Self-contained method for correction of an inertial system over a body of water

• US 5,345,241 A
• Filed: 12/07/1992
• Issued: 09/06/1994
• Est. Priority Date: 12/07/1992
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Litton Systems Incorporated
• Inventors: Huddle, James R.
• Primary Examiner(s): Barron, Jr., Gilberto
• Application Number:
  US07/986,333
• Time in Patent Office: 638 Days
• Field of Search: 342/63, 342/64, 342/120, 342/121, 364/453, 364/454, 364/456, 364/457
• US Class Current: 342/63
• CPC Class Codes: G01C 21/005 with correlation of navigation data from several sources, e.g. map or contour matching G01C21/30 takes precedence
• CPC Class Codes: G01C 21/188 for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems

Abstract

A method and apparatus for performing on-board corrections to the computed navigation variables of an inertial system on an aircraft while flying over a body of water. Onboard instruments, including a barometric altimeter and a radar altimeter, measure the vertical distance of the aircraft above an ellipsoidal model of the earth and above the body of water respectively. An on-board computer calculates the differences between such heights over a plurality of points along the path the aircraft travels over the water as indicated by its inertial navigation system. The differences are compared with a map of the undulation of the geoid encompassing the region to determine the deviation of the navigated course from the true course. Appropriate corrections to the aircraft'"'"'s inertial system may then be made to reduce error.

Claims

1. An on-board method for the correction of the inertial system of an aircraft as it proceeds on a course over a region of a body of water comprising the steps of:

a) continuously determining the location of a point horizontally along said course by means of said aircraft'"'"'s inertial navigation system; and

b) measuring the vertical distance of said aircraft, at said point, above an ellipsoidal model of a geoid that includes said region; and

c) measuring the vertical distance of said aircraft, at said point, above the surface of said body of water;

then

d) computing the difference between the values measured in steps b and c to determine the measured undulation of said geoid at said point;

then

e) comparing said measured undulation of said geoid with the undulation of said geoid at said point as determined by gravitational surveys;

then

f) repeating steps a through e;

then

g) determining a position correction by correlating said measured undulation values with values pre-determined by said survey; and

then

h) adjusting at least one of the aircraft'"'"'s inertial navigation system variable computations by means of said position correction.

2. A method as defined in claim 1 further including the step of measuring the vertical distance of said aircraft above said ellipsoidal model of the earth by means of a barometric altimeter.

3. A method as defined in claim 1 further including the step of measuring the vertical distance of said aircraft above said body of water by means of a radar altimeter.

4. A method as defined in claim 1 further including the step of correlating said measured and survey values of undulations by means of an on-board computer.

5. Apparatus for correcting at least one of the inertial system computed navigation variables of an aircraft while proceeding over a region of a body of water comprising, in combination:

a) means for measuring the vertical distance of said aircraft above an ellipsoidal model of the earth;

b) means for measuring the vertical distance of said aircraft above said body of water;

c) means for computing the difference between said vertical distances;

d) means for storing a map of the undulation of the geoid of said region; and

e) means for comparing a plurality of said differences with said map of the undulation of the geoid of said region, correlating said differences with said map and adjusting at least one of said aircraft'"'"'s navigation variable computations.

6. Apparatus as defined in claim 5 wherein said means for measuring the vertical distance of said aircraft above an ellipsoidal model of the earth is a barometric altimeter.

7. Apparatus as defined in claim 5 wherein said means for measuring the vertical distance of said aircraft above said body of water is a radar altimeter.

8. Apparatus as defined in claim 5 wherein said means for comparing, correlating and adjusting is an on-board computer.