Formation flying of multiple spacecraft with autonomous rendezvous and docking capability

被引:16
|
作者
Wang, P. K. C. [1 ]
Hadaegh, F. Y.
机构
[1] Univ Calif Los Angeles, Dept Elect Engn, Los Angeles, CA 90095 USA
[2] CALTECH, Jet Prop Lab, Pasadena, CA 91109 USA
来源
IET CONTROL THEORY AND APPLICATIONS | 2007年 / 1卷 / 02期
关键词
D O I
10.1049/iet-cta:20050411
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The idea of incorporating autonomous rendezvous and docking (ARVD) capability into spacecraft flying in formation is explored. The situations where it is advantageous to incorporate ARVD capability into spacecraft formations are identified. Attention is focused on various potential problems pertaining to the control of multiple spacecraft with ARVD capability. Multiple-model-based control laws for formation acquisition and ARVD are developed using generic spacecraft models. In particular, the use of such control laws for simultaneous docking of multiple spacecraft in formation acquisition and reconfiguration is studied. Various optimal formation reconfiguration problems are briefly discussed. The effectiveness of the developed control laws is studied via computer simulation using a six-spacecraft formation model.
引用
收藏
页码:494 / 504
页数:11
相关论文
共 50 条
  • [31] Adaptive Control for Spacecraft Autonomous Rendezvous and Docking under 6-DOF Motion Constraints
    Dong, Hongyang
    Hu, Qinglei
    Akella, Maruthi R.
    2019 18TH EUROPEAN CONTROL CONFERENCE (ECC), 2019, : 2932 - 2937
  • [32] Autonomous rendezvous and docking sensor suite
    Tanner, E
    Granade, S
    Whitehead, CA
    LASER RADAR TECHNOLOGY AND APPLICATIONS VIII, 2003, 5086 : 329 - 339
  • [33] Optimal autonomous manoeuvre planning for spacecraft formation flying - Position assignment'
    Burgon, Ross
    Roberts, Peter C. E.
    Ankersen, Finn
    SPACEFLIGHT MECHANICS 2008, VOL 130, PTS 1 AND 2, 2008, 130 : 1015 - +
  • [34] Output Tracking Control for Autonomous Spacecraft Rendezvous
    Yang, Xuebo
    Bo, Yuming
    Liu, Yurong
    Ji, Zhijian
    Gao, Huijun
    PROCEEDINGS OF THE 48TH IEEE CONFERENCE ON DECISION AND CONTROL, 2009 HELD JOINTLY WITH THE 2009 28TH CHINESE CONTROL CONFERENCE (CDC/CCC 2009), 2009, : 5227 - 5232
  • [35] Autonomous spacecraft rendezvous with finite time convergence
    He, Shaoming
    Lin, Defu
    Wang, Jiang
    JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2015, 352 (11): : 4962 - 4979
  • [36] Autonomous navigation and rendezvous of spacecraft in lunar orbit
    Mikrin E.A.
    Mikhailov M.V.
    Rozhkov S.N.
    Gyroscopy and Navigation, 2010, 1 (04) : 310 - 320
  • [37] The Multiple coils to Perform Autonomous Rendezvous & Docking of CubeSat/micro-satellite
    Chen, Wenwen
    Mu, Zhongcheng
    Wang, Wei
    Sun, Guowen
    Chen, Hongyu
    2017 29TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2017, : 3178 - 3183
  • [38] Stochastic trajectory optimization for 6-DOF spacecraft autonomous rendezvous and docking with nonlinear chance constraints
    Zhang, Yanquan
    Cheng, Min
    Nan, Bin
    Li, Shunli
    ACTA ASTRONAUTICA, 2023, 208 : 62 - 73
  • [39] Mathematical modeling and simulation of nonlinear spacecraft rendezvous and formation flying problems via averaging method
    Ogundele, Ayansola D.
    Agboola, Olufemi A.
    Sinha, Subhash C.
    COMMUNICATIONS IN NONLINEAR SCIENCE AND NUMERICAL SIMULATION, 2021, 95
  • [40] Design and control of multiple spacecraft formation flying in elliptical orbits
    王鹏基
    杨涤
    Journal of Harbin Institute of Technology, 2005, (01) : 25 - 30