Servo actuators actuate flight control surfaces to verify gust lock status before engine start.
A monitoring device analyzes guidance instructions to identify defective flight management systems.
Dynamic phase lag compensation prevents off-axis moments during flight maneuvers.
Independent flap positioning via a single drive link optimizes lift-drag tradeoffs, reducing fuel consumption and noise during takeoff and landing.
A breakable link merges dual yoke inputs to enable remote pilot assistance, reducing operational complexity and personnel requirements.
Segmented control systems adapt aileron and spoiler deflection to gust length, resolving the trade-off between peak load reduction and control authority.
Closure panel bridges gap between wing and control surface, eliminating aerodynamic disturbances caused by movable flight surfaces.