Predictive aircraft flight envelope protection system

Patent metadata

Field	Value
Publication number	US-11651699-B2
Application number	US-201916552629-A
Country	US
Kind code	B2
Filing date	Aug 27, 2019
Priority date	Aug 27, 2018
Publication date	May 16, 2023
Grant date	May 16, 2023

Abstract

The aircraft threat envelope protection system employs a threat envelope data structure in a computer-readable medium that stores at least one trigger condition for each of a plurality of different types of threats associated with the aircraft, and modeled using a common schema. A processor computes plural different projected trajectories representing different possible aircraft paths through spacetime. The processor associates at least some of the plurality of the threats to specific trigger points in spacetime along each of the projected trajectories. The processor will deprecate ones of the projected trajectories when they are deemed not viable to recover from a threat. The processor initiates an aircraft protective response when all projected trajectories but one have been deprecated and the aircraft is within a predetermined proximity to the closest trigger point in spacetime along the non-deprecated trajectory.

First claim

What is claimed is:

1. An aircraft threat envelope protection system, comprising:
a threat envelope data structure embodied in a computer-readable medium that stores a plurality of trigger conditions, each of the plurality of trigger conditions associated with at least one threat of a plurality of different types of threats associated with an aircraft,
wherein each of the plurality of different types of threats is parameterized using a common schema;
a processor programmed to compute a plurality of projected trajectories, each of the plurality of projected trajectories representing a different possible aircraft path through spacetime beginning from a current aircraft location;
wherein the processor is programmed to associate each of at least some of the plurality of trigger conditions obtained from the threat envelope data structure to at least one specific trigger point in spacetime along at least one of the plurality of projected trajectories;
wherein the processor is further programmed to deprecate ones of the plurality of projected trajectories during times when such ones are computed as not viable to recover from a threat associated with one of the plurality trigger conditions;
wherein the processor is further programmed to initiate an aircraft protective response when both 1) all but one of the plurality of projected trajectories have been deprecated, and 2) the aircraft is within a determined proximity to a closest trigger point in spacetime of the at least one specific trigger points along the non-deprecated projected trajectory.

2. The protection system of claim 1 wherein the processor is programmed to express each of the plurality of projected trajectories in terms used by the common schema.

3. The protection system of claim 1 wherein the common schema expresses each of the plurality of different types of threats in terms of a g-force vector and an energy state vector.

4. The protection system of claim 1 wherein the common schema expresses each of the plurality of different types of threats in terms of (a) a force normal to the longitudinal axis of the aircraft, (b) an aircraft bank angle, (c) an specific excess power of the aircraft, and (d) a flight path angle.

5. The protection system of claim 1 wherein the processor repeatedly updates the plurality of projected trajectories and the at least one specific trigger point along each of the updated plurality of projected trajectories.

6. The protection system of claim 1 wherein the threat envelope data structure stores at least one of the plurality of trigger conditions associated with an energy boundary.

7. The protection system of claim 1 wherein the threat envelope data structure stores at least one of the plurality of trigger conditions associated with a matter boundary.

8. The protection system of claim 1 wherein the aircraft protective response is selected from the group consisting of issuing an alert message to an aircraft pilot, issuing a control command to an autopilot system and combinations thereof.

9. The protection system of claim 1 further comprising an autopilot system coupled to the processor and operable to carry out the aircraft protective response automatically when both 1) all but one of the plurality of projected trajectories have been deprecated, and 2) the aircraft is within the determined proximity to the closest trigger point in spacetime of the at least one specific trigger points along the non-deprecated projected trajectory.

10. The protection system of claim 1 wherein the processor is programmed to iteratively compute the plurality of projected trajectories, with each iteration beginning at a current aircraft location.

11. A method of providing aircraft threat envelope protection for an aircraft, comprising:
populating a threat envelope data structure embodied in a computer-readable medium to store a plurality of trigger conditions, each of the plurality of trigger conditions associated with at least one threat of a plurality of different types of threats associated with the aircraft,
wherein each of the plurality of different types of threats is parameterized using a common schema;
computing a plurality of projected trajectories, each of the plurality of projected trajectories representing a different possible aircraft path through spacetime beginning from a current aircraft location;
associating each of at least some of the plurality of trigger conditions obtained from the threat envelope data structure to at least one specific trigger point in spacetime along at least one of the plurality of projected trajectories;
deprecating ones of the plurality of projected trajectories during times when such ones are computed as not viable to recover from a threat associated with one of the plurality trigger conditions;
initiating an aircraft protective response when both 1) all but one of the plurality of projected trajectories have been deprecated, and 2) the aircraft is within a determined proximity to a closest trigger point in spacetime of the at least one specific trigger points along the non-deprecated projected trajectory.

12. The method of claim 11 wherein each of the plurality of projected trajectories is expressed in terms used by the common schema.

13. The method of claim 11 wherein the common schema expresses each of the plurality of different types of threats in terms of (a) a force affecting trajectory of the aircraft and (b) an energy state of the aircraft.

14. The method of claim 11 wherein the common schema expresses each of the plurality of different types of threats in terms of a g-force vector and an energy state vector.

15. The method of claim 11 wherein the common schema expresses each of the plurality of different types of threats in terms of (a) a force normal to the longitudinal axis of the aircraft, (b) an aircraft bank angle, (c) an excess specific power of the aircraft, and (d) a flight path angle.

16. The method of claim 11 further comprising repeatedly updating the plurality of projected trajectories and the at least one specific trigger point along each of the updated plurality of projected trajectories.

17. The method of claim 11 wherein the threat envelope data structure stores at least one of the plurality of trigger conditions associated with an energy boundary.

18. The method of claim 11 wherein the threat envelope data structure stores at least one of the plurality of trigger conditions associated with a matter boundary.

19. The method of claim 11 wherein the aircraft protective response is selected from the group consisting of issuing an alert message to an aircraft pilot, issuing a control command to an autopilot system and combinations thereof.

20. The method of claim 11 further comprising iteratively computing the plurality of projected trajectories, with each iteration beginning at a current aircraft location.

21. A method of providing aircraft threat envelope protection for an aircraft, comprising:
populating a threat envelope data structure embodied in a computer-readable medium to store a plurality of trigger conditions, each of the plurality of trigger conditions associated with at least one threat of a plurality of different types of threats associated with the aircraft,
wherein each of the plurality of different types of threats is parameterized using a common schema;
iteratively computing pluralities of projected trajectories, each iteration of the pluralities of projected trajectories computing a plurality of different possible aircraft paths throug

Assignees

• Gulfstream Aerospace Corp

Inventors

• Prosser Kevin
• Landers Thomas
• Vaidya Abhishek
• Sakhaei Alborz
• Finlayson Blake

Classifications

• G08G5/74

  for monitoring terrain · CPC title

• G08G5/723

  from the aircraft · CPC title

• G08G5/21 Primary

  located onboard the aircraft · CPC title

• G08G5/80 Primary

  Anti-collision systems · CPC title

• G08G5/0086

  Physics · mapped topic