EMBEDDED FREE FLIGHT OBSTACLE AVOIDANCE SYSTEM

• US 20040239529A1
• Filed: 05/27/2003
• Published: 12/02/2004
• Est. Priority Date: 05/27/2003
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Tran, My
• Granted Patent: US 6,873,269 B2
• Time in Patent Office: Days
• US Class Current: 340/961
• 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 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 13/935 for terrain-avoidance
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91
• CPC Class Codes: G08G 5/0086 for monitoring terrain radar or analogous systems specially adapted for terrain avoidance G01S13/935
• CPC Class Codes: G08G 5/045 Navigation or guidance aids, e.g. determination of anti-collision manoeuvers radar or analogous systems specially adapted for anti-collision between aircraft G01S13/933

Abstract

A free flight obstacle avoidance system (OAS) is a commanded obstacle resolution feedback system. The system employs insertion of hybridized elements to the existing designs of Adaptive Ground Collision Avoidance Systems and Midair Collision Avoidance Systems along with a newly design module, the obstacle avoidance dispatcher and resolver, to provide a coherent obstacle resolution. The system is capable of filtering data produced by the hybrid ground collision avoidance module and the hybrid air collision avoidance module, inserting evaluating solution status and command directives before routing avoidance data to hybrid modules for validation. The dispatcher and resolver module determines the final obstacle resolution to generate avoidance control guidance and appropriate warnings clearly indicated obstacle situation and obstacle avoidance maneuvers to the flight crew. In addition to the avoidance capabilities, the system also provides extended functions of terrain following guidance and space separation warnings.

Claims

1. A method for free flight obstacle avoidance, the method comprising the steps of:

providing a ground collision avoidance module and an air collision avoidance module;

providing an obstacle avoidance dispatcher and resolver module;

routing ground collision solution data from the ground collision avoidance module to the obstacle avoidance dispatcher and resolver module;

routing air collision solution data from the air collision avoidance module to the obstacle avoidance dispatcher and resolver module;

filtering the ground collision solution data and the air collision solution data;

commanding the ground collision avoidance module to validate the ground collision solution data and commanding the air collision avoidance module to validate the air collision solution data;

providing feedback from the obstacle avoidance dispatcher and resolver module with the ground collision solution data and the air collision solution data to the ground collision avoidance module and the air collision avoidance module for evaluation; and

generating a final obstacle avoidance solution from the obstacle avoidance dispatcher and resolver module.

2. The method of claim 1 wherein the step of filtering the ground collision solution data comprises filtering and extracting the ground collision solution data for processing a cross-domain clearance.

3. The method of claim 1 further comprising the step of evaluating the ground collision solution data from a feedback loop and determining a first obstacle avoidance solution.

4. The method of claim 1 wherein step of providing feedback from the obstacle avoidance dispatcher and resolver module with the ground collision solution data and the air collision solution data to the ground collision avoidance module and the air collision avoidance module for evaluation comprises providing identified ground obstacle data to the air collision avoidance module.

5. The method of claim 1 wherein the step of filtering the air collision solution data comprises filtering and extracting the air collision solution data for processing a cross-domain clearance.

6. The method of claim 1 further comprising the step of evaluating the air collision solution data from a feedback loop and determining a second obstacle avoidance solution.

7. The method of claim 1 wherein step of providing feedback from the obstacle avoidance dispatcher and resolver module with the ground collision solution data and the air collision solution data to the ground collision avoidance module and the air collision avoidance module for evaluation comprises providing identified air obstacle data to the ground collision avoidance module.

8. The method of claim 1 further comprising the step of generating a control command and a flight guidance for executing the final obstacle avoidance solution.

9. The method of claim 1 further comprising the step of processing terrain following guidance data.

10. The method of claim 1 further comprising the step of processing air space separation guidance data and issuing flight crew advisories.

11. A free flight obstacle avoidance system for an aircraft comprising a ground collision avoidance module and an air collision avoidance module, the apparatus comprising:

an obstacle avoidance dispatcher and resolver module;

a means for routing ground collision solution data from the ground collision avoidance module to the obstacle avoidance dispatcher and resolver module;

a means for routing air collision solution data from the air collision avoidance module to the obstacle avoidance dispatcher and resolver module;

a filter for filtering the ground collision solution data and the air collision solution data;

a means for commanding the ground collision avoidance module to validate the ground collision solution data and a means for commanding the air collision avoidance module to validate the air collision solution data;

a feedback loop from the obstacle avoidance dispatcher and resolver module to the ground collision avoidance module and the air collision avoidance module for sharing the ground collision solution data and the air collision solution data; and

a means for generating a final obstacle avoidance solution from the obstacle avoidance dispatcher and resolver module.

12. The obstacle avoidance system in accordance with claim 11 wherein said obstacle avoidance dispatcher and resolver module comprises a filter and extract ground collision avoidance component for processing a cross-domain clearance.

13. The obstacle avoidance system in accordance with claim 11 wherein said obstacle avoidance dispatcher and resolver module comprises a component for evaluating the ground collision solution data from the feedback loop and for determining a first flight obstacle avoidance solution.

14. The obstacle avoidance system in accordance with claim 11 wherein said obstacle avoidance dispatcher and resolver module comprises a component for providing identified ground obstacle data to the air collision avoidance module.

15. The obstacle avoidance system in accordance with claim 11 wherein said obstacle avoidance dispatcher and resolver module comprises a filter and extract air collision avoidance component for processing a cross-domain clearance.

16. The obstacle avoidance system in accordance with claim 11 wherein said obstacle avoidance dispatcher and resolver module comprises a component for evaluating air collision solution data from the feedback loop and for determining a second obstacle avoidance resolution.

17. The obstacle avoidance system in accordance with claim 11 wherein said obstacle avoidance dispatcher and resolver module comprises a component for providing identified air obstacles to the ground collision avoidance module.

18. The obstacle avoidance system in accordance with claim 11 wherein said obstacle avoidance dispatcher and resolver module comprises a generate control command and flight guidance component for executing the final obstacle avoidance solution.

19. The obstacle avoidance system in accordance with claim 11 wherein said obstacle avoidance dispatcher and resolver module comprises a terrain following guidance component.

20. The obstacle avoidance system in accordance with claim 11 wherein said obstacle avoidance dispatcher and resolver module comprises an air space separation guidance and advisory component.

21. The obstacle avoidance system in accordance with claim 20 wherein said air space separation guidance and advisory component comprises a control and warnings apparatus for maintaining the aircraft within a specified corridor.