NORMAL CONDITIONS
Lateral deflection of the sidestick results in a roll rate that is intuitive to the pilot.
The greater the lateral deflection of the sidestick, the greater the resulting roll rate.
Maximum lateral deflection of the sidestick results in a 15° / second roll rate.
When the sidestick is in the neutral position:
- At AOB of 33 ° and less:
- The current AOB is maintained
- Pitch compensation is provided
- At AOB of greater than 33°:
- AOB reduces to 33°
- Pitch compensation is not provided
- Aircraft maintains spiral stability
The computed lateral component of Normal Law is a mixture of roll and yaw demand with:
- Automatic turn coordination
- Automatic yaw damping
- Initial yaw damper response to aircraft lateral asymmetry (including asymmetric thrust).