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Deployment and control of spacecraft solar array considering joint stick-slip friction

  • Published:2015-04 Issue: Volume:42 Page:342-352
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Li Hai-Quan,Liu Xiao-Feng,Duan Liu-Cheng,Cai Guo-Ping

Funder

National Natural Science Foundation of China

Shanghai Municipal Education Commission

Natural Science Foundation of Shanghai

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference15 articles.

1. Attitude motion of spacecraft during oblique solar panel deployment;Bai;Aircr. Eng. Aerosp. Technol.,2012

2. Study on the behavior of solar array deployment with root hinge drive assembly;Ding;Chin. J. Aeronaut.,2012

3. On the modeling and simulation of friction;Haessig;J. Dyn. Syst. Meas. Control,1991

4. Computational Dynamics of Multibody Systems;Hong,1999
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