Missile Guidance System with PID Control

This project focuses on developing a Ground-to-Air Missile Guidance System using a triple-loop PID control structure in MATLAB/ Simulink.
The following image illustrates the implementation of the autopilot acceleration control system.

For mission success, the ground-to-air missile must intercept the target within a minimal distance of 5 meters and detonate.

All additional information can be obtained in the following files:

1. Missile Orientation Control (Briefing), 1_report_briefing.pdf
2. Missile Orientation Control (Theory), 2_report_theory.pdf
3. Missile Orientation Control (MATLAB File), 3_report_matlab.pdf
4. Simulation Report, 4_report_simulation.pdf

Tech Stack: MATLAB, C, Control Theory, PID Controllers, Mathematics, Physics