Anti-hijacking system operable in emergencies to deactivate on-board flight controls and remotely pilot aircraft utilizing autopilot
AssigneeCubic Defense Systems, Inc.
InventorDouglas G. Nelson
Life of this patent
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AssigneeCubic Defense Systems, Inc.
InventorDouglas G. Nelson
Estimating the term…
In an anti-hijacking system for autopilot equipped aircraft, a transceiver communicates with at least one remote guidance facility. A panic button is activated by flight crew in case of hijacking. A manager is coupled to the transceiver and the panic button, as well as existing avionics including the aircraft's master computer and autopilot. Optionally, a relay is coupled between the pilot controls and selected aircraft flight systems. The manager recognizes predetermined override inputs, such as activation of the panic button or receipt of override signals from the remote guidance facility. Responsive to the override input, the manager deactivates on-board control of selected aircraft flight systems and the autopilot system, and directs the autopilot to fly the aircraft to a safe landing. Flight routing and landing instructions are obtained from the remote guidance facility, or by self-evaluating nearby airports in view of the aircraft's position and various preestablished criteria.
A method for preventing hijacking of an aircraft, comprising operations of:
A signal-bearing medium tangibly embodying a program of machine-readable instructions executable by a hijacking intervention module aboard an aircraft having an autopilot system to perform a method for preventing hijacking of the aircraft, the operations comprising:
A logic circuit of multiple interconnected electrically conductive elements configured to perform operations to prevent hijacking of an aircraft by operating a hijacking intervention module aboard the aircraft, the operations comprising:
An anti-hijacking system for use in an aircraft having an autopilot system, comprising:
An anti-hijacking system for use in an aircraft having an autopilot system, comprising:
Dependencies are inferred from the claim text.