OPTIMAL CONTROL OF STRETCHING PROCESS OF SOLAR WINGS ON SPACECRAFT

GE Xinsheng; LIU Yanzhu

doi:10.11728/cjss1997.04.360

Volume 17 Issue 4

Dec. 1997

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Article Navigation > Chinese Journal of Space Science > 1997 > 17(4): 360-366

GE Xinsheng, LIU Yanzhu. OPTIMAL CONTROL OF STRETCHING PROCESS OF SOLAR WINGS ON SPACECRAFT[J]. Chinese Journal of Space Science, 1997, 17(4): 360-366. doi: 10.11728/cjss1997.04.360

Citation:

GE Xinsheng, LIU Yanzhu. OPTIMAL CONTROL OF STRETCHING PROCESS OF SOLAR WINGS ON SPACECRAFT[J]. Chinese Journal of Space Science, 1997, 17(4): 360-366. doi: 10.11728/cjss1997.04.360

GE Xinsheng, LIU Yanzhu. OPTIMAL CONTROL OF STRETCHING PROCESS OF SOLAR WINGS ON SPACECRAFT[J]. Chinese Journal of Space Science, 1997, 17(4): 360-366. doi: 10.11728/cjss1997.04.360

Citation:

GE Xinsheng, LIU Yanzhu. OPTIMAL CONTROL OF STRETCHING PROCESS OF SOLAR WINGS ON SPACECRAFT[J]. Chinese Journal of Space Science, 1997, 17(4): 360-366. doi: 10.11728/cjss1997.04.360

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OPTIMAL CONTROL OF STRETCHING PROCESS OF SOLAR WINGS ON SPACECRAFT

doi: 10.11728/cjss1997.04.360 cstr: 32142.14.cjss1997.04.360

GE Xinsheng¹,
LIU Yanzhu²

1.
Basic Science Courses Department, Beijing Institute of Machinery Industry 100085
2.
Department of Engineering Mechanics, Shanghai Jiao Tong University

Received Date: 1996-10-23
Rev Recd Date: 1997-03-08
Publish Date: 1997-12-24

Abstract

Abstract

The optimal attitud control problem of speecraf during the sbetehing Process ofsolar wings is discussed in mis paper Amathematical model of the systom isestabished by use of the mulhbody dynamics and oPtical control theory. An algorithmof contro for the stretching process is proposed, considering the nonhlonomic behavior of the system. The effectiveness of the apprach is shown by numerical simulation.
- Mulhbody dynamics,
- Optimal control,
- Attitude control,
- Stretching of solar wings