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平流层飞艇上升段高度控制方案

侯勇 杨军

兵工自动化2011,Vol.30Issue(3):73-74,89,3.
兵工自动化2011,Vol.30Issue(3):73-74,89,3.DOI:10.3969/j.issn.1006-1576.2011.03.023

平流层飞艇上升段高度控制方案

Height-Control Scheme of Stratospheric Airship Ascending Stage

侯勇 1杨军1

作者信息

  • 1. 西北工业大学航天学院,西安,710072
  • 折叠

摘要

Abstract

In order to better control stratospheric airship ascending stage and accelerate its ascending speed, construct the stratospheric airship 3-dimensional portrait dynamics equation. After analyze the problem of slow ascending speed of the semi-control scheme of ballonets, a new control scheme that depend on static lift, airscrew thrust and aerodynamic lift to ascend in the ascending stage is presented. According to these two schemes, the comparison controller is designed. The feasibility of the composite control scheme is tested by computer simulation.

关键词

飞艇/高度控制/控制方案/上升段

Key words

airship/ height-control/ control scheme/ ascending stage

分类

信息技术与安全科学

引用本文复制引用

侯勇,杨军..平流层飞艇上升段高度控制方案[J].兵工自动化,2011,30(3):73-74,89,3.

兵工自动化

OACSTPCD

1006-1576

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