Apparatus and method for closing flight plans and locating aircraft

• US 5,351,194 A
• Filed: 05/14/1993
• Issued: 09/27/1994
• Est. Priority Date: 05/14/1993
• Status: Expired due to Term

• Current Assignee: WNS Holdings LLC
• Original Assignee: Worldwide Notification Systems, Inc.
• Inventors: Farmakis, Tom, Ross, John
• Primary Examiner(s): Chin, Gary
• Application Number:
  US08/062,406
• Time in Patent Office: 501 Days
• Field of Search: 364/428, 364/439, 364/441, 364/443, 364/446, 364/460, 364/447, 364/449, 73/178 R, 340/904, 340/947, 340/948, 340/951, 340/960, 340/991, 340/992, 342/33-35, 342/42, 342/450, 342/357, 342/451, 342/457, 342/463, 342/464, 379/59
• US Class Current: 455/456.3
• CPC Class Codes: B60R 2325/304 Boats
• CPC Class Codes: B60R 25/102 a signal being sent to a remote location, e.g. a radio signal being transmitted to a police station, a security company or the owner
• CPC Class Codes: B60W 2556/50 of positioning data, e.g. GPS [Global Positioning System] data
• CPC Class Codes: G01S 19/17 Emergency applications
• CPC Class Codes: G01S 2205/002 for traffic control, mobile tracking, guidance, surveillance or anti-collision
• CPC Class Codes: G01S 2205/005 for aircraft positioning relative to other aircraft
• CPC Class Codes: G01S 2205/008 using a mobile telephone network
• CPC Class Codes: G01S 5/0009 Transmission of position information to remote stations involving assistance data G01S5/0236
• CPC Class Codes: G01S 5/0027 of actual mobile position, i.e. position determined on mobile
• CPC Class Codes: G01S 5/0072 Transmission between mobile stations, e.g. anti-collision systems
• CPC Class Codes: G08G 1/205 Indicating the location of the monitored vehicles as destination, e.g. accidents, stolen, rental
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0056 in an emergency situation, e.g. hijacking

Abstract

An apparatus and method of canceling a flight plan of an aircraft to facilitate release of an IFR airspace to other aircraft and for communicating the location of a downed aircraft during emergencies. A controller receives and analyzes positioning signals transmitted from know locations to determine the location of the aircraft periodically. Upon arrival of the aircraft at its destination, the controller calls the air traffic controllers to cancel the flight plan. In the event of an emergency, the controller calls the air traffic control center to report the emergency and the location of the aircraft with high accuracy to improve search and rescue operations.

Claims

1. An apparatus for monitoring a status and location of an aircraft, comprising:

a receiver attached to an aircraft for receiving a positioning signal from each of a plurality of transmitters located at separate known locations;

a switch located on the aircraft and indicating a status of the aircraft;

a controller operatively connected to the receiver and the switch for determining the location of the aircraft based upon the positioning signals, said controller detecting the status of the aircraft by sensing the switch;

a communicator operatively connected to the controller for communicating a signal to the air traffic control center to report the status and location of the aircraft in response to the switch.

2. The apparatus as recited in claim 1, wherein the controller comprises a microprocessor.

3. The apparatus as recited in claim 2, wherein said communicator comprises a wireless cellular telephonic transmitter.

4. The apparatus as recited in claim 1, further comprising:

a second switch located on the aircraft and operatively connected to the controller, said second switch being responsive to a high-impact force to signal the controller to initiate communications with an air traffic control center for reporting the location of said aircraft which has been downed.

5. The apparatus of claim 1 wherein said receiver comprises a global positioning system (GPS) receiver for receiving positioning signals from a plurality of GPS satellites.

6. The apparatus of claim 1, wherein said switch comprises a plurality of switches, each indicating an unique status of the aircraft.

7. The apparatus of claim 1 wherein said switch comprises an automatic switch operatively connected to the aircraft landing gear for automatically indicating that the aircraft is landing.

8. The apparatus of claim 1 wherein said switch comprises an emergency switch located on the aircraft, the emergency switch indicating whether or not the aircraft is in an emergency situation and requires assistance.

9. A method of monitoring a status and location of an aircraft, comprising the steps of:

a) receiving at the aircraft a positioning signal from each of a plurality of transmitters positioned at separate known locations;

b) determining a current location of the aircraft based upon the received positioning signals;

c) sensing a switch, the switch located on the aircraft and indicating the status of the aircraft;

d) communicating a signal from the aircraft to a central station to report the status and the location of the aircraft, in response to said step of sensing the switch.

10. The method of claim 9, wherein said step of receiving comprises the step of receiving at the aircraft a positioning signal from each of a plurality of transmitters located on global positioning system (GPS) satellites.

11. The method of claim 9, wherein said step of sensing comprises the step of periodically polling each of a plurality of switches located on the aircraft to determine the status of the aircraft, each of the switches indicating an unique status of the aircraft.

12. The method of claim 9 wherein said step of sensing comprises the step of sensing the position of a down-aircraft switch, the down-aircraft switch indicating that the aircraft is unintentionally down when the switch is in an actuated position.

13. The method of claim 12 wherein said step of communicating comprises the step of communicating a signal from the aircraft to a central station to report the location of the aircraft and to report that the aircraft is down if the down-aircraft switch is sensed to be in the actuated state, the down-aircraft switch being automatically actuated when the aircraft is downed.

14. The method of claim 9 wherein said step of sensing comprises the step of sensing the state of a flight-plan switch, the flight-plan switch indicating that the flight plan is to be closed when the flight-plan switch is in the actuated state.

15. The method of claim 9 wherein said step of sensing comprises the step of sensing the state of an emergency switch located on the aircraft, the emergency switch indicating when in an actuated state that the aircraft is in an emergency and requires assistance.

16. The method of claim 15 wherein said step of communicating comprises the step of communicating a signal from the aircraft to a central station to periodically report the location of the aircraft and to report that the aircraft is in a state of emergency if the emergency switch is in an actuated state.

17. The method of claim 9 further comprising the step of sensing on the aircraft a request to close the aircraft'"'"'s flight plan, said step of communicating further comprises the step of communicating to the central station the request to close the aircraft'"'"'s flight plan to the central station in response to said step of sensing the request to close the aircraft'"'"'s flight plan.

18. The method of claim 17, wherein said step of sensing a request to close the aircraft'"'"'s flight plan comprises the step of sensing the state of a manual flight-plan switch located on the aircraft, the flight-plan switch indicating that the flight plan is to be canceled when the flight-plan switch has been actuated.

19. The method of claim 9 wherein said step of sensing comprises the step of sensing the state of an automatic switch operatively connected to the aircraft landing gear for automatically indicating that the aircraft is landing upon lowering of the landing gear.

20. The method of claim 19 wherein said step of communicating comprises communicating a signal from the aircraft to the central station to identify the aircraft, to report that the aircraft is landing, to request closing of the aircraft'"'"'s flight plan and to report the location of the aircraft, in response to said step of sensing.