Fuzzy Logic-Based Aerodynamic Modeling with Continuous Differentiability

Table 1

The final main aerodynamic models of longitudinal aerodynamics.

Coef.	𝛼	𝛼̇	𝑞	𝑘1	𝛽	𝛿𝑒	𝑀	𝑝	𝑞	𝑛	𝑅^2
𝐶𝑧	2	3	3	2	3	3	2	3	2	3888	0.9618
𝐶𝑚	2	2	3	4	2	3	2	2	3	3456	0.9873