MODEL ROCKET

This model rocket project focuses on implementing thrust vector control (TVC) technology to achieve stable and controlled flight. Unlike traditional model rockets that rely on fins for passive stabilization, this project uses active control of the rocket engine's direction to maintain stability and enable more complex flight paths.

I've learned a lot about multiple disciplines of engineering while working on this project, like mechanical, electrical, and embedded software engineering. I've also learned a lot about the importance of design and simulation in the engineering process.

The rocket incorporates several technical systems working together to achieve controlled flight:

• Gimbal-mounted motor for two-axis thrust vectoring
• Flight computer for real-time control
• IMU (Inertial Measurement Unit) with accelerometer and gyroscope
• Custom PID control algorithms for flight stabilization
• 3D printed structural components for weight optimization
• Telemetry system for real-time data transmission
• Redundant deployment systems for recovery parachutes
• Custom PCB design for electronics integration

The rocket design balances several key factors:

• Weight distribution for proper center of gravity
• Aerodynamic stability during powered and unpowered flight
• Structural integrity to withstand launch forces
• Electronics bay thermal management
• Modular construction for easy maintenance and modification
• Recovery system reliability and redundancy

The development of this model rocket follows an iterative engineering approach, starting with design and simulation, followed by component testing, and culminating in full flight tests. The process includes:

• CAD modeling of all mechanical components
• Static thrust testing of the engine and gimbal system
• Control algorithm development and tuning
• Flight software simulations
• Electronics integration and testing
• Ground testing of all systems
• Flight testing with data collection and analysis
• Iterative improvements based on test results

This project is currently under development, with detailed documentation and code to be published upon completion of initial flight tests.