A robust control method of lunar orbit spacecraft autonomous rendezvous

Yunyi Hou; Guangfu Ma; Jianwen Hou; Wenlong Li; Peng Shi

A robust control method of lunar orbit spacecraft autonomous rendezvous

Yunyi Hou
, Guangfu Ma
, Jianwen Hou
, Wenlong Li
, Peng Shi

School of Astronautics

Harbin Institute of Technology
China Aerospace Science and Technology Corporation
Beihang University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

The lunar orbital rendezvous is a key technique of lunar return mission. In this paper, the C-W relative dynamic model is established. The virtual target trajectory was segmented designed, allowing the chaser remain at the docking corridor. The H∞ sub-optimal theory was applied in controller design, restraining the interference and over much energy consumption. The mathematical simulation showed that the proposed control method have advantages of high-accuracy, low power consumption, strong robustness and rapidity. Finally, the real-time visualization platform was established to demonstrate the whole process of lunar orbit spacecraft autonomous rendezvous mission.

Original language	English
Title of host publication	Astrodynamics 2013 - Advances in the Astronautical Sciences
Subtitle of host publication	Proceedings of the AAS/AIAA Astrodynamics Specialist Conference
Publisher	Univelt Inc.
Pages	467-475
Number of pages	9
ISBN (Print)	9780877036050
State	Published - 2014
Event	2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013 - Hilton Head Island, SC, United States Duration: 11 Aug 2013 → 15 Aug 2013

Publication series

Name	Advances in the Astronautical Sciences
Volume	150
ISSN (Print)	0065-3438

Conference

Conference	2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013
Country/Territory	United States
City	Hilton Head Island, SC
Period	11/08/13 → 15/08/13

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

Cite this

@inproceedings{8f63d16e9483457b9813587de2fca01a,

title = "A robust control method of lunar orbit spacecraft autonomous rendezvous",

abstract = "The lunar orbital rendezvous is a key technique of lunar return mission. In this paper, the C-W relative dynamic model is established. The virtual target trajectory was segmented designed, allowing the chaser remain at the docking corridor. The H∞ sub-optimal theory was applied in controller design, restraining the interference and over much energy consumption. The mathematical simulation showed that the proposed control method have advantages of high-accuracy, low power consumption, strong robustness and rapidity. Finally, the real-time visualization platform was established to demonstrate the whole process of lunar orbit spacecraft autonomous rendezvous mission.",

author = "Yunyi Hou and Guangfu Ma and Jianwen Hou and Wenlong Li and Peng Shi",

year = "2014",

language = "英语",

isbn = "9780877036050",

series = "Advances in the Astronautical Sciences",

publisher = "Univelt Inc.",

pages = "467--475",

booktitle = "Astrodynamics 2013 - Advances in the Astronautical Sciences",

note = "2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013 ; Conference date: 11-08-2013 Through 15-08-2013",

}

Hou, Y, Ma, G, Hou, J, Li, W & Shi, P 2014, A robust control method of lunar orbit spacecraft autonomous rendezvous. in Astrodynamics 2013 - Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference. Advances in the Astronautical Sciences, vol. 150, Univelt Inc., pp. 467-475, 2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013, Hilton Head Island, SC, United States, 11/08/13.

A robust control method of lunar orbit spacecraft autonomous rendezvous. / Hou, Yunyi; Ma, Guangfu; Hou, Jianwen et al.
Astrodynamics 2013 - Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference. Univelt Inc., 2014. p. 467-475 (Advances in the Astronautical Sciences; Vol. 150).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - A robust control method of lunar orbit spacecraft autonomous rendezvous

AU - Hou, Yunyi

AU - Ma, Guangfu

AU - Hou, Jianwen

AU - Li, Wenlong

AU - Shi, Peng

PY - 2014

Y1 - 2014

N2 - The lunar orbital rendezvous is a key technique of lunar return mission. In this paper, the C-W relative dynamic model is established. The virtual target trajectory was segmented designed, allowing the chaser remain at the docking corridor. The H∞ sub-optimal theory was applied in controller design, restraining the interference and over much energy consumption. The mathematical simulation showed that the proposed control method have advantages of high-accuracy, low power consumption, strong robustness and rapidity. Finally, the real-time visualization platform was established to demonstrate the whole process of lunar orbit spacecraft autonomous rendezvous mission.

AB - The lunar orbital rendezvous is a key technique of lunar return mission. In this paper, the C-W relative dynamic model is established. The virtual target trajectory was segmented designed, allowing the chaser remain at the docking corridor. The H∞ sub-optimal theory was applied in controller design, restraining the interference and over much energy consumption. The mathematical simulation showed that the proposed control method have advantages of high-accuracy, low power consumption, strong robustness and rapidity. Finally, the real-time visualization platform was established to demonstrate the whole process of lunar orbit spacecraft autonomous rendezvous mission.

UR - https://www.scopus.com/pages/publications/84898961687

M3 - 会议稿件

AN - SCOPUS:84898961687

SN - 9780877036050

T3 - Advances in the Astronautical Sciences

SP - 467

EP - 475

BT - Astrodynamics 2013 - Advances in the Astronautical Sciences

PB - Univelt Inc.

T2 - 2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013

Y2 - 11 August 2013 through 15 August 2013

ER -

A robust control method of lunar orbit spacecraft autonomous rendezvous

Abstract

Publication series

Conference

UN SDGs

Other files and links

Fingerprint

Cite this