Fuzzy Logic-Based Aerodynamic Modeling with Continuous Differentiability

Table 2

The final main aerodynamic models of lateral-directional aerodynamics.

Coef.	𝛼	𝛽	𝜙	𝑝	𝑟	𝑘2	𝛿𝑎	𝛿𝑟	𝑀	𝛼̇	𝛽̇	𝑛	𝑅^2
𝐶𝑙	2	3	3	2	2	3	2	2	3	3	2	15552	0.9617
𝐶𝑛	3	2	4	2	2	2	3	3	2	2	2	13824	0.9435