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Validation of Mathematical Models of UAV by Using the Parameter Estimation for Nonlinear System

비선형 시스템식별에 의한 무인비행기의 수학적 모델 적합성

  • 이환 (한국항공우주연구원 첨단비행제어팀) ;
  • 최형식 (한국항공우주연구원 첨단비행제어팀) ;
  • 성기정 (한국항공우주연구원 첨단비행제어팀)
  • Published : 2007.10.01

Abstract

The sophisticated mathematical model is required for the design and the database construction of the advanced flight control system of UAV. In this paper, flight test of KARI's research UAV, often called DURUMI-II, is implemented for the data acquisition from the maneuver flight. The flight path reconstruction is implemented to ensure that the measured data is consistent and error free. The nonlinear system identification for the refined mathematical modeling is implemented with the verified measurements from the flight path reconstruction. The simulation with the identified results have a good validation when the simulated responses were compared to the flight tested data.

Keywords

References

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