제어로봇시스템학회:학술대회논문집
- 제어로봇시스템학회 2004년도 ICCAS
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- Pages.383-388
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- 2004
System Identification of Aerodynamic Coefficients of F-16XL (ICCAS 2004)
- Seo, In-Yong (Korea Electric Power Research Institute) ;
- Pearson, Allan E. (Department of Engineering, Brown University)
- 발행 : 2004.08.25
초록
This paper presents the aerodynamic coefficient modeling with a new model structure explored by Least Squares using Modulating Function Technique (LS/MFT) for an F-16XL airplane using wind tunnel data supplied by NASA/LRC. A new model structure for aerodynamic coefficient was proposed, one that considered all possible combination terms of angle of attack