A model thrust vector control system to maneuver a rocket with tuned PID settings.
To Work On:
- Integrity (To handle 7 - 10Ns of force)
- Using bearings.
- Using heat Resistant and strong material.
- Structural integrity
- Offset Angles
- Speed
- Accuracy
- Range +-3 degrees
- Noise Damping
- Faster Response
- 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