Inertial navigation with gravity deflection compensation

• US 5,774,832 A
• Filed: 04/19/1996
• Issued: 06/30/1998
• Est. Priority Date: 04/19/1996
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Vanderwerf, Kevin D.
• Primary Examiner(s): ZANELLI, MICHAEL J
• Application Number:
  US08/633,978
• Time in Patent Office: 802 Days
• Field of Search: 701/220, 701/221, 73/1.38, 364/571.03, 364/571.04, 364/577, 33/320, 33/317 D, 707/101, 707/104
• US Class Current: 701/220
• CPC Class Codes: G01C 21/166 Mechanical, construction or arrangement details of inertial navigation systems
• CPC Class Codes: G01P 7/00 Measuring speed by integrating acceleration measuring travelled distance by double integration of acceleration G01C21/16

Abstract

The novel navigation system, suited for commercial aircraft, includes a sensor for outputting a signal representing a first navigation parameter, a memory having condensed gravity compensation data, and a processor for deriving a second navigational parameter. The processor derives the second navigational parameter from the signal and a subset of the condensed compensation data based on aircraft position. The condensed memory, based on regional gravity deflections, stores sequential gravity compensation values and corresponding navigational coordinates. To conserve memory, adjacent compensation values differ by at least a preset gravity compensation increment. The compensation increment, based on a gravity deflection between 30 and 100 micro-radians, is adequate for commercial aircraft.

Claims

1. A navigation system for mounting to a vehicle, the system comprising:

an inertial sensor for sensing a first navigational parameter of the vehicle and outputting a sensor signal representing the first parameter;

a memory having gravity compensation data for a geographic region; and

a processor coupled to the inertial sensor and the memory, the processor including;

means for accessing a subset of the gravity compensation data, based on position of the vehicle; and

means for deriving a second navigational parameter, based on the sensor signal and the subset of gravity compensation data.

2. The system of claim 1

wherein the geographic region includes an ordered sequence of rectangular subregions having a common longitude, a respective latitude, and a respective gravity deflection;

and

wherein the gravity compensation data includes a plurality of sequential gravity compensation values, each value based on a gravity deflection of a subregion of the plurality and differing from an adjacent value by at least a preset gravity compensation increment.

3. The system of claim 2 wherein the preset gravity compensation increment is based on a gravity deflection with a magnitude between 30 and 100 micro-radians.

4. The system of claim 2 wherein the gravity compensation data includes a plurality of sequential latitudes, each latitude corresponding to the respective latitude of a subregion of the plurality of rectangular subregions.

5. The system of claim 4 wherein each gravity compensation value is paired with its respective latitude.

6. The system of claim 4

wherein the means for accessing a subset of the gravity compensation data includes means for searching the plurality of sequential latitudes for a set of latitudes corresponding to a latitude of the vehicle;

and

wherein the means for deriving the second navigational parameter includes;

means for interpolating a new gravity compensation value from the subset of gravity compensation values; and

means for adding the new gravity compensation value to the first navigational parameter.

7. The system of claim 1 wherein the inertial sensor is an accelerometer, the first navigational parameter is an acceleration, and the second navigational parameter is a velocity.

8. The system of claim 1 wherein the second navigational parameter is a position.

9. The system of claim 1 wherein the gravity compensation data is condensed.

10. The system of claim 9 wherein the gravity compensation data includes a plurality of sequential gravity compensation values, each value based on a gravity deflection of a subregion of the geographic region and each value differing from an adjacent value.

11. The system of claim 10 wherein each value differs from an adjacent value by at least a preset gravity compensation increment.

12. The system of claim 11 wherein the preset gravity compensation increment is based on a gravity deflection having a magnitude between 30 and 100 micro-radians.

13. The system of claim 11 wherein the gravity compensation data includes a plurality of sequential navigation coordinates, each coordinate corresponding to a value of the plurality of sequential gravity compensation values.

14. The system of claim 1

wherein the region includes an ordered sequence of rectangular subregions having a common longitude, a respective latitude, and a respective gravity deflection;

and

wherein the gravity compensation data includes a plurality of sequential gravity compensation values, each value based on a gravity deflection of at least one of the subregions, the plurality including;

a first value based on the gravity deflection of a first subregion of the plurality;

a second value based on the gravity deflection of the nearest subregion having a gravity deflection different from that of the first subregion; and

a third value based on the gravity deflection of the second nearest subregion having a gravity deflection different from that of the second value.

15. The system of claim 1 further including:

a flight management system coupled to the processor; and

a navigational display coupled to the processor.

16. A method of condensing gravity compensation data for use in a navigation system having a compensation memory, the method comprising:

storing a plurality of sequential gravity compensation values to a first memory, each value having an associated navigational coordinate corresponding to a geographic region;

storing a first gravity compensation value of the plurality to a first location of the compensation memory;

searching the plurality of values for a nearest different sequential value, the nearest different sequential value differing from the first value by at least a preset gravity compensation increment; and

storing the nearest different sequential value to a second location of the compensation memory.

17. The method of claim 16 further including:

storing the navigational coordinate associated with the first value to the first location; and

storing the navigational coordinate associated with the nearest different sequential value to the second location.

18. The method of claim 17 further including:

(1) searching the plurality of values for a second nearest different sequential value, the second nearest different value differing from the previous nearest different sequential value by at least the preset gravity compensation increment;

(2) storing the second nearest different sequential value and its associated navigational coordinate to another location of the compensation memory; and

(3) repeating steps (1) and (2) successively, until step (1) reaches a last value of the plurality of sequential gravity compensation values.

19. The method of claim 16 wherein storing the plurality of sequential gravity compensation values includes filtering the plurality to reduce high-frequency content.

20. The method of claim 16 wherein storing the plurality of sequential gravity compensation values includes quantizing the gravity compensation values, based on the preset gravity compensation increment.

21. The method of claim 16 wherein storing the plurality of sequential gravity compensation values includes reducing the number of values in the plurality of gravity compensation values.

22. The method of claim 16 wherein the preset gravity compensation increment is based on a gravity deflection having a magnitude between 30 and 100 micro-radians.

23. A method of compensating gravity deflection in a navigation system having a sensor for determining a navigational parameter of a vehicle, the method comprising:

storing a plurality of sequential gravity compensation values to a compensation memory, each value having an associated navigational coordinate corresponding to a region of earth;

accessing a subset of the plurality of gravity compensation values, based on position of the vehicle; and

compensating the navigational parameter, based on the subset of gravity compensation data.

24. The method of claim 23

wherein accessing a subset of the gravity compensation values includes searching for gravity compensation values corresponding to regions near the position of the vehicle;

and

wherein compensating the navigational parameter includes;

interpolating the subset of the plurality of gravity compensation values to determine a gravity compensation value for the position of the vehicle; and

adding the gravity compensation value to the navigational parameter.

25. The method of claim 24 wherein storing the plurality of sequential gravity compensation values to the compensation memory includes:

storing a first gravity compensation value of the plurality and the navigational coordinate associated with the first value to a first location of the compensation memory;

searching the plurality of values for a nearest different sequential value, the nearest different sequential value differing from the first value by at least a preset gravity compensation increment; and

storing the nearest different sequential value and the navigational coordinate associated with the nearest different sequential value to a second location of the compensation memory;

(1) searching the plurality of values for a second nearest different sequential value, the second nearest different value differing from the previous nearest different sequential value by at least the preset gravity compensation increment;

(2) storing the second nearest different sequential value and its associated navigational coordinate to another location of the compensation memory; and

(3) repeating steps (1) and (2) successively, until step (1) reaches a last value of the plurality of sequential gravity compensation values.

26. The method of claim 23 wherein storing the plurality of sequential gravity compensation values includes:

filtering the plurality to reduce high-frequency content;

quantizing the gravity compensation data, based on the preset gravity compensation increment; and

reducing the number of values in the plurality of gravity compensation values by redefining the regions of the plurality of regions.

27. The system of claim 23 wherein the preset gravity compensation increment is based on a gravity deflection having a magnitude between 30 and 100 micro-radians.