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Turning mechanism and composite control of stratospheric airships
- Turning mechanism and composite control of stratospheric airships
- Frontiers of Information Technology & Electronic Engineering Vol. 13, Issue 11, Pages: 859-865(2012)
- Affiliations：
1.Institute of Aerospace Science and Technology, Shanghai Jiao Tong University, Shanghai 200240, China
2.Institute of Aerospace Science and Technology Center of Ministry of Education, Shanghai 200240, China
- Author bio：
[ "Mao-hua ZHANG, E-mail: superzhangmaohua@126.com" ]
[ "Li CHEN, E-mail:chenli2006@163.com" ]
- Funds：
DOI：10.1631/jzus.C1200084
CLC： V249.121Received：26 March 2012，
Revised：2012-10-12，
Published：2012-11
- Accepted：
Scan QR Code
Mao-hua ZHANG, Deng-ping DUAN, Li CHEN. Turning mechanism and composite control of stratospheric airships[J]. Frontiers of Information Technology & Electronic Engineering, 2012, 13(11): 859-865.
Mao-hua ZHANG, Deng-ping DUAN, Li CHEN. Turning mechanism and composite control of stratospheric airships[J]. Frontiers of Information Technology & Electronic Engineering, 2012, 13(11): 859-865. DOI： 10.1631/jzus.C1200084.
摘要
Abstract
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.
关键词
Keywords
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