Piecewise recovery system

Patent metadata

Field	Value
Publication number	US-11990049-B2
Application number	US-201916552620-A
Country	US
Kind code	B2
Filing date	Aug 27, 2019
Priority date	Aug 27, 2018
Publication date	May 21, 2024
Grant date	May 21, 2024

Abstract

A projected recovery trajectory for an aircraft autopilot system is precomputed by providing a stored set of predefined recovery mode segments, including: a mode 1 segment that models the aircraft coasting; a mode 2 segment that models the aircraft executing a nose high recovery; a mode 3 segment that models the aircraft executing a nose low recovery; a mode 4 segment that models the aircraft executing a throttle only recovery; and a mode 5 segment that models the aircraft executing a terrain avoidance recovery. A processor generates at least one projected recovery trajectory based on a current state of the aircraft, where the processor selectively concatenates selected ones of the predefined recovery mode segments into a sequence and uses that sequence to generate the projected trajectory.

First claim

What is claimed is:

1. A method of precomputing a projected recovery trajectory for an aircraft autopilot system, comprising:
providing a stored set of predefined recovery mode segments, including:
a mode 1 segment that models an aircraft coasting;
a mode 2 segment that models the aircraft executing a nose high recovery;
a mode 3 segment that models the aircraft executing a nose low recovery;
a mode 4 segment that models the aircraft executing a throttle only recovery;
a mode 5 segment that models the aircraft executing a terrain avoidance recovery;

using a processor to generate at least one projected recovery trajectory based on a current in-flight state of the aircraft and a predicted future state of the aircraft as it executes a recovery, where the processor concatenates selected ones of the predefined recovery mode segments into a sequence and uses that sequence to generate a projected trajectory, such that the progress of one recovery mode segment determines which subsequent recovery mode segment will follow, if any.

2. The method of claim 1 wherein the processor selects the mode 1 segment as a first segment in the sequence to generate the projected trajectory.

3. The method of claim 1 wherein the processor selects the mode 5 segment as a last segment in the sequence to generate the projected trajectory.

4. The method of claim 1 wherein the processor selectively concatenates one or more of modes 2, 3 and 4 and places them between the mode 1 segment and the mode 5 segment.

5. The method of claim 1 wherein the processor selectively concatenates one or more of modes 2 and 3 and places them between the mode 1 segment and the mode 5 segment.

6. The method of claim 1 wherein the processor selectively concatenates one or more of modes 2 and 4 and places them between the mode 1 segment and the mode 5 segment.

7. The method of claim 1 wherein the processor iteratively generates a plurality of projected trajectories each having a plurality of sequences.

8. The method of claim 1 wherein the processor iteratively generates a plurality of sequences, each sequence being calculated relative to a different predicted future state of the aircraft during an execution of a recovery sequence.

9. The method of claim 1 wherein a plurality of the predefined recovery mode segments are based on plural different types of hazards each modeled using common schema.

10. An apparatus for precomputing a projected recovery trajectory for an aircraft autopilot system, comprising:
a computer-readable medium configured to store a set of predefined recovery mode segments, including:
a mode 1 segment that models an aircraft coasting;
a mode 2 segment that models the aircraft executing a node high recovery;
a mode 3 segment that models the aircraft executing a nose low recovery;
a mode 4 segment that models the aircraft executing a throttle only recovery;
a mode 5 segment that models the aircraft executing a terrain avoidance trajectory;

a processor programmed to generate at least one projected recovery trajectory based on a current in-flight state of the aircraft, and a predicted future state of the aircraft as it executes a recovery, where the processor is programmed to access said computer-readable medium and to concatenate selected one of the predefined recovery mode segments into a sequence and uses that sequence to generate a projected trajectory, such that the progress of one recovery mode segment determines which subsequent recovery mode segment will follow, if any.

11. The apparatus of claim 10 wherein the processor is programmed to select the mode 1 segment as a first segment in the sequence to generate the projected trajectory.

12. The apparatus of claim 10 wherein the processor is programmed to select the mode 5 segment as a last segment in the sequence to generate the projected trajectory.

13. The apparatus of claim 10 wherein the processor is programmed to selectively concatenate one or more of modes 2, 3 and 4 and places them between the mode 1 segment and the mode 5 segment.

14. The apparatus of claim 10 wherein the processor is programmed to selectively concatenate one or more of modes 2 and 3 and places them between the mode 1 segment and the mode 5 segment.

15. The apparatus of claim 10 wherein the processor is programmed to selectively concatenate one or more of modes 2 and 4 and places them between the mode 1 segment and the mode 5 segment.

16. The apparatus of claim 10 wherein the processor iteratively generates a plurality of sequences used to generate a plurality of projected trajectories.

17. The apparatus of claim 10 wherein the processor iteratively generates a plurality of sequences each sequence being calculated relative to a different predicted future state of the aircraft during an execution of a recovery sequence.

18. The apparatus of claim 10 wherein a plurality of the predefined recovery mode segments are based on plural different types of hazards each modeled using common schema.

19. A method of precomputing a projected recovery trajectory for an aircraft autopilot system, comprising:
providing a stored set of predefined recovery mode segments; and
using a processor to generate at least one projected recovery trajectory based on a current in-flight state of an aircraft and a predicted future state of the aircraft as it executes a recovery, where the processor concatenates selected ones of the predefined recovery mode segments into a sequence and uses that sequence to generate the projected trajectory, such that the progress of one recovery mode segment determines which subsequent recovery mode segment will follow, if any.

20. An apparatus for precomputing a projected recovery trajectory for an aircraft autopilot system, comprising:
a computer-readable medium configured to store a set of predefined recovery mode segments; and
a processor programmed to generate at least one projected recovery trajectory based on a current in-flight state of an aircraft and a predicted future state of the aircraft as it executes a recovery, where the processor concatenates selected ones of the predefined recovery mode segments into a sequence and uses that sequence to generate a projected trajectory, such that the progress of one recovery mode segment determines which subsequent recovery mode segment will follow, if any.

Assignees

• Gulfstream Aerospace Corp

Inventors

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

Classifications

• B64D45/00 Primary

  Aircraft indicators or protectors not otherwise provided for · CPC title

• G05D1/81 Primary

  Handing over between on-board automatic and on-board manual control · CPC title

• G08G5/59

  in accordance with predefined flight zones, e.g. to avoid prohibited zones · CPC title

• G08G5/58

  for emergency situations, e.g. hijacking or bird strikes · CPC title

• G08G5/55

  for a single aircraft · CPC title