Very cool! Is it all artificial? Meaning since it's FBW, the computer generates the forces you encounter in the stick, right?
Yes.
Example, in the landing mode:
FLARE MODE
Applicable to: ALL
The flight mode changes to flare mode when the aircraft passes 50 ft RA as it descends to land.
The system memorizes the attitude at 50 ft, and that attitude becomes the initial reference for pitch
attitude control.
As the aircraft descends through 30 ft, the system begins to reduce the pitch attitude, reducing it to
2 ° nose down over a period of 8 s. This means that it takes gentle nose-up action by the pilot to flare
the aircraft.
FLIGHT MODE
The normal-law flight mode is a load-factor-demand mode with automatic trim and protection
throughout the flight envelope.
Following normal law, the sidestick controllers set the elevator and THS to maintain load factor
proportional to stick deflection and independent of speed.
With the sidestick at neutral, wings level, the system maintains 1 g in pitch (corrected for pitch
attitude), and there is no need for the pilot to trim by changing speed or configuration.
Pitch trim is automatic both in manual mode and when the autopilot is engaged. In normal turns (up
to 33 ° of bank) the pilot does not have to make any pitch corrections once the turn is established.
The flight mode is active from takeoff to landing, and follows the logic shown schematically (Refer to
DSC-27-20-10-10 General).
Automatic pitch trim freezes in the following situations:
‐ The pilot enters a manual trim order.
‐ The radio altitude is below 50 ft (100 ft with autopilot engaged).
‐ The load factor goes below 0.5 g.
When angle-of-attack protection is active, the THS setting is limited between the setting at the aircraft’s
entry into this protection and 3.5 ° nose down. (Neither the pilot nor the system can apply
additional nose-up trim).
Similarly, when the load factor is higher than 1.25 g or when the aircraft exceeds 33 ° of bank, the
THS setting is limited to values between the actual setting and 3.5 ° nose down.
When High Speed or High Mach Protection is active, the THS Setting is limited between the setting
at the aircraft’s entry into this protection and 11 ° nose-up.