Aircraft landing guidance system and method

• US 5,343,395 A
• Filed: 08/26/1992
• Issued: 08/30/1994
• Est. Priority Date: 08/26/1992
• Status: Expired due to Term

• Current Assignee: Safeflight Incorporated
• Original Assignee: Safeflight Incorporated
• Inventors: Watts, Alan B.
• Primary Examiner(s): Black, Thomas G.
• Assistant Examiner(s): WALDER, STEPHEN JOSEPH
• Application Number:
  US07/935,438
• Time in Patent Office: 734 Days
• Field of Search: 364/430, 364/428, 364/433, 364/427, 364/429, 364/431.07, 364/432, 364/434, 364/435, 364/442, 364/443, 364/449, 340/729, 340/948, 340/951, 340/952, 340/947, 340/967, 340/976, 340/972, 340/988, 340/995, 340/990, 340/973, 358/103, 244/183
• US Class Current: 701/16
• CPC Class Codes: G05D 1/0676 specially adapted for landing

Abstract

An aircraft navigational facilitation system (20) and method of use thereof operates in conjunction with conventional apparatus which provides aircraft current situational information. The system includes a memory (22) for storing runway and landing information for each of a plurality runways. An input device, such as a keyboard (24), is provided for selecting a destination runway. The system further includes a video display device (28) which simulates the view from a cockpit of the aircraft, with the view including the destination runway. The video display device is driven by a processor (26) which uses the current situational information and the runway information for periodically generating display signals for the video display device. The display signals cause the video display to provide an updated and scaled simulated three dimensional view of a perimeter of the destination runway from a perspective of the cockpit of the aircraft. The video display device also provides further information including runway identification information, runway centerline, and an indication of a projected touch down point of the aircraft relative to the perimeter of the destination runway.

Claims

1. A navigational facilitation system for use with apparatus which at least periodically provides aircraft current situational information for an aircraft, the system comprising:

a memory for storing, for each of a plurality of runways, runway display-generation information sufficient to generate a display of a runway perimeter;

an input device for selecting a destination runway from the plurality of runways;

a video display for simulating a view from a cockpit of the aircraft;

processor connected to the aircraft situational location apparatus, to the memory, to the input device, and to the video display, for using the current situational information and the runway information for the destination runway for periodically generating display signals for the video display whereby the video display provides a simulated three dimensional view of a perimeter of the destination runway from a perspective of the cockpit of the aircraft, the simulated view of the perimeter of the destination runway being scaled and updated on the basis of the periodically provided aircraft current situational information.

2. The system of claim 1, wherein glide slope information is received from the aircraft current situational information apparatus, and wherein the processor uses the glide slope information to generate display signals whereby the video display further provides an indication of a projected touch down point of the aircraft relative to the perimeter of the destination runway.

3. The system of claim 1, wherein the aircraft current situational information apparatus provides an indication when the aircraft is at first predetermined distance from the destination runway and additionally provides an indication when the aircraft is at second predetermined distance from the destination runway, the second predetermined distance being less than the first predetermined distance, and wherein the processor generates destination runway display signals for the video display only while the aircraft is between the first predetermined distance and the second predetermined distance.

4. The system of claim 3, wherein the first predetermined distance is at an outer marker location and the second predetermined distance is at a middle marker location.

5. The system of claim 1, wherein the perimeter of the runway includes a near width edge, a far width edge, a right longitudinal edge, and a left longitudinal edge, and wherein the far width edge is displayed as a horizon reference.

6. The system of claim 1, wherein the input device is a keypad.

7. The system of claim 1, wherein the memory is a read only memory.

8. The system of claim 1, wherein the memory is a compact disk read only memory.

9. The system of claim 1, wherein the runway information includes runway size information and runway identification information, and wherein the video display further provides the identification information for the destination runway.

10. The system of claim 1, wherein the simulated view of the perimeter of the destination runway is intermittently scaled and updated.

11. The system of claim 1, wherein the video display further provides an indication of a projected position of the aircraft relative to the simulated view of the destination runway.

12. A method for facilitating the navigation of an aircraft, the aircraft having apparatus which at least periodically provides aircraft current situational information for an aircraft, the method comprising:

retrieving, from a memory, runway information for a destination runway including display-generation information sufficient to generate a display of a runway perimeter, the memory having stored therein runway information for a plurality of runways;

using the aircraft current situational information and the runway information for the destination runway to periodically generate display signals;

driving the video display with the video display signals whereby the video display provides a simulated three dimensional view of a perimeter of the destination runway from a perspective of the cockpit of the aircraft, the simulated view of the perimeter of the destination runway being scaled and updated on the basis of the periodically provided aircraft current situational information.

13. The method of claim 12, wherein glide slope information is received from the aircraft current situational information apparatus, and wherein the glide slope information is used to generate display signals whereby the video display further provides an indication of a projected touch down point of the aircraft relative to the perimeter of the destination runway.

14. The method of claim 12, further comprising obtaining an indication when the aircraft is at first predetermined distance from the destination runway and an indication when the aircraft is at second predetermined distance from the destination runway, the second predetermined distance being less than the first predetermined distance,

and wherein display signals for the video display are generated only while the aircraft is between the first predetermined distance and the second predetermined distance.

15. The method of claim 14, wherein the first predetermined distance is at an outer marker location and the second predetermined distance is at a middle marker location.

16. The system of claim 12, wherein the runway information includes runway size information and runway identification information, and wherein the video display further provides the identification information for the destination runway.

17. The system of claim 12, wherein the simulated view of the perimeter of the destination runway is intermittently scaled and updated.

18. The system of claim 12, wherein the video display further provides an indication of a projected position of the aircraft relative to the simulated view of the destination runway.