Aerodynamic Model Analysis and Flight Simulation Research of UAV Based on Simulink

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ISSN Print: 1945-3116
ISSN Online: 1945-3124

Website: https://www.scirp.org/journal/jsea
E-mail: jsea@scirp.org

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Submission

"Aerodynamic Model Analysis and Flight Simulation Research of UAV Based on Simulink"
written by Chao Yun, Xiao-Min Li,
published by Journal of Software Engineering and Applications, Vol.6 No.2, 2013

has been cited by the following article(s):

[1]	Karakteristik Aerodinamika Flying Boat pada Ketinggian Ground Effect (Studi Kasus Model Remote Control Flying Boat Pada Ketinggian 0, 2 m dan 1 m)
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[2]	UAV engine fault and diagnosis with parameter models based on telemetry data
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[3]	Adaptive Backstepping Approach For Longitudinal Control Of Aircraft Unmanned Aerial Vehicles
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[4]	Adaptive Back stepping Approach for Longitudinal Control of Aircraft Unmanned Aerial Vehicles
	International Advanced Research Journal in Science, Engineering and Technology, 2016

[5]	Design and Implementation of a Control and Navigation System for a Small Unmanned Aerial Vehicle
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[6]	Particle System Modelling and Dynamic Simulation of a Tethered Rigid Wing Kite for Power Generation
	2016

[7]	Design of Longitudinal Motion Controller of a Small Unmanned Aerial Vehicle
	2015

[8]	Implementation of Spring Parameters with Computer Based Simulation Process–A Review
	International Journal of Science and Research, 2015

[9]	The Aerodynamic Characteristics of A Flying Boat on the Ground Effect Altitude (Case Study: A Flying Boat Remote Control Model at 0,2 m and 1 m altitute)
	Jurnal Perhubungan Udara, 2015

[10]	Identification, Modeling and Control of Unmanned Aerial Vehicles
	2014

[11]	Identification, Modeling and Control of Unmanned Aerial Vehicles.
	International Journal of Advanced Science & Technology, 2014

[12]	Synthesis of SimMechanics Model of Quadcopter Using SolidWorks CAD Translator Function

[1]	New Methodology for Longitudinal Flight Dynamics Modelling of the UAS-S4 Ehecatl towards its Aerodynamics Estimation Modelling AIAA Modeling and Simulation Technologies Conference, 2017 DOI:10.2514/6.2017-0807

[2]	UAV engine fault and diagnosis with parameter models based on telemetry data 2017 Prognostics and System Health Management Conference (PHM-Harbin), 2017 DOI:10.1109/PHM.2017.8079278

[3]	Design and Implementation of a Control and Navigation System for a Small Unmanned Aerial Vehicle IFAC-PapersOnLine, 2016 DOI:10.1016/j.ifacol.2016.11.155