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.