GPS based terrain referenced navigation system

• US 20020188386A1
• Filed: 05/07/2002
• Published: 12/12/2002
• Est. Priority Date: 05/09/2001
• Status: Abandoned Application

• Current Assignee: BAE Systems Plc
• Original Assignee: BAE Systems Plc
• Inventors: Day, Laurence
• Application Number:
  US10/139,626
• Publication Number:
  US 20020188386A1
• Time in Patent Office: Days
• US Class Current: 701/4
• CPC Class Codes: G01S 13/86 Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
• CPC Class Codes: G01S 13/935 for terrain-avoidance
• CPC Class Codes: G01S 19/15 Aircraft landing systems
• CPC Class Codes: G01S 19/47 the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial
• CPC Class Codes: G01S 19/50 whereby the position solution is constrained to lie upon a particular curve or surface, e.g. for locomotives on railway tracks

Abstract

The terrain referenced navigation system uses data from a global positioning system (GPS) to determine a vehicles position, velocity and height above ground. The system uses input data from an altimeter device, a digital terrain elevation data, and a GPS position, velocity and time data. The system applies a GPS error process model in addition to a TRN measurement model, to obtain a state vector which includes estimates of current errors in the GPS data. The PVT data input from a GPS receiver is used to determine a current vehicle position and height in geographic axis. Using specifically constructed Kalman filter states, a geographical position and height of the vehicle is reference to the digital terrain elevation data, and an estimated ground clearance at the vehicle position is determined. The ground clearance is differenced with a radar altimeter output, and the residual is processed by Kalman filter to determine a new state vector, including estimates of current errors in the GPS data. The output can be configured to be either referenced to navigation axis, or to the digital terrain database for use by other digital terrain system functions.

Claims

1. A global positioning system based terrain referenced navigation system comprising:

at least one data processor;

a memory device, configured to communicate with said processor for storage of data;

a global positioning system interface capable of receiving 3-dimensional position, velocity and time data from a global positioning system;

an altimeter interface capable of receiving altitude data from an altimeter device;

a digital terrain elevation data interface capable of receiving digital terrain elevation data.

2. The system as claimed in claim 1, wherein said memory device and data processor are configured to:

store digital terrain elevation data;

apply a terrain referenced navigation measurement model to said digital terrain elevation data;

apply said terrain referenced navigation measurement model to said altitude data;

input a result of said terrain referenced navigation measurement model on said altitude and digital terrain elevation data into a global positioning system error process model;

input said global positioning system position, velocity and time data into said global positioning system error process model; and

produce an error processed output of said global positioning system, position, velocity and time data and said terrain referenced navigation measurement model data.

3. A method of terrain referencing of navigation data, said navigation data produced by a global positioning system, said method comprising the steps of:

inputting global positioning system position, velocity and time data from a global positioning receiver system;

determining a current geographical position data and height data of a vehicle in geographic axes from said data input from said global positioning system;

referencing said determined geographical position data and height data to a digital terrain elevation data using Kalman filter states;

determining an estimated ground clearance of said vehicle at a current position of said vehicle;

obtaining a difference between said estimated ground clearance of said vehicle at said current position, and an altimeter data received from an altimeter data source; and

processing said difference by a Kalman filter to determine an estimate of current errors in said global positioning system data.

4. The method as claimed in claim 3, wherein said estimate of current errors in said global positioning system data are determined as a vector data.

5. A method of producing terrain referenced navigation data from data inputs including:

digital terrain elevation data;

altitude data; and

position, velocity and time data,

said method comprising the processes of;

storing said digital terrain elevation data;

applying a terrain referenced navigation measurement model to said digital terrain elevation data;

applying a terrain referenced navigation measurement model to said altitude data;

applying a global positioning system error processing model to an output of said terrain referenced navigation measurement model and said position, velocity and time data; and

generating an error corrected output of said position, velocity and time data.

6. A method of error correcting an output of a global positioning system using attitude data output of a radio altimeter, and terrain elevation data, said method comprising the processes of:

receiving a 3-dimensional position, velocity and time data from said global positioning system;

receiving said altitude data from said altimeter device;

receiving said terrain elevation data; and

applying a global positioning system error process model to said 3-dimensional position, velocity and time data, wherein said error process model applies said altitude data and said terrain elevation data to said 3-dimensional position, velocity and time data to produce a terrain referenced position, velocity and time data output.

7. The method as claimed in claim 6, comprising the processes of;

applying a terrain referenced navigation measurement model to said terrain elevation data;

applying said terrain reference navigation measurement model to said altitude data;

inputting a result of said terrain referenced navigation measurement model on said altitude and terrain elevation data into said global positioning system error process model;

inputting said 3-dimensional position, velocity and time data into said global positioning system error process model; and

producing a global positioning system error processed output of said global positioning system position, velocity and time data and said terrain referenced navigation measurement model.