Thrust Vector Control for Model Rockets: A Beginner's Roadmap

Added:

TVC Basics
Hardware Setup
Core Components
Part Selection
Electronics Build
Software Logic
Control Theory
PID Explained
Conclusion
Q&A Session

TVC Basics

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Playing Section
  • 1

    Defines thrust vector control as a technique, not a physical object.

  • 2

    Explains methods like gimballing, jet vanes, and liquid injection.

  • 3

    Shows how vectored thrust changes the direction of a rocket's force.

Basic Rocketry Physics: Understanding Center of Gravity (CG), Center of Pressure (CP), and aerodynamic stability.
Fundamentals of Microcontrollers: Experience with hardware platforms like Arduino, including reading sensor inputs and outputting PWM signals to servos.
Introductory Programming (C/C++): Familiarity with basic coding structures, logic, and variables used in flight computer software.
Basic Vector Mathematics and Trigonometry: Comprehending forces, angles, and 3D coordinate systems to understand thrust redirection.
Sensor Fusion and State Estimation: Implementing Kalman Filters to combine accelerometer and gyroscope data for precise attitude estimation.
Advanced PID Tuning and Control Algorithms: Exploring gain scheduling, active roll control, or transitioning to Linear Quadratic Regulators (LQR).
Hardware-in-the-Loop (HIL) Testing: Simulating aerodynamic environments on hardware to test flight computers prior to physical launch.
High-Power Rocketry (HPR) Certification and Safety Regulations: Navigating official guidelines (such as NAR or Tripoli) for launching actively-guided rockets safely and legally.
326.9K views12.7Klikes50:12@BPSspaceOriginal Release: 2020-03-09

This video provides a comprehensive roadmap for building thrust vector controlled (TVC) model rockets, covering the fundamental concepts of TVC (changing thrust direction to stabilize rockets), practical implementation methods (gimbal mounts, jet vanes, liquid injection, paddle systems), flight computer components (microcontrollers, IMUs, barometers, MOSFETs), and the critical PID control algorithm (proportional-integral-derivative) for maintaining rocket stability. The presenter emphasizes starting small with 500-1000g rockets using cardboard airframes and F motors, implementing a state machine for flight phases, and carefully tuning PID gains for stable flight.