Full Text:   <3046>

CLC number: V249.121

On-line Access: 2012-11-02

Received: 2012-03-26

Revision Accepted: 2012-07-31

Crosschecked: 2012-10-12

Cited: 3

Clicked: 5632

Citations:  Bibtex RefMan EndNote GB/T7714

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Journal of Zhejiang University SCIENCE C 2012 Vol.13 No.11 P.859-865


Turning mechanism and composite control of stratospheric airships

Author(s):  Mao-hua Zhang, Deng-ping Duan, Li Chen

Affiliation(s):  Institute of Aerospace Science and Technology, Shanghai Jiao Tong University, Shanghai 200240, China; more

Corresponding email(s):   superzhangmaohua@126.com, chenli2006@163.com

Key Words:  Stratospheric airships, Horizontal turn, Composite control, Control allocation, Vectored thrust

Mao-hua Zhang, Deng-ping Duan, Li Chen. Turning mechanism and composite control of stratospheric airships[J]. Journal of Zhejiang University Science C, 2012, 13(11): 859-865.

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%DOI 10.1631/jzus.C1200084

T1 - Turning mechanism and composite control of stratospheric airships
A1 - Mao-hua Zhang
A1 - Deng-ping Duan
A1 - Li Chen
J0 - Journal of Zhejiang University Science C
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DOI - 10.1631/jzus.C1200084

The parametric model of stratospheric airships is established in the body axes coordinate system. In this paper we study the turning mechanism of stratospheric airships including the generated forces and the key parameters for steady turning. We compare and analyze the different driven-characteristics between aerodynamic control surfaces and vectored thrust in turning. We design a composite control combining aerodynamic control surfaces and vectored thrust according to different dynamic pressure conditions, to achieve coordinated turning under high or low airspeed situations.

Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article


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