Commercial Aircraft Dynamic Flight Simulation with Optimal Control

A comprehensive commercial aircraft dynamic flight simulation program implementing optimal control for longitudinal motion

Simulink Vehicle Full-Vehicle Modeling

MATLAB-based Simulink vehicle full-vehicle modeling incorporating seven degrees of freedom (DoF), including longitudinal motion, lateral motion, yaw motion, and wheel rotation (4 DoF)

Grumman Aerospace F-14 Tomcat Flight Control Simulation

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.