[1]LIU Xiao-long,MA Sheng-gang.Simulation Research on Launch Performance of UAV Pneumatic Launch System[J].Journal of Zhengzhou University (Engineering Science),2013,34(05):55-58.[doi:10.3969/j. issn.1671 -6833.2013.05.012]
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Journal of Zhengzhou University (Engineering Science)[ISSN
1671-6833/CN
41-1339/T] Volume:
34
Number of periods:
2013 05
Page number:
55-58
Column:
Public date:
2013-09-10
- Title:
-
Simulation Research on Launch Performance of UAV Pneumatic Launch System
- Author(s):
-
LIU Xiao-long; MA Sheng-gang
-
School of Mechanical Engineering,Zhengzhou University ,Zhengzhou 450001,China
-
- Keywords:
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pneumatic launch system; bond graph; mathematical model; simulation model; launch perform-ance
- CLC:
-
TH412
- DOI:
-
10.3969/j. issn.1671 -6833.2013.05.012
- Abstract:
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This paper introduces the working principle of an Unmanned Aerial Vehicle ( UAV ) pneumaticlaunch system,which takes an air tank as power supply and a pulley block as growth mechanism. The mathe-matical model of the system is deduced by using the bond graph method. And the simulation model is estab-lished by using MATLAB. Through adjusting the design parameters of the system,the influence of these pa-rameters on the launch performance is obtained. The launch performance can be optimized by reasonable matc-hing of these parameters,which provides the theoretical guidance for this system.