Anti-hijacking security system and apparatus for aircraft

• US 6,584,383 B2
• Filed: 09/28/2001
• Issued: 06/24/2003
• Est. Priority Date: 09/28/2001
• Status: Expired due to Fees

• Current Assignee: Phillip Mckinney Pippenger
• Original Assignee: Phillip Mckinney Pippenger
• Inventors: Pippenger, Phillip McKinney
• Primary Examiner(s): Camby, Richard M.
• Application Number:
  US09/967,026
• Publication Number:
  US 20030093193A1
• Time in Patent Office: 634 Days
• Field of Search: 701/1, 701/41, 701/3, 701/2, 701/300, 701/301, 701/36, 701/213, 701/214, 701/200-212, 307/10.5, 342/29, 340/988-995
• US Class Current: 701/3
• CPC Class Codes: B64D 45/0031 means for overriding or restricting access to flight controls
• CPC Class Codes: B64D 45/0059 by communicating emergency situations to ground control or between crew members
• CPC Class Codes: G05D 1/0061 for transition from automatic pilot to manual pilot and vice versa
• CPC Class Codes: G08G 5/0056 in an emergency situation, e.g. hijacking

Abstract

A vehicle security system and method allows for the disabling of manual vehicle control, while automatic vehicle guidance provides control of the vehicle. The vehicle, which may be an aircraft, boat, train, truck, etc. is thus secured against unauthorized guidance that could harm passengers or other persons or property. In an embodiment, the security system automatically controls the vehicle to avoid collision with ground features when imminent collision is detected.

Claims

1. An apparatus for securing an aircraft against unauthorized direction or misdirection of the aircraft, the apparatus comprising:

a security navigation module further comprising;

an alarm interface to an alarm source for receiving an alarm signal directed to the security navigation module from the alarm source;

a control interface for sending communications to flight control facilities of the aircraft; and

a sensor interface for receiving communications from aircraft sensor facilities,

whereby receipt of an alarm signal at the alarm interface is operative to cause the security navigation module to disable manual navigation control of the aircraft and to assert automatic control of the aircraft by sending a communication to the flight control facilities of the aircraft via the control interface, wherein the automatic control of the aircraft is based at least in part on signals received by the security navigation module at the sensor interface.

2. The apparatus of claim 1, wherein the alarm source is a manual actuator manipulatable by a human operator.

3. The apparatus of claim 1, wherein the alarm source is an automatic sensor adapted to detect crossing of a boundary by a human or an object.

4. The apparatus of claim 3, wherein the boundary comprises a boundary segment lying between the cabin and cockpit of the aircraft.

5. The apparatus of claim 3, wherein the sensor comprises a photoelectric sensor.

6. The apparatus of claim 3, wherein the sensor comprises a mechanical sensor.

7. The apparatus of claim 1, wherein the security navigation module further comprises a data entry interface associated with a data entry module, whereby receipt of a coded override signal at the data entry interface from the data entry module causes the security navigation module to re-enable manual navigation control of the aircraft.