Turning mechanism and composite control of stratospheric airships

Mao-hua ZHANG; Deng-ping DUAN; Li CHEN

doi:10.1631/jzus.C1200084

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Turning mechanism and composite control of stratospheric airships

计算机与自动化 | Updated：2022-12-09

- Turning mechanism and composite control of stratospheric airships
- Turning mechanism and composite control of stratospheric airships
- 信息与电子工程前沿（英文） 2012年13卷第11期页码：859-865
- 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：
  
  Project (No. 61175074) supported by the National Natural Science Foundation of China
- DOI：10.1631/jzus.C1200084
  中图分类号： V249.121
- 收稿：2012-03-26，
  
  修回：2012-10-12，
  
  纸质出版：2012-11
- Accepted：
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Turning mechanism and composite control of stratospheric airships[J]. 信息与电子工程前沿（英文）, 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.
Turning mechanism and composite control of stratospheric airships[J]. 信息与电子工程前沿（英文）, 2012,13(11):859-865. DOI： 10.1631/jzus.C1200084.

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

references

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