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http://dx.doi.org/10.12673/jant.2016.20.5.387

Development and Validation of an Improved 5-DOF Aircraft Dynamic Model for Air Traffic Control Simulation  

Kang, Jisoo (Department of Aerospace Engineering, Inha University)
Oh, Hyeju (Department of Aerospace Engineering, Inha University)
Choi, Keeyoung (Department of Aerospace Engineering, Inha University)
Lee, Hak-Tae (Department of Aerospace Engineering, Inha University)
Publication Information
Journal of Advanced Navigation Technology / v.20, no.5, 2016 , pp. 387-393 More about this Journal
Abstract
To perform realistic air traffic control (ATC) simulation in various air traffic situations, an aircraft dynamic model that is accurate and efficient is required. In this research, an improved five degree of freedom (5-DOF) dynamic model with feedback control and guidance law is developed, which utilizes selected performance data and operational specifications from the base of aircraft data (BADA) and estimations using aircraft design techniques to improve the simulation fidelity. In addition, takeoff weight is estimated based on the aircraft type and flight plan to improve simulation accuracy. The dynamic model is validated by comparing the simulation results with recorded flight trajectories. An ATC simulation system using this 5-DOF model can be used for various ATC related research.
Keywords
5-Degree of freedom flight dynamic model; Base of aircraft data; Air traffic control simulation; Takeoff weight estimation; Trajectory validation;
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