Approach for Vertical Loading Error Compensation for Wheel Test Bench of Lunar Rover Vehicle

被引:0
|
作者
Gao, Haibo [1 ]
Liang, Zhongchao [1 ]
Ding, Liang [1 ]
Deng, Zongquan [1 ]
机构
[1] Harbin Inst Technol, State Key Lab Robot & Syst, Harbin 150080, Peoples R China
来源
JOURNAL OF THE CHINESE SOCIETY OF MECHANICAL ENGINEERS | 2013年 / 34卷 / 06期
基金
中国国家自然科学基金;
关键词
Lunar roving vehicle; Terramechanics; Wheel testing bench; Torsion spring loading;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A lunar roving vehicle (LRV) is the key for manned lunar explorations and for supporting a lunar base. It is therefore necessary for the maneuverability and adaptability to the environment of its wheels to be known during the design phase. Toward this end, it is essential to build a test bench for LRV wheels. A torsion spring loading mechanism with a parallelogram linkage instead of a counterweight enables continuous vertical loading of the testing wheel and reduces the inertia and start-up time of the testing wheel. However, the vertical load during transition from the initial stationary state to the stable movement state contains an error because of slip sinkage. The variation of sinkage leads to variations in the vertical displacement of the testing wheel, causing changes in the torque of the torsion spring and in turn causing vertical loading errors in the wheel. In this study, the vertical loading error of a testing wheel loaded by a torsion spring was analyzed, and an error compensation algorithm was deduced theoretically. Finally, highly accurate vertical loading of the wheel test bench for an LRV was realized. This should lay the foundation for future wheel experiments of LRVs.
引用
收藏
页码:561 / 569
页数:9
相关论文
共 28 条
  • [1] Approach for vertical loading error compensation for wheel test bench of lunar rover vehicle
    Liang, Z., 2013, Chinese Mechanical Engineering Society (34):
  • [2] Simulation test on lunar dust raising by lunar rover wheel
    Li, Man
    Tian, Dong-Bo
    Bai, Yu
    Wang, Zhi-Hao
    Yu, Qiang
    Li, Yu
    DESIGN, MANUFACTURING AND MECHATRONICS (ICDMM 2015), 2016, : 35 - 40
  • [3] Inertia force compensation strategy for loading system of a vehicle steering test bench
    Chen S.
    Luo Y.
    Mai Y.
    Liu D.
    Mai, Yunfei, 1600, Chinese Vibration Engineering Society (36): : 242 - 246
  • [4] Structural Analysis of Flexible Metal Wheel in the Application of Lunar Rover Vehicle
    Nasaruddin, Muhammad Hakim
    Basri, Adi Azriff
    Basri, Ernnie Illyani
    Sultan, Mohamed Thariq Haji Hameed
    Ahmad, Kamarul Arifin
    JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION, 2023, 55 (01): : 1 - 12
  • [5] Prediction of tractive performance of wheel on moon surface for lunar rover vehicle
    Sun, Peng
    Gao, Feng
    Yao, Sheng-Zhuo
    Li, Wen
    Jilin Daxue Xuebao (Gongxueban)/Journal of Jilin University (Engineering and Technology Edition), 2010, 40 (04): : 925 - 930
  • [6] Four-Wheel Rover Performance Analysis at Lunar Analog Test
    Britton, Nathan
    Walker, John
    Yoshida, Kazuya
    Shimizu, Toshiro
    Paniccia, Tommaso
    Nakata, Kei
    FIELD AND SERVICE ROBOTICS: RESULTS OF THE 10TH INTERNATIONAL CONFERENCE, 2016, 113 : 361 - 371
  • [7] Analysis and Test of the Driving Wheel of Planetary Rover in Simulated Lunar Surface
    Huang, Yuxin
    Wang, Tongyu
    Lin, Lin
    Wang, Limeng
    Zhang, Hu
    ADVANCES IN MACHINING AND MANUFACTURING TECHNOLOGY XII, 2014, 589-590 : 701 - 707
  • [8] Design and Test of an Electromechanical Rover Tether for the Exploration of Vertical Lunar Pits
    McGarey, Patrick
    Tien Nguyen
    Pailevanian, Torkom
    Nensas, Issa
    2020 IEEE AEROSPACE CONFERENCE (AEROCONF 2020), 2020,
  • [9] TRACTIVE PERFORMANCE ANALYSIS ON RADIALLY DEPLOYABLE WHEEL CONFIGURATION OF LUNAR ROVER VEHICLE BY DISCRETE ELEMENT METHOD
    Li Wen
    Gao Feng
    Jia Yang
    CHINESE JOURNAL OF MECHANICAL ENGINEERING, 2008, 21 (05) : 13 - 18
  • [10] TRACTIVE PERFORMANCE ANALYSIS ON RADIALLY DEPLOYABLE WHEEL CONFIGURATION OF LUNAR ROVER VEHICLE BY DISCRETE ELEMENT METHOD
    LI Wen School of Aeronautic Science and Technology
    Chinese Journal of Mechanical Engineering, 2008, (05) : 13 - 18