Fly-by-Wire Control System for Fixed WIng Aircraft

The main goal of this project was to create a Simulink based fly-by-wire control system which can be then used to control a fixed-wing aircraft simulation model. The objectives were:

1. Design a roll, pitch, yaw damper.

2. Gain Optimization.

3. Modeling Autotrim function.

4. Gain mapping 

Figure: Roll Rate Command Model 

Figure: Gain Mapping