The Modeling and Simulation of UAV Pneumatic Launch System

Author:

Liu Xiao Long1,Xia Chuang Na2,Ma Sheng Gang1

Affiliation:

1. Zhen Zhou University

2. Zhengzhou University

Abstract

This paper is based on the Bond Graph method to establish the mathematical model of UAV (Unmanned Aerial Vehicle) pneumatic launch system, simulates its work process through using MATLAB software, analyzes the influence of changing air tank inflation pressure, air tank volume on launch performance, and draws some important conclusions, which can provide a theoretical foundation for the future development and improvement of the system.

Publisher

Trans Tech Publications, Ltd.

Reference5 articles.

1. Karnopp D C. State variables and pseudo bond graphs for compressible thermo-fluid systems [J]. ASME Journal of Dynamic Systems, Measurement, and Control, 1979, 101(3): 210-215.

2. Andrew Parr. Hydraulics and pneumatics: a technician´s and engineer´s guide [M]. Oxford: Elsevier, (2006).

3. Daxian Cheng. Mechanical design handbook: pneumatic drive [M]. Beijing: chemical industry press, (2004).

4. Defeng Zhang, Wenyin Yang. MATLAB simulation technology and application: Tsinghua university press, (2012).

5. Yan Li, Yunlong Zhou. The Use of Bonded Diagram Method in an Aerodynamic System: Journal of Engineering for Thermal Energy & Power, (1999).

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