Aircraft navigational warning system

• US 6,219,618 B1
• Filed: 01/25/1999
• Issued: 04/17/2001
• Est. Priority Date: 01/25/1999
• Status: Expired due to Fees

• Current Assignee: Wesley H. Bateman
• Original Assignee: Wesley H. Bateman
• Inventors: Bateman, Wesley H.
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): ARTHUR JEANGLAUDE, GERTRUDE
• Application Number:
  US09/236,853
• Time in Patent Office: 813 Days
• Field of Search: 701/9, 701/13-14, 701/206, 701/207, 701/208, 701/213, 701/300, 701/301, 340/425.5, 340/945, 340/961, 340/970, 244/75.R, 244/158.R
• US Class Current: 701/301
• CPC Class Codes: G01C 21/005 with correlation of navigation data from several sources, e.g. map or contour matching G01C21/30 takes precedence
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence

Abstract

An aircraft navigational system allows for reduced storage and increased computing power for comparing terrain maps to the flight path and enroute track of the aircraft. Unique provisions are made for reporting and recording navigational hazards.

Claims

1. An aircraft navigational warning system comprising:

a position data generator installed on an aircraft for producing a position data representation of the position of said aircraft;

a map storage unit containing a multiplicity of terrain maps corresponding to the flight path of said aircraft for storing said multiplicity of terrain maps;

an evaluator coupled to said position data generator and further coupled to said map storage unit for comparing said position data representation to at least one of said multiplicity of terrain maps corresponding to the flight path of said aircraft; and

a warning indicator coupled to said evaluator for producing a warning signal when said evaluator calculates that a projected position of said aircraft and a position of upcoming terrain on the flight path of said aircraft are separated by less than a safe distance or time of approach.

2. An aircraft navigational warning system in accordance with claim 1 wherein said position data generator comprises a Global Positioning System receiver.

3. An aircraft navigational warning system in accordance with claim 1 wherein said map storage unit comprises a computer memory.

4. An aircraft navigational warning system in accordance with claim 1 wherein and said map storage unit is initialized from a plurality of CD-ROM discs containing terrain map data.

5. An aircraft navigational warning system in accordance with claim 1 further comprising a visual display coupled to said map storage unit for displaying map data extracted from at least one of said multiplicity of terrain maps.

6. An aircraft navigational warning system in accordance with claim 1 further comprising a warning transmitter coupled to said evaluator for transmitting an output of said warning indicator to a ground receiver for informing ground personnel of a danger to said aircraft.

7. An aircraft navigational warning system in accordance with claim 6 wherein said warning transmitter comprises a cellular telephone communications transmitter.

8. An aircraft navigational warning system in accordance with claim 1 wherein an output of said evaluator is an input to a flight event recording system installed on said aircraft.

9. An aircraft navigational warning system in accordance with claim 8 wherein said output is activated after said warning indication has been present for a predetermined amount of time.

10. An aircraft navigational warning system comprising:

a position data generator installed on an aircraft for producing a position data representation of the position of said aircraft;

an identification generator for generating an identification code unique to said aircraft;

a transmitter installed on said aircraft and coupled to said position data generator and further coupled to said identification generator for transmitting said position data representation and identification code;

at least one remote receiver for receiving said position data representation and identification code;

at least one remote map storage unit containing a multiplicity of terrain maps;

at least one remote evaluator coupled to said at least one remote receiver and further coupled to said at least one remote map storage unit for comparing said position data representation with said multiplicity of terrain maps;

at least one remote warning transmitter coupled to said at least one remote evaluator for producing a warning transmission when said at least one remote evaluator calculates that a projected position of said aircraft and a position of upcoming terrain on the flight path of said aircraft are separated by less than a safe distance or time of approach;

a warning receiver installed on said aircraft for receiving said warning transmission; and

a warning indicator coupled to said warning receiver for producing a visual or audible warning to the operator of said aircraft when said warning transmission is received.

11. An aircraft navigational warning system in accordance with claim 10 wherein an output of said warning receiver is input to a flight event record system installed on said aircraft.

12. An aircraft navigational warning system in accordance with claim 11 wherein said output is activated after said warning indication has been present for a predetermined amount of time.

13. An aircraft navigational warning system in accordance with claim 10 wherein said position data generator comprises a Global Positioning System receiver.

14. An aircraft navigational warning system in accordance with claim 10 wherein said transmitter comprises a cellular telephone communication transmitter and said at least one receiver comprises a cellular telephone communication receiver.

15. An aircraft navigational warning system in accordance with claim 10 wherein said at least one remote warning transmitter comprises a cellular telephone communication transmitter and said warning receiver comprises a cellular telephone communication receiver.

16. An aircraft navigational warning system comprising:

a position data generator installed on said aircraft for producing a position data representation of the position of said aircraft;

an identification generator for generating an identification code unique to said aircraft;

a local transmitter installed on said aircraft and coupled to said position data generator and further coupled to said identification generator for transmitting said position data representation and identification code;

at least one remote receiver for receiving said position data representation and identification code;

at least one remote map storage unit containing a multiplicity of terrain maps, coupled to said at least one remote receiver;

at least one remote transmitter coupled to said map storage unit for transmitting map data corresponding to said position data representation;

a local receiver installed on said aircraft for receiving map data from said at least one transmitter;

a local map storage unit coupled to said local receiver for storing received map data;

an evaluator coupled to said position data generator and further coupled to said local map storage unit for comparing said position data representation with said received map data; and

a warning indicator coupled to said evaluator for producing a visual or audible warning to the operator of said aircraft when said evaluator calculates that a projected position of said aircraft and a position of upcoming terrain on the flight path of said aircraft are separated by less than a safe distance or time of approach.

17. An aircraft navigational warning system in accordance with claim 16 wherein said local transmitter comprises a cellular telephone communications transmitter and said at least one remote receiver comprises a cellular telephone communications receiver.

18. An aircraft navigational warning system in accordance with claim 16 wherein said at least one remote transmitter comprises a cellular telephone communications transmitter and said local receiver comprises a cellular telephone communications receiver.

19. An aircraft navigational warning system in accordance with claim 16 wherein said local transmitter further transmits an output of said warning indicator to said at least one remote receiver for informing ground personnel of a danger to said aircraft.

20. An aircraft navigational warning system in accordance with claim 16 wherein said position data generator comprises a Global Positioning System receiver.

21. An aircraft navigational warning system in accordance with claim 16 wherein an output of said warning receiver is input to a flight event record system installed on said aircraft.

22. An aircraft navigational warning system in accordance with claim 21 wherein said output is activated after said warning indication has been present for a predetermined amount of time.