Aerial user equipment switches to directional transmit mode when elevation exceeds thresholds, reducing interference to neighboring base stations.
Segmenting the brake controller from the screw shaft members eliminates axial feedback forces, reducing maintenance complexity and motor workload.
A flap deployment system integrates aerodynamic surfaces into the support structure to maintain a continuous profile in the stowed position.
A dual actuation assembly links inboard and outboard flight control surfaces to move them in tandem.
Destination transceivers authenticate drones via beacon signals to resolve delivery precision and security trade-offs.
Analog hydraulic control loops balance load sharing between dual actuators, eliminating software certification delays and enabling KHz transient compensation.
Replacing mechanical transmissions with a linear electric motor reduces movement device mass and footprint while enhancing flap precision.
Flap-driven jackscrew linkage moves a wing droop panel through mechanical coupling, eliminating bulky dedicated actuators and reducing wing assembly weight.
A remote sensor interface generates pseudo-GPS signals to merge with inertial tracking data.
An aircraft energy protection device manages autothrust using angle of attack and control member position data.
Variable wing sweep and membrane tension generate control torques, resolving the trade-off between precise angular orientation and mechanical complexity.
A shape-memory alloy actuator uses induction heating and magneto-thermal convection cooling to transform material phases and drive mechanical motion.
A torque tube door attaches to an inboard wing flap to cover a fuselage opening during cruise flight.