DEPLOYMENT DYNAMICS OF FLEXIBLE SOLAR ARRAYS CONSIDERING FRICTIONAL JOINT

Duan Liucheng; Li Haiquan; Liu Xiaofeng; Cai Guoping

doi:10.6052/0459-1879-14-152

Volume 46 Issue 6

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Article Navigation > Chinese Journal of Theoretical and Applied Mechanics > 2014 > 46(6): 957-970

Duan Liucheng, Li Haiquan, Liu Xiaofeng, Cai Guoping. DEPLOYMENT DYNAMICS OF FLEXIBLE SOLAR ARRAYS CONSIDERING FRICTIONAL JOINT[J]. Chinese Journal of Theoretical and Applied Mechanics, 2014, 46(6): 957-970. doi: 10.6052/0459-1879-14-152

Citation:

Duan Liucheng, Li Haiquan, Liu Xiaofeng, Cai Guoping. DEPLOYMENT DYNAMICS OF FLEXIBLE SOLAR ARRAYS CONSIDERING FRICTIONAL JOINT[J]. Chinese Journal of Theoretical and Applied Mechanics, 2014, 46(6): 957-970. doi: 10.6052/0459-1879-14-152

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DEPLOYMENT DYNAMICS OF FLEXIBLE SOLAR ARRAYS CONSIDERING FRICTIONAL JOINT

doi: 10.6052/0459-1879-14-152

Department of Engineering Mechanics, State Key Laboratory of Ocean Engineering, Shanghai Jiaotong University, Shanghai 200240, China

Funds: The project was supported by the Natural Science Foundation of China (11132001, 11272202), the Aviation Science Foundation of China (20120157002) and the Key Project of Shanghai Scientific Research (14ZZ021).

Received Date: 2014-05-30
Rev Recd Date: 2014-08-11
Publish Date: 2014-11-18

Abstract

Abstract

The deployment and locking of solar arrays of a free-floating spacecraft is studied in this paper. The rigid-flexible coupling dynamic model for describing the deployment and locking process is established using the Jourdain's velocity variational principle and the approach of forward recursive formulation. The contribution of joint friction to the dynamic equation of the system is derived based on the virtual power principle. The 3-D bristle friction model is introduced to study the influence of joint friction on the deployment dynamics of solar arrays. The validity of the proposed model is verified through the comparison of simulation results with those using the commercial software ADAMS and NASTRAN, and this model is available for predicting the deployment process of solar arrays and the attitude motion of spacecraft.
- flexible solar arrays,
- deployment dynamics,
- joint friction,
- forward recursive formulation,
- virtual power principle

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References(20)

References

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