Design and Simulation of On-Orbit Assembly System Based on Insect-Inspired Transportation

被引:4
|
作者
Shi, Yuetian [1 ]
Hou, Xuyan [1 ]
Gao, Guowei [1 ]
Na, Zhonglai [1 ]
Liu, Yuhui [1 ]
Deng, Zongquan [1 ]
机构
[1] Harbin Inst Technol, Aerosp Mfg Engn Dept, Harbin 150001, Peoples R China
关键词
on-orbit assembly; dynamic modeling; space robot; flexible deformation; SPACE SOLAR POWER; ANTENNA; ARCHITECTURES; TENSEGRITY;
D O I
10.3390/biomimetics8020256
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In response to the requirements of large-scale space in-orbit assembly and the special environment of low gravity in space, this paper proposes a small robot structure with the integration of assembly, connection, and vibration reduction functionalities. Each robot consists of a body and three composite mechanical arms-legs, which can dock and transfer assembly units with the transport spacecraft unit, and also crawl along the edge truss of the assembly unit to a designated location to complete in-orbit assembly while ensuring precision. A theoretical model of robot motion was established for simulation studies, and in the research process, the vibration of the assembly unit was studied, and preliminary adjustments were made to address the vibration issue. The results show that this structure is feasible for in-orbit assembly schemes and has good adjustment ability for flexible vibration.
引用
收藏
页数:15
相关论文
共 50 条
  • [31] A Copula Based Approach to On-orbit Satellite Breakup Simulation
    Wang Tieyan
    Huang Hai
    Jia Guanghui
    PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2, 2010, : 760 - 764
  • [32] On-orbit assembly trajectory plan based on improved genetic algorithm
    Sun C.
    Wu X.
    Xie Y.
    Song T.
    Sun J.
    Wang Z.
    Wu, Xiande (xiande_wu@163.com), 1600, Editorial Board of Journal of Harbin Engineering (38): : 1167 - 1172
  • [33] Design and on-orbit status of the trigger system for the DAMPE mission
    Yong-Qiang Zhang
    Jian-Hua Guo
    Yang Liu
    Chang-Qing Feng
    Yun-Long Zhang
    Tie-Kuang Dong
    Jing-Jing Zang
    Chuan Yue
    ResearchinAstronomyandAstrophysics, 2019, 19 (09) : 13 - 20
  • [34] The parallel crank-rocker flapping mechanism: An insect-inspired design for micro air vehicles
    Conn, Andrew T.
    Burgess, Stuart C.
    Ling, Chung Seng
    INTERNATIONAL JOURNAL OF HUMANOID ROBOTICS, 2007, 4 (04) : 625 - 643
  • [35] A critical review of micro-scale pumping based on insect-inspired membrane kinematics
    Tripathi, Dharmendra
    Bhandari, D. S.
    Beg, O. Anwar
    SENSORS AND ACTUATORS A-PHYSICAL, 2023, 360
  • [36] Component Encoding and Fiducial Marker System Design for the On-orbit Intelligent Assembly of Modular Space Truss Structure
    Hu J.
    Zhao C.
    Guo W.
    Jixie Gongcheng Xuebao/Journal of Mechanical Engineering, 2021, 57 (15): : 15 - 22
  • [37] Simulation platform to design and validate control laws for a space manipulator system performing on-orbit servicing
    Kraiem, Sofiane
    Rognant, Mathieu
    Waitman, Sergio
    2024 INTERNATIONAL CONFERENCE ON SPACE ROBOTICS, ISPARO, 2024, : 98 - 103
  • [38] A new procedural for the integration of the HIL simulation system for on-orbit docking
    Chang, Tongli
    Cong, Dacheng
    Ye, Zhengmao
    Han, Junwei
    2007 IEEE INTERNATIONAL CONFERENCE ON INTEGRATION TECHNOLOGY, PROCEEDINGS, 2007, : 769 - +
  • [39] Ground Simulation System of On-orbit Releasing Satellite Motion and Control
    Han Fei
    Liang Yan
    Qi Quan
    Qi Naiming
    Xia Qi
    2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 8775 - 8779
  • [40] Optimal Orbit Design and Mission Scheduling for Sun-Synchronous Orbit On-Orbit Refueling System
    Han, Peng
    Guo, Yanning
    Wang, Pengyu
    Li, Chuanjiang
    Pedrycz, Witold
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2023, 59 (05) : 4968 - 4983