Optimal reconfiguration with collision avoidance for a granular spacecraft using laser pressure

被引:4
|
作者
Zhang, Kunpeng [1 ]
Zhang, Yao [1 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
关键词
Granular spacecraft; Collision avoidance; Optimal transport; Voronoi partitioning; Laser pressure; MULTIPLE SPACECRAFT; PARTICLES; BINDING;
D O I
10.1016/j.actaastro.2019.04.021
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Granular spacecraft, as a new type of distributed spacecraft system, "are complex multibody systems composed of a spatially disordered distribution of a large number of elements" (Quadrelli et al., 2013), designed and controlled to perform certain desired functions. To achieve the collision-free reconfiguration of granular spacecraft, an optimal reconfiguration algorithm with collision avoidance for a granular spacecraft using laser pressure is presented in this paper. The three-dimensional model of granular spacecraft using laser pressure is established first, and the reconfiguration problem statement is presented. The optimal reconfiguration plan is designed based on optimal transport, and the collision-free trajectories for all the particles are generated based on Voronoi partitioning, with the motion constraints under the control of laser pressure. Finally, the numerical simulations are provided to demonstrate the effectiveness of the proposed reconfiguration algorithm and the feasibility of using laser actuators for the reconfiguration of a granular spacecraft.
引用
收藏
页码:163 / 174
页数:12
相关论文
共 50 条
  • [1] Optimal Spacecraft Formation Reconfiguration with Collision Avoidance Using Particle Swarm Optimization
    Huang, Haibin
    Zhuang, Yufei
    Ma, Guangfu
    Lv, Yueyong
    [J]. INFORMATION TECHNOLOGY AND CONTROL, 2012, 41 (02): : 143 - 150
  • [2] Spacecraft formation reconfiguration with collision avoidance
    Schlanbusch, Rune
    Kristiansen, Raymond
    Nicklasson, Per J.
    [J]. AUTOMATICA, 2011, 47 (07) : 1443 - 1449
  • [3] Spacecraft Formation Reconfiguration with Dynamic Collision Avoidance
    Schlanbusch, Rune
    Oland, Espen
    [J]. 2013 IEEE AEROSPACE CONFERENCE, 2013,
  • [4] Underactuated spacecraft formation reconfiguration with collision avoidance
    Huang, Xu
    Yan, Ye
    Zhou, Yang
    [J]. ACTA ASTRONAUTICA, 2017, 131 : 166 - 181
  • [5] Energy- and time-optimal reconfiguration of spacecraft clusters with collision avoidance
    Huang, Yong
    Sun, Silang
    Chu, Jing
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2023, 237 (13) : 3045 - 3061
  • [6] Distributed RISE control for spacecraft formation reconfiguration with collision avoidance
    Guo, Yaohua
    Zhou, Jun
    Liu, Yingying
    [J]. JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2019, 356 (10): : 5332 - 5352
  • [7] Multiple Spacecraft Formation Reconfiguration Planning with Nonconvex Collision Avoidance Constraints
    Zhou, Ding
    Hu, Yuting
    Li, Shunli
    [J]. 2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2016, : 643 - 647
  • [8] Multiple-Spacecraft Reconfiguration Through Collision Avoidance, Bouncing, and Stalemate
    Y. Kim
    M. Mesbahi
    F. Y. Hadaegh
    [J]. Journal of Optimization Theory and Applications, 2004, 122 : 323 - 343
  • [9] Multiple-spacecraft reconfiguration through collision avoidance, bouncing, and stalemate
    Kim, Y
    Mesbahi, M
    Hadaegh, FY
    [J]. JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS, 2004, 122 (02) : 323 - 343
  • [10] Optimal control of spacecraft for close proximity with collision avoidance
    Ni, Qing
    Feng, Licheng
    Huang, Yiyong
    [J]. 2016 3RD INTERNATIONAL CONFERENCE ON INFORMATION SCIENCE AND CONTROL ENGINEERING (ICISCE), 2016, : 1019 - 1023