F16 Six-Degree-of-Freedom Nonlinear Aerodynamic Model
A six-degree-of-freedom nonlinear aerodynamic model for F16 aircraft flight control and simulation, developed using MATLAB with implementation of aerodynamic coefficients and dynamic equations
Explore MATLAB source code curated for "气动模型" with clean implementations, documentation, and examples.
A six-degree-of-freedom nonlinear aerodynamic model for F16 aircraft flight control and simulation, developed using MATLAB with implementation of aerodynamic coefficients and dynamic equations