Explore MATLAB source code curated for "飞行控制" with clean implementations, documentation, and examples.
Application Context: Using the F16 model as an example, this program employs open-loop control techniques with MATLAB simulation, containing detailed aerodynamic parameters. The aircraft model is implemented using S-functions for high computational efficiency. Key Technology: Primarily utilizes MATLAB/Simulink for F16 modeling and flight condition simulation, featuring aerodynamic coefficient calculations and state-space representation of flight dynamics.
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
Unmanned Aerial Vehicle Flight Control Simulation Program utilizing MATLAB's Simulink module for dynamic model construction and flight simulation of UAVs, featuring mathematical modeling of aircraft dynamics and control system implementation.
This demonstration implements a longitudinal flight control system model for the Grumman Aerospace F-14 Tomcat, integrating first-order linear approximations of aircraft and actuator dynamics with an analog flight control architecture. The design utilizes pilot stick inputs for pitch attitude commands while incorporating pitch angle and pitch rate feedback. The implementation includes atmospheric turbulence modeling using a simplified Dryden wind gust model.
A high-fidelity six-degree-of-freedom nonlinear aerodynamic model for F-16 flight dynamics simulation
Classic F16 Flight Control Simulation with Aerodynamic Modeling and Control System Design
Mutual conversion between Euler angle control method and quaternion control method based on position coordinate transformation relationships using quaternions and Euler angles.