AIRCRAFT NAVIGATION USING THE GLOBAL POSITIONING SYSTEM, INERTIAL REFERENCE SYSTEM, AND DISTANCE MEASUREMENTS

• US 20100106416A1
• Filed: 10/28/2008
• Published: 04/29/2010
• Est. Priority Date: 10/28/2008
• Status: Abandoned Application

• Current Assignee: Universal Avionics Systems Corporation (Elbit Systems Limited)
• Original Assignee: Universal Avionics Systems Corporation (Elbit Systems Limited)
• Inventors: Yochum, Thomas E.
• Application Number:
  US12/259,489
• Publication Number:
  US 20100106416A1
• Time in Patent Office: Days
• US Class Current: 701/213
• CPC Class Codes: G01C 21/165 combined with non-inertial navigation instruments
• CPC Class Codes: G01S 19/11 wherein the cooperating elements are pseudolites or satellite radio beacon positioning system signal repeaters
• CPC Class Codes: G01S 19/15 Aircraft landing systems
• CPC Class Codes: G01S 19/49 whereby the further system is an inertial position system, e.g. loosely-coupled

Abstract

A navigation technique for a vehicle employs an inertial reference system to derive a first position indication and a first velocity value. A first receiver processes signals of a global positioning system from which a second position indication and a second velocity value are derived. A second receiver processes signals from a plurality of distance measuring equipment stations at fixed positions on the earth and determines the distance between the vehicle and each of those stations. A third position indication is derived from those distances. A Kalman filter function is applied to the first, second and third position indications and to the first and second velocity values to compensate for uncertainty in the first position indication and in the first velocity value and thereby produce a vehicle position estimate and a vehicle velocity estimate.

Claims

1. A navigation system for a vehicle comprising:

an inertial reference system onboard the vehicle and producing a first set of data from which a first position indication is produced;

a first receiver, onboard the vehicle, for signals of a global positioning system and producing a second set of data from which a second position indication is produced;

a second receiver, onboard the vehicle, for receiving signals from a plurality of distance measuring equipment stations located at fixed positions on the earth and in response thereto producing a third set of data denoting distances between the vehicle and each distance measuring equipment station, from which third set of data a third position indication is produced; and

a processor that employs the second and third position indications to compensate for uncertainty in the first position indication and thereby produce a position estimate.

2. The navigation system as recited in claim 1 wherein the processor applies a recursive data processing algorithm to the first, second and third position indications.

3. The navigation system as recited in claim 1 wherein the processor applies a Kalman filter to the first, second and third position indications.

4. The navigation system as recited in claim 1 wherein:

the first set of data from the first receiver is employed to produce a first velocity value;

the second set of data from the second receiver is employed to produce a second velocity value; and

the processor employs the second velocity value to compensate for uncertainty in the first velocity value and thereby produce a velocity estimate.

5. The navigation system as recited in claim 4 wherein the processor employs a recursive data processing algorithm to the first, second and third position indications and to the first and second velocity values.

6. The navigation system as recited in claim 4 wherein the processor applies a Kalman filter to the first, second and third position indications and to the first and second velocity values.

7. The navigation system as recited in claim 1 further comprising a database of information related to distance measuring equipment stations within a geographical area;

and a mechanism that selects, from the database, the plurality of distance measuring equipment stations and tunes the second receiver to each one of the plurality of distance measuring equipment stations.

8. A navigation method for a vehicle comprising:

providing an inertial reference system onboard the vehicle which produces a first set of data;

deriving a first position indication from the first set of data;

receiving, via a receiver onboard the vehicle, signals of a global positioning system and in response thereto producing a second set of data;

deriving a second position indication from the second set of data;

receiving, via a transceiver onboard the vehicle, signals from a plurality of distance measuring equipment stations at fixed positions on the earth and in response thereto producing a third set of data denoting distances between the vehicle and each distance measuring equipment station;

deriving a third position indication from the second third of data; and

employing the second and third position indications in a processor to compensate for uncertainty in the first position indication and thereby produce a position estimate.

9. The navigation method as recited in claim 8 wherein employing the second and third position indications applies a Kalman filter function to the first, second and third position indications.

10. The navigation method as recited in claim 8 further comprising:

deriving a first velocity value from the first set of data;

deriving a second velocity value from the second set of data; and

employing the second velocity value in the processor to compensate for uncertainty in the first velocity value and thereby produce a velocity estimate.

11. The navigation method as recited in claim 10 wherein employing the second velocity value applies a Kalman filter function to the first and second velocity values.

12. The navigation method as recited in claim 8 wherein receiving signals from a plurality of distance measuring equipment stations comprises sequentially tuning the transceiver to each of the plurality of distance measuring equipment stations and transmitting an interrogation signal.

13. A navigation method for a vehicle comprising:

providing an inertial reference system onboard the vehicle which produces a first position indication and a first velocity value;

receiving, onboard the vehicle, signals of a global positioning system and in response thereto producing a second position indication and a second velocity value;

receiving, onboard the vehicle, signals from a plurality of distance measuring equipment stations at fixed positions on the earth and in response thereto producing a third position indication; and

applying a Kalman filter function to the first, second, and third position indications and to the first and second velocity values to compensate for uncertainty in the first position indication and in the first velocity value and thereby produce a vehicle position estimate and a vehicle velocity estimate.

14. The navigation method as recited in claim 13 wherein receiving signals from a plurality of distance measuring equipment stations comprises sequentially tuning a transceiver to each such station, transmitting an interrogation signal to each such station, and receiving a reply signal.

15. The navigation method as recited in claim 13 wherein receiving signals from a plurality of distance measuring equipment stations further comprises determining from those signals distances between the vehicle and each distance measuring equipment station;

and deriving the third position indication from the distances.