Journal of the Korean Society for Aviation and Aeronautics (한국항공운항학회지)

The Korean Society for Aviation and Aeronautics (한국항공운항학회)
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Development of 4-D Trajectory Modeling using BADA

BADA를 활용한 4-D 경로 모델링법 개발

  • 오은미 (한국항공우주연구원 교통.항법기술연구센터) ;
  • 은연주 (한국항공우주연구원 교통.항법기술연구센터) ;
  • 전대근 (한국항공우주연구원 교통.항법기술연구센터)
  • Received : 2012.05.24
  • Accepted : 2012.06.04
  • Published : 2012.06.30
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Abstract

Four dimensional(4-D) trajectory modeling is conducted based on flight plan. The flight plan is divided into several segments which represent certain operating flight modes. Thrust, drag and fuel consumption rate of an aircraft are calculated using BADA provided by Eurocontrol. The trajectory is modeled with the rate of climb/descent calculated with Total-Energy Equation. The simulation results with a typical aircraft and its flight plan indicate that the trajectory modeled corresponds well with the suggested flight plan. The performance profiles including total endurance time and time history for speed, thrust, drag and fuel consumption were also appropriately generated.

Keywords

References

  1. A. Nuic, "User Manual for The Base of Aircraft Data(BADA) Revision 3.8," Eurocontrol Experimental Centre, France, 2010, pp. 5-28.
  2. Vincent Mouillet, "Use of Radar Data to Improve Modeling of Aircraft Operational Factors," BADA User Group Meeting, 2010.
  3. M. D. Dupuy, and M. Porretta, "Preliminary Results for A Robust Trajectory Prediction Method using Advanced Flight Data," Digital Avionics Systems Conference, Dallas, TX, 2007, pp.1.C.5-3-1.C.5-6.
  4. Y. Fukuda, M. Shirakawa, A. Senoguchi, "Development of Trajectory Prediction Model," ENRI International Workshop on ATM/CNS, Tokyo, Japan, 2010, pp.97.
  5. T. A. Becher, "Development of an FMS Flyability Model for Terminal RNAV Procedure Design," AIAA's Aircraft Technology, Integration, and Operations(ATIO) 2002 Technical, Los Angelos, CA, Oct. 2002, pp. 8-9.

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