Automatic horizontal and vertical scanning radar with terrain display

• US 5,781,146 A
• Filed: 03/11/1996
• Issued: 07/14/1998
• Est. Priority Date: 03/11/1996
• Status: Expired due to Term

• Current Assignee: Honeywell International Inc.
• Original Assignee: Imaging Accessories, Inc.
• Inventors: Frederick, Philip R.
• Primary Examiner(s): Sotomayor, John B.
• Application Number:
  US08/613,017
• Time in Patent Office: 855 Days
• Field of Search: 342/26, 342/65, 342/176, 342/179, 342/185, 342/197
• US Class Current: 342/26.00B
• CPC Class Codes: G01S 13/935 for terrain-avoidance
• CPC Class Codes: G01S 13/953 mounted on aircraft
• CPC Class Codes: G01S 7/22 Producing cursor lines and indicia by electronic means
• CPC Class Codes: Y02A 90/10 Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Abstract

A weather radar and terrain map display system for aircraft with the terrain elevation and weather information displayed in an easy to read and comprehend presentation. The system includes an antenna for transmitting and receiving radar signals, a receiver for digitizing the reflected radar signals, and a computer for storing the signals and calculating the latitude and longitude coordinates of the locations from which the reflected radar signals were reflected, and for storing terrain elevation data. A display simultaneously shows a plan view image and vertical views of contoured terrain elevation data and the weather conditions found by the radar. The terrain and weather displays are superimposed over one another to enable quick and efficient location of critical terrain and weather conditions. The system can also calculate the latitude and longitude coordinates of the radar echoes without antenna stabilization.

Claims

1. A weather radar and terrain map display system for aircraft comprising

means for transmitting radar signals out from the aircraft and for receiving back reflected radar signals,

means for digitizing the reflected radar signals received by the transmitting and receiving means,

means for calculating the latitude and longitude coordinates of the locations from which the reflected radar signals were reflected,

first means for storing the digitized signals and the latitude and longitude coordinates calculated for the reflected radar signals,

second means for storing terrain elevation data referenced to latitude and longitude coordinates of the ground over which the aircraft will travel, and

display means, responsive to the first and second storing means, for simultaneously displaying a plan view image over a horizontal range (a) of weather, represented by digitized reflected radar signals, relative to the calculated latitude and longitude coordinates, and (b) terrain elevation data relative to the latitude and longitude coordinates of that data, said weather display and terrain data display being superimposed over one another.

2. A system as in claim 1 further comprising

means for determining the altitude of the aircraft,

means for comparing the altitude of the aircraft to the terrain elevation data and selecting the latitude and longitude coordinates of the critical terrain elevation data where the elevation of the terrain is at a selected level with respect to the altitude of the aircraft, and

means for highlighting the image of the selected critical terrain elevation on the display means.

3. A system as in claim 2 further comprising means for producing an alarm signal when critical terrain elevation data is selected.

4. A system as in claim 1 wherein the display means, responsive to the first and second storing means, simultaneously displays a vertical view (a) of weather, represented by digitized reflected radar signals, relative to the calculated latitude and longitude coordinates and (b) terrain elevation data relative to the latitude and longitude coordinates of the terrain elevation data, the weather display and terrain data display being superimposed over one another.

5. A system as in claim 4 wherein the display means, responsive to the first and second storing means, for simultaneously displaying a vertical view includes

a vertical front view (a) of weather, represented by digitized reflected radar signals, relative to the calculated latitude and longitude coordinates, and (b) terrain elevation data relative to the latitude and longitude coordinates of that data, said weather display and terrain data display being superimposed over one another, and

at least one vertical side view (a) of weather, represented by digitized reflected radar signals, relative to the calculated latitude and longitude coordinates, and (b) terrain elevation data relative to the latitude and longitude coordinates of that data, said weather display and terrain data display being superimposed over each another.

6. A system as in claim 1 further comprising

third means for storing an elevation coding table assigning a distinctive color and pattern to each range of elevation, and

means for comparing the height in the terrain elevation data at each coordinate with the stored elevation color coding table, and assigning distinctive color and pattern to represent the terrain elevation height at each coordinate on the plan view image.

7. A system as in claim 1 further comprising means for retrieving the terrain elevation data relative at each coordinate to generate contour lines on the display means.

8. A system as in claim 1 further comprising navigation means for locating the present position of the aircraft and of superimposing an aircraft position marker at the latitude and longitude coordinates of the present position over the weather display and terrain data on the plan view image of the display means.

9. A system as in claim 4 further comprising

means for determining the altitude of the aircraft,

means for superimposing an aircraft position marker at the determined altitude of the aircraft over the weather display and terrain data on the vertical view image of the display means.

10. A system as in claim 1 further comprising

third means for storing map data referenced to the latitude and longitude coordinates of the ground over which the aircraft will travel,

display means, responsive to the first, second, and third storing means, for simultaneously displaying a plan view image over a horizontal range (a) of weather, represented by digitized reflected radar signals, relative to the calculated latitude and longitude coordinates, b) of the map data relative to the latitude and longitude coordinates of the map data, and (c) terrain elevation data relative to the latitude and longitude coordinates of that data, said weather display, map data display, and terrain data display being superimposed over each another.

11. A system as in claim 1 further comprising

a region at a fixed distance from the aircraft, the region having a transverse length and a vertical distance,

means for continually determining the latitude and longitude coordinates of locations within the region as the aircraft moves through space, and

means for comparing the latitude and longitude coordinates of the locations within the region to the latitude and longitude of the stored terrain elevation data and for selecting the latitude and longitude of any location within the region that has the same latitude and longitude as any stored terrain elevation data.

12. A system as in claim 11 further comprising means for generating an output signal when the latitude and longitude of the terrain elevation data is selected.

13. A system as in claim 11 further comprising means for highlighting on the display the latitude and longitude of all the selected terrain elevation data.

14. A system as in claim 1 wherein the means for calculating the latitude and longitude coordinates includes means for calculating the latitude and longitude coordinates when antenna stabilization is not used.

15. A system as in claim 1 further wherein the means for calculating the latitude and longitude coordinates further comprises a means for calculating the antenna slew corrected for bank of the aircraft A and the antenna tilt angle corrected for pitch of the aircraft θ

, given the antenna slew uncorrected for roll A_b, the range or distance of radar echo R, the pitch in degrees above or below horizontal P, the antenna elevation relative to the horizontal plane uncorrected for roll θ

_b and the bank angle B as follows;

##EQU3##

16. A weather radar and terrain map display system for aircraft comprising

means for transmitting radar signals out from the aircraft and for receiving back reflected radar signals,

means for digitizing the reflected radar signals received by the transmitting and receiving means,

means for calculating the latitude, longitude, and elevation coordinates of the locations from which the reflected radar signals were reflected,

first means for storing the digitized radar signals and the latitude, longitude, and elevation coordinates calculated for the reflected radar signals,

second means for storing terrain elevation data referenced to latitude and longitude coordinates of the ground over which the aircraft will travel,

filtering means, responsive to the first and second storing means, for comparing the digitized radar signals with the terrain elevation data at the same latitude and longitude as the latitude and longitude calculated for the digitized radar signal and blocking those digitized radar signals where calculated elevation of the radar signal is below the corresponding terrain elevation.

display means, responsive to the filtering means, for displaying a plan view image over a horizontal range of weather, represented by the filtered digitized reflected radar signals, relative to the calculated latitude and longitude and elevation coordinates.

17. A system as in claim 16 wherein the display means, responsive to the filtering means, displays a vertical view image of weather, represented by the filtered digitized reflected radar signals, relative to the calculated latitude and longitude and elevation coordinates.

18. A system as in claim 16 further comprising

a region at a fixed distance from the aircraft, the region having a transverse length and a vertical distance,

means for continually determining the latitude and longitude coordinates of locations within the region as the aircraft moves through space, and

means for comparing the latitude and longitude coordinates of the locations within the region to the latitude and longitude of the stored terrain elevation data and for selecting the latitude and longitude of any location within the region that has the same latitude and longitude as any stored terrain elevation data.

19. A system as in claim 18 further comprising means for generating an output signal when the latitude and longitude of the terrain elevation data is selected.

20. A system as in claim 18 further comprising means for highlighting on the display the latitude and longitude of all the selected terrain elevation data.

21. A system as in claim 16 wherein the means for calculating the latitude and longitude coordinates includes means for calculating the latitude and longitude coordinates when antenna stabilization is not used.

22. A system as in claim 16 further wherein the means for calculating the latitude and longitude coordinates further comprises a means for calculating the antenna slew corrected for bank of the aircraft A and the antenna tilt angle corrected for pitch of the aircraft θ

, given the antenna slew uncorrected for roll A_b, the range or distance of radar echo R, the pitch in degrees above or below horizontal P, the antenna elevation relative to the horizontal plane uncorrected for roll θ

_b and the bank angle B as follows;

##EQU4##

23. A terrain map display system for aircraft comprising

means for storing terrain elevation data referenced to latitude and longitude coordinates of the ground over which the aircraft will travel, and

display means, responsive to the storing means, for displaying a plan view image over a horizontal range showing the terrain elevation data relative to the latitude and longitude coordinates of that data.

24. A system as in claim 23 further comprising

means for determining the altitude of the aircraft,

means for comparing the altitude of the aircraft to the terrain elevation data and selecting the latitude and longitude coordinates of the critical terrain elevation data where the elevation of the terrain is at a selected level with respect to the altitude of the aircraft, and

means for highlighting the image of the selected critical terrain elevation on the display means.

25. A system as in claim 23 further comprising means for producing an alarm signal when critical terrain elevation data is selected.

26. A system as in claim 23 wherein the display means, responsive to the storing means, displays a vertical view showing the terrain elevation data relative to the latitude and longitude coordinates of that data.

27. A system as in claim 26 wherein the display means, responsive to storing means, for displaying a vertical view includes

a vertical front view of terrain elevation data relative to the latitude and longitude coordinates of that data, and

at least one vertical side view of terrain elevation data relative to the latitude and longitude coordinates of that data.

28. A system as in claim 23 further comprising

fourth means for storing an elevation coding table assigning a distinctive color and pattern to each range of elevation, and

means for comparing the height in the terrain elevation data at each coordinate with the stored elevation color coding table, and assigning distinctive color and pattern to represent the terrain elevation height at each coordinate on the plan view image.

29. A system as in claim 23 further comprising means for retrieving the terrain elevation data relative at each coordinate to generate contour lines on the display means.

30. A system as in claim 23 further comprising navigation means for locating the present position of the aircraft and of superimposing an aircraft position marker at the latitude and longitude coordinates of the present position over the terrain data on the plan view image of the display means.

31. A system as in claim 23 further comprising

means for determining the altitude of the aircraft,

means for superimposing an aircraft position marker at the determined altitude of the aircraft over the terrain data on the vertical view image of the display means.

32. A system as in claim 23 further comprising

means for receiving radar signals with the latitude and longitude coordinates calculated for the radar signals, and

wherein the display means, also responsive to the means for receiving radar signals, simultaneously displays (a) weather, represented by digitized radar signals, relative to the calculated latitude and longitude coordinates, and (b) terrain elevation data relative to the terrain elevation data relative to the latitude and longitude coordinates of that data, said weather display and terrain data display being superimposed over one another.