Thrust-Vector-Control-Rocket

A model thrust vector control system to maneuver a rocket with tuned PID settings.

TVC Development

Version 1

To Work On:

Integrity (To handle 7 - 10Ns of force)
Using bearings.
Using heat Resistant and strong material.

Design TVC 2.0

Improvements:

Structural integrity
Offset Angles

Control System Design:

Requirements

Speed
Accuracy
Range +-3 degrees
Noise Damping
Faster Response

System Characteristics

Nonlinear control design
Closed loop
Rotational system
Discrete data
Time-varying system
The mass of the object decreases as fuel on board is being consumed during flight.

Sources:

Control Systems Engineering - Norman S. Nise