Optimal orbit design of lunar modules soft landing

Jing Yang Zhou; Di Zhou; Guang Ren Duan

doi:10.1109/CHICC.2006.280951

Optimal orbit design of lunar modules soft landing

Jing Yang Zhou^*
, Di Zhou
, Guang Ren Duan

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

2 Scopus citations

Abstract

Precise three dimensional dynamics for lunar soft landing were presented. To realize the minimal fuel strategy, an optimal control law was proposed based on the maximum principle. By solving the two-point boundary value problem, the optimal trajectory of the lunar soft landing was obtained. Performance of the proposed control law was verified by simulation.

Original language	English
Title of host publication	2006 Chinese Control Conference Proceedings, CCC 2006
Pages	2226-2229
Number of pages	4
DOIs	https://doi.org/10.1109/CHICC.2006.280951
State	Published - 2007
Event	25th Chinese Control Conference, CCC 2006 - Harbin, China Duration: 7 Aug 2006 → 11 Aug 2006

Publication series

Name	2006 Chinese Control Conference Proceedings, CCC 2006

Conference

Conference	25th Chinese Control Conference, CCC 2006
Country/Territory	China
City	Harbin
Period	7/08/06 → 11/08/06

Keywords

Lunar module
Optimal trajectory
Soft lading

Access to Document

10.1109/CHICC.2006.280951

Cite this

@inproceedings{ebaef0711d1847e290539905f0a7f65c,

title = "Optimal orbit design of lunar modules soft landing",

abstract = "Precise three dimensional dynamics for lunar soft landing were presented. To realize the minimal fuel strategy, an optimal control law was proposed based on the maximum principle. By solving the two-point boundary value problem, the optimal trajectory of the lunar soft landing was obtained. Performance of the proposed control law was verified by simulation.",

keywords = "Lunar module, Optimal trajectory, Soft lading",

author = "Zhou, \{Jing Yang\} and Di Zhou and Duan, \{Guang Ren\}",

year = "2007",

doi = "10.1109/CHICC.2006.280951",

language = "英语",

isbn = "7810778021",

series = "2006 Chinese Control Conference Proceedings, CCC 2006",

pages = "2226--2229",

booktitle = "2006 Chinese Control Conference Proceedings, CCC 2006",

note = "25th Chinese Control Conference, CCC 2006 ; Conference date: 07-08-2006 Through 11-08-2006",

}

TY - GEN

T1 - Optimal orbit design of lunar modules soft landing

AU - Zhou, Jing Yang

AU - Zhou, Di

AU - Duan, Guang Ren

PY - 2007

Y1 - 2007

N2 - Precise three dimensional dynamics for lunar soft landing were presented. To realize the minimal fuel strategy, an optimal control law was proposed based on the maximum principle. By solving the two-point boundary value problem, the optimal trajectory of the lunar soft landing was obtained. Performance of the proposed control law was verified by simulation.

AB - Precise three dimensional dynamics for lunar soft landing were presented. To realize the minimal fuel strategy, an optimal control law was proposed based on the maximum principle. By solving the two-point boundary value problem, the optimal trajectory of the lunar soft landing was obtained. Performance of the proposed control law was verified by simulation.

KW - Lunar module

KW - Optimal trajectory

KW - Soft lading

UR - https://www.scopus.com/pages/publications/37349081224

U2 - 10.1109/CHICC.2006.280951

DO - 10.1109/CHICC.2006.280951

M3 - 会议稿件

AN - SCOPUS:37349081224

SN - 7810778021

SN - 9787810778022

T3 - 2006 Chinese Control Conference Proceedings, CCC 2006

SP - 2226

EP - 2229

BT - 2006 Chinese Control Conference Proceedings, CCC 2006

T2 - 25th Chinese Control Conference, CCC 2006

Y2 - 7 August 2006 through 11 August 2006

ER -

Optimal orbit design of lunar modules soft landing

Abstract

Publication series

Conference

Keywords

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