AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
PDF (7.2 MB)
Collect
Submit Manuscript AI Chat Paper
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline
Research Article | Open Access

Modeling and Trajectory Tracking Control for a Novel Multinode Flexible Small-Body Lander Based on a Port-Hamilton Framework

Jingxuan Chai1, Youmin Gong2( ), Jie Mei2( ), Pengyu Wang3, Guangfu Ma2
Insitute of Space Science and Applied Technology, Harbin Institute of Technology (Shenzhen), Guangdong, China
School of Mechanical Engineering and Automation, Harbin Institute of Technology (Shenzhen), Guangdong, China
Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST), Daejeon, Korea
Show Author Information

Abstract

Small bodies have the characteristics of noncooperative, irregular gravity, and complex terrain on the surface, which cause difficulties in successful landing for conventional landers. In this paper, a multinode flexible lander is put forward to address the problem. The dynamics of this new lander are constructed based on the port-Hamilton framework. The trajectory-tracking formation controller for the lander is designed in a passive way. The proposed dynamics and controller are further validated through numerical simulations. This research presents a fresh concept that holds inspiration for future design involving small-body landers.

References

【1】
【1】
 
 
Space: Science & Technology
Article number: 0113

{{item.num}}

Comments on this article

Go to comment

< Back to all reports

Review Status: {{reviewData.commendedNum}} Commended , {{reviewData.revisionRequiredNum}} Revision Required , {{reviewData.notCommendedNum}} Not Commended Under Peer Review

Review Comment

Close
Close
Cite this article:
Chai J, Gong Y, Mei J, et al. Modeling and Trajectory Tracking Control for a Novel Multinode Flexible Small-Body Lander Based on a Port-Hamilton Framework. Space: Science & Technology, 2024, 4: 0113. https://doi.org/10.34133/space.0113

1472

Views

31

Downloads

5

Crossref

10

Web of Science

11

Scopus

Received: 10 July 2023
Accepted: 27 October 2023
Published: 13 March 2024
© 2024 Jingxuan Chai et al. Exclusive licensee Beijing Institute of Technology Press. No claim to original U.S. Government Works.

Distributed under a Creative Commons Attribution License 4.0 (CC BY 4.0).