Modeling and Simulation Research on Tailless Unmanned Aerial Vehicle

2006 ◽  
Author(s):  
Yong Fan ◽  
Ji-hong Zhu ◽  
Jia-qiang Zhu ◽  
Zeng-qi Sun
Keyword(s):  
Modeling And Simulation ◽  
Unmanned Aerial Vehicle ◽  
Simulation Research ◽  
Aerial Vehicle

scholarly journals Research of Pneumatic Distributors for Launcher of Unmanned Aerial Vehicle (UAV)

2017 ◽  
Vol 43 (1) ◽  
pp. 249-276
Author(s):  
Paweł Szczepaniak ◽  
Michał Jóźko
Keyword(s):  
Unmanned Aerial Vehicle ◽  
Design Process ◽  
Flow Characteristic ◽  
Flow Characteristics ◽  
Flow Simulation ◽  
Test Stand ◽  
Simulation Research ◽  
Aerial Vehicle

Abstract The test stand for investigations of flow characteristics of pneumatic distributor has been presented in this paper. This test stand has been composed as requirements include in standard PN-92/M-73763. The results of experimental and simulation investigations for standard five ways and two position pneumatic distributor have been presented. In simulations have been used CFD of SolidWorks Flow Simulation application. Flow characteristic of pneumatic distributor is necessary for design process of special pneumatic circuits of UAV launchers. CFD methods allow specify flow characteristics. Simulation research allow effective pneumatic components modification, whose used of special pneumatic circuits of UAV launchers. Results of experimental and simulation investigations were analyzed and compared.

The Modeling and Simulation of UAV Pneumatic Launch System

2013 ◽  
Vol 299 ◽  
pp. 27-30
Author(s):  
Xiao Long Liu ◽  
Chuang Na Xia ◽  
Sheng Gang Ma
Keyword(s):  
Mathematical Model ◽  
Modeling And Simulation ◽  
Unmanned Aerial Vehicle ◽  
Future Development ◽  
Theoretical Foundation ◽  
Bond Graph ◽  
Inflation Pressure ◽  
Work Process ◽  
Aerial Vehicle ◽  
The Mathematical Model

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.

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