Terrain augmented 3D flight path display for flight management systems

• US 6,678,588 B2
• Filed: 04/12/2002
• Issued: 01/13/2004
• Est. Priority Date: 04/12/2002
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: He, Gang
• Primary Examiner(s): Beaulieu, Yonel
• Application Number:
  US10/122,046
• Publication Number:
  US 20030195672A1
• Time in Patent Office: 641 Days
• Field of Search: 701/1, 701/3, 701/4, 701/8, 701/9, 701/14, 701/300, 701/301
• US Class Current: 701/3
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G01S 7/22 Producing cursor lines and indicia by electronic means
• CPC Class Codes: G01S 7/24 the display being orientated or displaced in accordance with movement of object carrying the transmitting and receiving apparatus, e.g. true-motion radar
• CPC Class Codes: G06T 17/05 Geographic models
• CPC Class Codes: G06T 19/003 Navigation within 3D models or images
• CPC Class Codes: G06T 2210/36 Level of detail
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0052 for cruising combined instruments indicating more than one navigational value G01C23/00
• CPC Class Codes: G08G 5/0086 for monitoring terrain radar or analogous systems specially adapted for terrain avoidance G01S13/935

Abstract

The computation and data load for producing a flight plan and terrain display for a flight management system is reduced through the use of intelligent level of detail control which computes and displays flight plan areas and related terrain with a high level of detail. The outer terrain details, i.e., those further removed from the flight path, are processed and displayed in a manner that shows all significant terrain features, e.g., peaks, towers, and the like, but with much less detail so as to significantly reduce the overall computational load for producing such 3D flight path displays in real time. This ensures that all-important information relative to the flight path is correctly processed and displayed while secondary information is shown with important features to provide broad awareness of areas surrounding the intended flight path.

Claims

1. A flight deck display system comprising:

a display having a display screen for graphical display of data,

a graphics processor for receiving terrain data from at least a terrain data base and flight plan information from a source of navigational data and for providing input data to the display screen, the terrain data being in the form of a variable error bound polygon binary tree based terrain patch,

the display displaying a representation of the flight plan on the display screen and displaying a representation of the terrain underlying the flight plan,

the representation of the terrain proximate to the representation of the flight plan being rendered with a smaller error bound than the representation of the terrain elsewhere on the display.

2. A flight management system as set forth in claim 1, wherein the display of the terrain outside the area proximate to the flight plan displays significant terrain features.

3. A flight management system as set forth in claim 1 wherein the display of the terrain representation outside the area proximate to the flight path utilizes a larger error bound to suppress minor terrain features.

4. A flight management system as set forth in claim 3, wherein the display of the terrain representation outside the area proximate to the representation of the flight plan displays significant terrain features.

9. A flight management system as set forth in claim 1 wherein the error bound is adjustable by a user of the system.

10. A flight management system as set forth in claim 1 wherein the polygon binary tree is a triangle binary tree.

5. In a flight management system having a graphics processor for providing display data to a display wherein a flight plan representation is underlaid by a terrain representation, a method for reducing the computation and data load on the graphics processor for producing the display, comprising:

construction an error bound terrain height defining an area of terrain to be displayed on the display using a selected error bound, such that the display renders useful terrain detail while allowing an acceptable processing load on the graphics processor,

projecting the flight plan on the terrain representation, and

selecting smaller error bound values for the terrain display in the area proximate to the representation of the flight plan.

6. A flight management system as set forth in claim 5 wherein the error bound array is a binary tree based array.

7. A flight management system as set forth in claim 6 wherein the binary tree is a triangle binary tree.

8. A flight management system as set forth in claim 5 wherein the error bound values are modifiable by a user of the flight management system.

11. A flight management system as set forth in claim 5 wherein the selected error bound contributes to the reduced computation and data load on the graphics processor.

12. A flight management system as set forth in claim 5 wherein a larger error bound is selected for areas not proximate to the flight plan.