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Artificial Stability (Experimental)

uploaded by Vinarco 7 months ago


A tail-heavy test airplane with simple artificial stability using canards.
The canards work as extra elevators. Without pitch control input, the canards are controlled by a gyroscope, blended with the direction of the aircraft is traveling.

Why tail-heavy?
To move the center of mass aft and achieve high maneuverability in pitch, but doing so will make the aircraft unstable.

Control surfaces include ailerons, elevators, flaperons, elevons, and rudder.

- P : Unpin
- UP / DOWN : Pitch control
- LEFT / RIGHT : Bank control
- Z / X : Yaw control
- CTRL (Toggle) : Add thrust
- SHIFT : Add thrust
- C (Toggle) : Increase lift & drag
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