Method and apparatus for measuring gravity with lever arm correction

• US 5,728,935 A
• Filed: 08/14/1996
• Issued: 03/17/1998
• Est. Priority Date: 08/14/1996
• Status: Expired due to Term

• Current Assignee: Jozsef Czompo
• Original Assignee: Jozsef Czompo
• Inventors: Czompo, Jozsef
• Primary Examiner(s): Oda, Christine K.
• Application Number:
  US08/689,827
• Time in Patent Office: 580 Days
• Field of Search: 73/382 R, 73/382 G, 73/510, 364/420, 364/566, 33/365, 33/395
• US Class Current: 73/382.00G
• CPC Class Codes: G01V 7/16 specially adapted for use on moving platforms, e.g. ship, aircraft

Abstract

The gravimetry apparatus includes two rigidly connected accelerometer triads and a global positioning system antenna defining a kinematic reference point. The apparatus has a specific layout where the nominal center of the accelerometer triads and the kinematic reference point are collinear and the corresponding accelerometers of the two triads are parallel. In this gravimetry system, the lever arm correction is measured internally and the magnitude of gravity is calculated without the need for stabilized platforms or measurement of the spatial orientation of the gravimeter.

Claims

1. An apparatus for measuring the magnitude of gravity comprising:

a. means for measuring specific force at a first nominal center;

b. means for measuring specific force at a second nominal center;

c. kinematic acceleration measurement means for measuring kinematic acceleration at a kinematic reference point (KRP) wherein the first nominal center, second nominal center and kinematic reference point are collinear and the first nominal center and the second nominal center are each a fixed and known distance from the kinematic reference point wherein measurement of the specific force at the first and second nominal centers and kinematic acceleration at the KRP are made independently of each other;

d. means for calculating gravitational acceleration at the kinematic reference point on the basis of said independent measurement of the specific force at the first and second nominal centers and kinematic acceleration at the KRP.

2. An apparatus as in claim 1 wherein the means for measuring specific force at the first nominal center includes three virtually orthogonal accelerometers.

3. An apparatus as in claim 1 wherein the means for measuring specific force at the second nominal center includes three virtually orthogonal accelerometers.

4. An apparatus as in claim 1 wherein the means for calculating gravitational acceleration at the kinematic reference point includes a Global Positioning System (GPS) antenna and processor for calculating kinematic acceleration at the KRP.

5. An apparatus as in claim 1 wherein the means for measuring specific force at the first nominal center, means for measuring specific force at the second nominal center and the kinematic acceleration measurement means are mounted in a sensor mounting block.

6. An apparatus as in claim 1 wherein the means for calculating gravitational acceleration at the KRP includes:

a. means for estimating the difference in gravity between the KRP and first nominal center;

b. means for estimating the difference in gravity between the first and second nominal centers;

c. means for determining a corrected force at the first nominal center from the specific force at the first nominal center and the gravity difference between the KRP and the first nominal center;

d. means for determining a corrected force at the second nominal center from the specific force at the second nominal center and the gravity difference between the first and second nominal centers;

e. means for determining an interpolated specific force at the KRP from the corrected force at the first nominal center, the corrected force at the second nominal center and the distance between the KRP and first nominal center and the distance between the first and second nominal centers;

f. means for determining the gravitational acceleration at the KRP from the interpolated specific force and the kinematic acceleration at the KRP.

7. An apparatus as in claim 6 wherein the means for estimating the difference in gravity between the KRP and first nominal center and the means for estimating the difference in gravity between the first and second nominal centers includes a database of gravity values and program means for retrieving a gravity value for a given coordinate.

8. An apparatus as in claim 7 wherein the means for estimating the difference in gravity between the KRP and first nominal center and the means for estimating the difference in gravity between the first and second nominal centers includes dynamic tilt sensing means for measuring the dynamic tilt of the apparatus for correction of the estimate of the difference in gravity between the KRP and first nominal center and the estimate of the difference in gravity between the first and second nominal centers.

9. An apparatus as in claim 2 wherein the means for measuring specific force at the second nominal center includes three virtually orthogonal accelerometers.

10. An apparatus as in claim 9 wherein the means for calculating gravitational acceleration at the kinematic reference point includes a Global Positioning System (GPS) antenna and processor for calculating kinematic acceleration at the KRP.

11. An apparatus as in claim 10 wherein the means for calculating gravitational acceleration at the KRP includes:

a. means for estimating the difference in gravity between the KRP and first nominal center;

b. means for estimating the difference in gravity between the first and second nominal centers;

c. means for determining a corrected force at the first nominal center from the specific force at the first nominal center and the gravity difference between the KRP and the first nominal center;

d. means for determining a corrected force at the second nominal center from the specific force at the second nominal center and the gravity difference between the first and second nominal centers;

e. means for determining an interpolated specific force at the KRP from the corrected force at the first nominal center, the corrected force at the second nominal center and the distance between the KRP and first nominal center and the distance between the first and second nominal centers;

f. means for determining the gravitational acceleration at the KRP from the interpolated specific force and the kinematic acceleration at the KRP.

12. An apparatus as in claim 11 wherein the means for estimating the difference in gravity between the KRP and first nominal center and the means for estimating the difference in gravity between the first and second nominal centers includes a database of gravity values and program means for retrieving a gravity value for a given coordinate.

13. An apparatus as in claim 12 wherein the means for estimating the difference in gravity between the KRP and first nominal center and the means for estimating the difference in gravity between the first and second nominal centers includes dynamic tilt sensing means for measuring the dynamic tilt of the apparatus and for correction of the estimate of the difference in gravity between the KRP and first nominal center and the estimate of the difference in gravity between the first and second nominal centers.

14. An apparatus as in claim 13 wherein the first and second accelerometer triads and the kinematic acceleration measurement means are mounted in a sensor mounting block.

15. An apparatus for measuring the magnitude of gravity comprising:

a. a sensor block;

b. a global positioning system within the sensor block for measuring kinematic acceleration at a kinematic reference point (KRP);

c. a first virtually orthogonal acclerometer triad within the sensor block for measuring specific force at a first nominal center wherein the first nominal center is a fixed and known distance from the KRP;

d. a second virtually orthogonal acclerometer triad within the sensor block for measuring specific force at a second nominal center wherein the second nominal center is a fixed and known distance from the KRP and is collinear with respect to the first nominal center and the KRP and corresponding accelerometers of the first and second triad are virtually parallel;

e. means for estimating the difference in gravity between the KRP and first nominal center;

f. means for estimating a difference in gravity between the first and second nominal centers;

g. means for determining a corrected force at the first nominal center from the specific force at the first nominal center and the gravity difference between the KRP and the first nominal center;

h. means for determining a corrected force at the second nominal center from the specific force at the second nominal center and the gravity difference between the first and second nominal centers;

i. means for determining an interpolated specific force at the KRP from the corrected force at the first nominal center, the corrected force at the second nominal center and the distance between the KRP and first nominal center and the distance between the first and second nominal centers;

j. means for determining the gravitational acceleration at the KRP from the interpolated specific force and the kinematic acceleration at the KRP.

16. A method of measuring the magnitude of gravity in an apparatus having a first nominal center, second nominal center and kinematic reference point wherein the first nominal center and second nominal center are collinear with and at a fixed and known distance from the kinematic reference point, the method comprising the steps of:

a. measuring specific force at the first nominal center;

b. measuring specific force at the second nominal center;

c. measuring kinematic acceleration at a kinematic reference point;

d. calculating the gravitational acceleration at the kinematic reference point from the specific force at the first nominal center and the second nominal center, the kinematic acceleration and the distance between the kinematic reference point and the first nominal center and the distance between the first nominal center and the second nominal center.

17. A method as in claim 16 wherein steps c) and d) include correlating the estimate of the difference in gravity between the KRP and first nominal center and the estimate of the difference in gravity between the first and second nominal centers to the dynamic tilt of the apparatus.

18. A method of measuring gravity comprising the steps of:

a. measuring kinematic acceleration at a kinematic reference point (KRP);

b. measuring specific force at a first nominal center;

c. measuring specific force at a second nominal center;

d. estimating the difference in gravity between the KRP and first nominal center from a gravity model;

e. estimating the difference in gravity between the first and second nominal centers from a gravity model;

f. calculating a corrected force at the first nominal center from the specific force at the nominal center and the gravity difference between the KRP and the first nominal center;

g. calculating a corrected force at the second nominal center from the specific force at the second nominal center and the gravity difference between the first and second nominal centers;

h. calculating an interpolated specific force at the KRP from the corrected force at the first nominal center, the corrected force at the second nominal center and the distance between the KRP and first nominal center and the distance between the first and second nominal centers;

i. calculating the gravitational acceleration at the KRP from the interpolated specific force and the kinematic acceleration at the KRP.