Design the Angle of Attack Autopilot design using MATLAB | MATLAB Solutions | MATLAB helpers
In this project we are going to design the Angle of Attack Autopilot design using MATLAB, we have to define the open loop state space model in workspace and create the close loop system using the LQR and pole placement technique with the objective of the maximum overshoot of 10% is permitted. The closed loop performance such as stability analysis, time response, gain and phase margins, controllability and observability analysis. Advanced control finds a significant application in the field of aircraft control. This particular project focuses on creating flight path feedback controllers for the Lockheed Martin F-16. The autopilot function of this aircraft is a crucial mode of relief for pilots as it enables the aircraft to maintain a steady flight path angle. The variable that requires control is the flight path angle, which is determined by the pitch angle (θ) and angle of attack (α), i.e., γ = θ − α. In this autopilot, the feedback controller has access to the state variables, and the elevator is the primary control surface used. Now we will create the script which will simulate the model and plot the results on figure and command window.
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