System for correlation and recognition of terrain elevation

• US 4,584,646 A
• Filed: 06/29/1983
• Issued: 04/22/1986
• Est. Priority Date: 06/29/1983
• Status: Expired due to Term

• Current Assignee: Harris Corporation Melbourne
• Original Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Inventors: Chan, Luen C., Snyder, Franklin B.
• Primary Examiner(s): Chin, Gary
• Application Number:
  US06/509,052
• Time in Patent Office: 1,028 Days
• Field of Search: 364/433, 364/443, 364/449, 364/460, 364/423, 364/728, 244/3.15-3.18, 73/178 R, 343/5 MM, 343/5 DP, 343/7 TA, 343/378
• US Class Current: 701/207
• CPC Class Codes: G01C 21/005 with correlation of navigation data from several sources, e.g. map or contour matching G01C21/30 takes precedence

Abstract

In a dead reckoning navigation system a correlation scheme that operates in the frequency domain (using a discrete cosine transform (DCT) function) is implemented separately from the navigation system to determine a two-dimensional position error estimate. In this separate processing system measured terrain data is correlated (in the frequency domain) with reference elevation stored in map format (as by way of a digital map generator (DMG)). The results of this correlation are then employed to enhance the independently operated dead reckoning navigation system so that an accurate determination of geographic position may be obtained.

Claims

1. For use with a vehicle guidance system in which geographic position data is supplied from a navigation system, an arrangement for providing said navigation system with error estimates in geographic position data supplied thereby comprising:

first means for generating first signals representative of a discrete cosine transform function based upon the measured elevation of the terrain at the geographic position of the vehicle; and

second means for correlating, in the discrete cosine transform domain, the first signals generated by said first means with a set of second signals representative of respective discrete cosine transform functions based upon data representative of the elevations of a plurality of geographic positions disposed about the geographic position of said vehicle as identified by data supplied from said navigation system, and producing, from said correlation of said first and second signals, third signals representative of the error estimates of position data supplied by said navigation system corresponding to said identified geographic position, a selected one of said third signals being coupled to said navigation system for updating the information processed thereby for the guidance of said vehicle.

2. An arrangement according to claim 1, wherein said vehicle guidance system includes means for storing elevation data in the form of a terrain profile map encompassing a prescribed geographical area within which the travel path of said vehicle is located, and for extracting from said map data representative of the elevations of said plurality of geographic positions.

3. An arrangement according to claim 1, wherein said second means comprises means for producing as said third signals, signals representative of the expression ##EQU5## wherein:

Δ

x and Δ

y are respective orthogonal offsets corresponding to the displacements in orthogonal geographic directions among adjacent ones of said plurality of geographic positions,

W(k) and W'"'"'(k) are frequency weighting coefficients,

C(k) corresponds to said first signals;

C'"'"'(k,Δ

x,Δ

y) corresponds to said second signals; and

K₁ and K₂ define the boundaries of said frequency domain.

4. An arrangement according to claim 3, wherein said second means further comprises means for coupling to said navigation system, as said selected one of said third signals, that third signal whose value R(Δ

x,Δ

y) is maximum for said plurality of geographic positions.

5. For use with vehicle guidance system in which geographic position data is supplied from a navigation system, a method for providing said navigation system with error estimates in geographic position data supplied thereby comprising the steps of:

(a) generating first signals representative of a discrete cosine transform function based upon the measured elevation of the terrain at the geographic position of the vehicle,

(b) correlating, in the discrete cosine transform domain, the first signals generated in step (a) with a set of second signals representative of respective discrete cosine transform functions based upon data representative of the elevations of a plurality of geographic positions disposed about the geographic position of said vehicle as identified by data supplied from said navigation system, and

(c) producing, from the correlation of said first and second signals, third signals representative of the error estimates of position data supplied by said navigation system corresponding to said identified geographic position,

a selected one of said third signals being coupled to said navigation system for updating the information processed thereby for the guidance of said vehicle.

6. A method according to claim 5, wherein, within said vehicle guidance system there are stored elevation data in the form of a terrain profile map encompassing a prescribed geographical area within which the travel path of said vehicle is located, and from said map data representative of the elevations of said plurality of geographic positions are extracted.

7. A method according to claim 5, wherein step (b) comprises producing, as said third signals, signals representative of the expression ##EQU6## wherein:

Δ

x and Δ

y are respective orthogonal offsets corresponding to the displacements in orthogonal geographic directions among adjacent ones of said plurality of geographic positions,

W(k) and W'"'"'(k) are frequency weighting coefficients,

C(k) corresponds to said first signals;

C'"'"'(k,Δ

x,Δ

y) corresponds to said second signals; and

K₁ and K₂ define the boundaries of said frequency domain.

8. A method according to claim 7, wherein said selected one of said third signals is that third signal whose value R(Δ

x,Δ

y) is maximum for said plurality of geographic positions.