method respectively, are designed to track reference descent trajectory; finally, the validity of the proposed scheme is confirmed by computer simulation.

Original language	English
Pages (from-to)	239-247
Number of pages	9
Journal	Aerospace Science and Technology
Volume	10
Issue number	3
DOIs	https://doi.org/10.1016/j.ast.2005.12.003
Publication status	Published - Apr 2006
Externally published	Yes

Keywords

Autonomous landing
Error phase analysis
Feature tracking
Navigation and guidance
PWPF

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10.1016/j.ast.2005.12.003

Cite this

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title = "Autonomous navigation and guidance for landing on asteroids",

abstract = "This paper presents an autonomous landing navigation and guidance scheme for future asteroid sample return mission. An autonomous navigation scheme based on feature tracking technology is brought out firstly; secondly, desired descent landing trajectories with the initial and terminal constraints are planned in order to achieve arrive-at-time landing on an asteroid; then, two guidance control laws, based on error phase analysis method and PD plus PWPF method respectively, are designed to track reference descent trajectory; finally, the validity of the proposed scheme is confirmed by computer simulation.",

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AU - Cui, Hutao

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AB - This paper presents an autonomous landing navigation and guidance scheme for future asteroid sample return mission. An autonomous navigation scheme based on feature tracking technology is brought out firstly; secondly, desired descent landing trajectories with the initial and terminal constraints are planned in order to achieve arrive-at-time landing on an asteroid; then, two guidance control laws, based on error phase analysis method and PD plus PWPF method respectively, are designed to track reference descent trajectory; finally, the validity of the proposed scheme is confirmed by computer simulation.

KW - Autonomous landing

KW - Error phase analysis

KW - Feature tracking

KW - Navigation and guidance

KW - PWPF

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DO - 10.1016/j.ast.2005.12.003

M3 - Article

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ER -

Autonomous navigation and guidance for landing on asteroids

Abstract

Keywords

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