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IJSTR >> Volume 6 - Issue 4, April 2017 Edition



International Journal of Scientific & Technology Research  
International Journal of Scientific & Technology Research

Website: http://www.ijstr.org

ISSN 2277-8616



Longitudinal And Lateral Dynamic System Modeling Of A Fixed-Wing UAV

[Full Text]

 

AUTHOR(S)

Pann Nu Wai Lin, Nang Lao Kham, Hla Myo Tun

 

KEYWORDS

Longitudinal, Lateral, Transfer function, State Space System, Stability

 

ABSTRACT

In this paper presents work completed for flight characteristics, mathematical model of an aircraft are the focus. To construct the mathematical model, type of UAV and flying mode quality must be chosen firstly.Longitudinal command hold outputs and lateral outputs (slide slip velocity, yaw rate, heading angle, and roll angle) must be considered to control the desired flight conditions.

 

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