Please submit manuscripts in either of the following two submission systems

    ScholarOne Manuscripts

  • ScholarOne

    • 勤云稿件系统

  • 登录

Search by Issue

  • 2024 Vol.31
  • 2023 Vol.30
  • 2022 Vol.29
  • 2021 Vol.28
  • 2020 Vol.27
  • 2019 Vol.26
  • 2018 Vol.25
  • 2017 Vol.24
  • 2016 vol.23
  • 2015 vol.22
  • 2014 vol.21
  • 2013 vol.20
  • 2012 vol.19
  • 2011 vol.18
  • 2010 vol.17
  • 2009 vol.16
  • No.1
  • No.2

Search by Keywords

  • Search by Title
  • Search by Keywords
  • Search by Abstract
  • Search by Author's Chinese Name
  • Search by Author's English Name
  • Search by Fund

News & AnnouncementMORE

Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

期刊网站二维码
微信公众号二维码
Related citation:GAO Hai-bo,DENG Zong-quan,DING Zhen-.Configuration and kinematics analysis of locking-releasing mechanism for side-loaded lunar rover[J].Journal of Harbin Institute Of Technology(New Series),2009,16(5):643-647.DOI:10.11916/j.issn.1005-9113.2009.05.009.
【Print】   【HTML】   【PDF download】   【View/Add Comment】  【Download reader】  【 Close 】
←Previous|Next→ Back Issue    Advanced Search
This paper has been: browsed 896times   downloaded 733times 本文二维码信息
码上扫一扫！
Shared by: Wechat More
Font:larger+|default|smaller-
Configuration and kinematics analysis of locking-releasing mechanism for side-loaded lunar rover
Author NameAffiliation
GAO Hai-bo quan (School of Mechatronic Engineering,Harbin Institute of Technology,Harbin 150001,China 
DENG Zong-quan quan (School of Mechatronic Engineering,Harbin Institute of Technology,Harbin 150001,China 
DING Zhen- quan (School of Mechatronic Engineering,Harbin Institute of Technology,Harbin 150001,China 
Abstract:
In order to save space for storing precision equipments,lower the center of mass of Lander and reduce lunar rover’s dimension constraint limited by mechanism of Lander,the locking-releasing mechanism of side-loaded lunar rover loaded outside Lander is presented,which is a kind of metamorphic mechanism.To ensure the working of this mechanism as the metamorphic process designed,configuration analysis of the locking-releasing mechanism is carried out,and topological structures are described by Huston lower numbered arrays.A kinematic mathematical model of the mechanism is established through homogeneous transformation matrix.The kinematic simulation validates the feasibility of the locking-releasing mechanism when the configurations are shifted from one to the other.
Key words:  lunar rover  locking-releasing mechanism  metamorphic mechanism  configuration analysis  kinematics analysis
DOI：10.11916/j.issn.1005-9113.2009.05.009
Clc Number:V476.3
Fund:

LINKS

Copyright © The Editorial Department of Journal of Harbin Institute of Technology
Address: 92 West Dazhi Street, Nan Gang District, Harbin, Heilongjiang Province, China Postcode: 150001
(C)2015 JOURNAL OF HIT ALL RIGHTS RESERVED. ICP. 0000423255