Method of operating a vehicle

Patent metadata

Field	Value
Publication number	US-11480260-B2
Application number	US-201916459848-A
Country	US
Kind code	B2
Filing date	Jul 2, 2019
Priority date	Jul 2, 2019
Publication date	Oct 25, 2022
Grant date	Oct 25, 2022

Abstract

A method of operating a vehicle includes navigating the vehicle along a path, collecting a set of navigation parameters of the vehicle from at least one of a sensor, a global positioning system, or an inertial reference system, determining a set of statistical uncertainties related to at least some navigation parameters in the set of navigation parameters, and associating a set of statistical weights to the at least some navigation parameters.

First claim

What is claimed is:

1. A method of operating a vehicle, the method comprising:
collecting a set of navigation parameters of the vehicle from at least one of a sensor, a global positioning system, or an inertial reference system;
applying a correction to each navigation parameter in the set of navigation parameters to determine a corresponding set of preliminary navigational solutions;
determining a statistical uncertainty corresponding to each preliminary navigational solution in the set of preliminary navigational solutions to define a set of statistical uncertainties;
associating a statistical weight to each navigation parameter in the set of navigation parameters, based on the set of statistical uncertainties, to define a set of statistical weights;
blending the set of preliminary navigational solutions, based on the set of statistical weights, to determine a single navigational solution for the vehicle; and
operating the vehicle in accordance with the single navigational solution.

2. The method of claim 1 , wherein the applying the correction is performed via a Kalman filter.

3. The method of claim 2 , further comprising determining a set of errors for the set of preliminary navigational solutions, wherein each error in the set of errors corresponds to a preliminary navigational solution in the set of preliminary navigational solutions.

4. The method of claim 3 wherein each statistical uncertainty in the set of statistical uncertainties corresponds to an error in the set of errors.

5. The method of claim 4 wherein the set of preliminary navigational solutions is determined prior to determining the set of errors, wherein the set of errors is determined prior to determining the set of statistical uncertainties, wherein the set of statistical weights is associated prior to determining the single navigational solution, and further comprising determining an overall uncertainty for the single navigational solution.

6. The method of claim 2 wherein the set of preliminary navigational solutions comprises at least one of a current position or a current velocity of the vehicle.

7. The method of claim 1 wherein the single navigational solution comprises an optimized single navigational solution based on the set of statistical weights.

8. The method of claim 1 wherein the set of navigation parameters comprises at least one of a position, a velocity, a heading, or a reference frame.

9. The method of claim 1 wherein the operating further comprises displaying at least one of an estimate of position uncertainty, an actual navigation performance, or a required navigation performance.

10. The method of claim 9 , further comprising comparing an estimate of position uncertainty to a required navigation performance, and wherein the displaying comprises a displayed alert when the estimate of position uncertainty is greater than the required navigation performance.

11. The method of claim 1 , further comprising automatically transmitting the single navigational solution to a vehicle management system.

12. The method of claim 1 , further comprising altering a current path based on the single navigational solution.

13. A method of operating an aircraft, the method comprising:
collecting a set of navigation parameters of the aircraft from at least one of a sensor, a global positioning system, or an inertial reference system;
applying a correction, by way of a Kalman filter, to each navigation parameter in the set of navigation parameters to determine a corresponding set of preliminary navigational solutions;
determining a set of errors for the set of preliminary navigational solutions;
determining, by a covariance matrix, a statistical uncertainty for each error in the set of errors to define a set of statistical uncertainties;
associating a statistical weight to each navigation parameter in the set of navigation parameters, based on the set of statistical uncertainties, to define a set of statistical weights;
blending the set of preliminary navigational solutions, based on the set of statistical weights, to determine a single navigational solution for the aircraft; and
operating the aircraft in accordance with the single navigational solution.

14. The method of claim 13 wherein the set of preliminary navigational solutions comprises at least one of a position of the aircraft or a velocity of the aircraft.

15. The method of claim 13 , further comprising determining an overall uncertainty for the single navigational solution based on the set of statistical weights.

16. The method of claim 15 wherein the overall uncertainty comprises an estimate of position uncertainty for the aircraft.

17. The method of claim 13 wherein the operating further comprises displaying at least one of an estimate of position uncertainty, an actual navigation performance, or a required navigation performance.

18. The method of claim 13 , further comprising comparing an estimate of position uncertainty to a required navigation performance, and wherein the operating comprises a displayed alert when the estimate of position uncertainty is greater than the required navigation performance.

19. The method of claim 13 , further comprising altering a current flight path based on the single navigational solution.

Assignees

• Ge Aviation Systems Llc

Inventors

• Karatsinides Spiro P
• Stark Gregory A

Classifications

• G01S5/0278

  involving statistical or probabilistic considerations (G01S5/0252, G01S5/0294 take precedence) · CPC title

• F16K15/028

  the valve member consisting only of a predominantly disc-shaped flat element · CPC title

• G01C21/165 Primary

  combined with non-inertial navigation instruments · CPC title

• F16K31/0658

  Armature and valve member being one single element · CPC title

• F16K31/082

  using a electromagnet and a permanent magnet · CPC title