https://github.com/pedroteixeiraw/missile_guidance_system
This project focuses on developing a Ground-to-Air Missile Guidance System using a triple-loop PID control structure in MATLAB/ Simulink.
https://github.com/pedroteixeiraw/missile_guidance_system
c control-theory guidance-system mathematics matlab missile-simulation physics pid-controller simulink
Last synced: 2 months ago
JSON representation
This project focuses on developing a Ground-to-Air Missile Guidance System using a triple-loop PID control structure in MATLAB/ Simulink.
- Host: GitHub
- URL: https://github.com/pedroteixeiraw/missile_guidance_system
- Owner: pedroteixeiraw
- Created: 2025-03-27T16:07:32.000Z (2 months ago)
- Default Branch: main
- Last Pushed: 2025-03-27T17:28:46.000Z (2 months ago)
- Last Synced: 2025-03-27T17:30:57.297Z (2 months ago)
- Topics: c, control-theory, guidance-system, mathematics, matlab, missile-simulation, physics, pid-controller, simulink
- Language: MATLAB
- Homepage:
- Size: 13.5 MB
- Stars: 0
- Watchers: 1
- Forks: 0
- Open Issues: 0
-
Metadata Files:
- Readme: README.md
Awesome Lists containing this project
README
# Missile Guidance System with PID Control
[
](https://www.youtube.com/watch?v=FXxbwfzK1f8)
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