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Estimation of Longitudinal Aerodynamic Derivatives Using Genetic Algorithm Optimized Method

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Figure

Table 1. Longitudinal Parameters of ATTAS aircraft (Simulated data -0% noise).
Figure 3. Scatter plots of longitudinal aerodynamic parameters – ATTAS aircraft (Simulated-10%).
Table 4. Longitudinal Parameters of ATTAS aircraft (Simulated data -15% noise).
Table 5. Longitudinal Parameters of ATTAS aircraft (Real flight data).
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