System and method for gravimetry without use of an inertial reference

Patent metadata

Field	Value
Publication number	US-10330820-B2
Application number	US-201414454468-A
Country	US
Kind code	B2
Filing date	Aug 7, 2014
Priority date	Aug 7, 2014
Publication date	Jun 25, 2019
Grant date	Jun 25, 2019

Abstract

A gravimeter for measuring the gravitational field of the Earth without an inertial reference comprises accelerometer pairs disposed on a platform where the sensitive axis of each accelerometer is arranged on the platform to measure plumb gravity. At least one accelerometer pair is spatially configured to define a baseline therebetween. The gravimeter is positioned so that the baseline is maintained parallel to a linear survey path. Each accelerometer outputs a signal representative of the sum total of the accelerations detected, including accelerations due to gravity and kinematic accelerations of the host vehicle and mounting structure. A processor subtracts the accelerometer pair outputs for common-mode rejection determination of a down gravity gradient and combines with a direct plumb gravity measurement to obtain an enhanced gravity data output that is not subject to frequency limits attributed to the performance limitations of inertial reference devices.

First claim

What is claimed is:

1. A system for measuring the gravitational field of the Earth without an inertial reference device comprising:
a pair of accelerometers disposed on a platform, said pair of accelerometers arranged to measure plumb gravity along a sensitive axis aligned with gravity, the pair of accelerometers comprising a first accelerometer and a second accelerometer spatially separated from each other to define a first baseline having a first baseline distance, the first baseline being configured to be maintained parallel to a linear survey path;
a computer processor in communication with each accelerometer, the computer processor including differencing circuitry, the computer processor being configured to, at each of a plurality of locations along the linear survey path as the platform continuously moves in a direction parallel to the linear survey path:
receive a first output signal from the first accelerometer of the pair;
receive a second output signal from the second accelerometer of the pair, wherein said first output signal said second output signal are representative of a sum total of all accelerations sensed by the associated first accelerometer and second accelerometer, respectively, including plumb gravity and other non-gravity components of acceleration;
determine, by the differencing circuitry, a difference of said first output signal and said second output signal and integrate over the first baseline distance to calculate a forward-down gravity gradient;
remove identifiable non-gravity components from the first output signal to generate a first compensated output signal;
remove identifiable non-gravity components from the second output signal to generate a second compensated output signal;
average said first compensated output signal and said second compensated output signal to generate a first direct plumb gravity measurement;
generate a first enhanced plumb gravity data measurement based on said first direct plumb gravity measurement and said forward-down gravity gradient; and
generate a model of a gravitational field that identifies the first enhanced plumb gravity data measurement at locations along the linear survey path; and

wherein the system lacks an inertial reference device.

2. The system of claim 1 , wherein said computer processor is further configured to:
apply a first weighting factor to said first direct plumb gravity measurement and a second weighting factor to said forward-down gravity gradient.

3. The system of claim 2 , wherein said first and second weighting factors are determined based on a frequency of said non-gravity components of acceleration.

4. The system of claim 3 , wherein said first weighting factor has greater influence than said second weighting factor when the frequency of said non-gravity components is less than about 0.01 Hz; and wherein said second weighting factor has more influence than said first weighting factor when the frequency of said non-gravity components is greater than about 0.01 Hz.

5. The system of claim 1 , further comprising a mounting assembly for coupling said platform to a host vehicle, said mounting device comprising:
a base configured to be rigidly attached to the host vehicle;
a rotational bearing configured to be coupled to and support said platform, wherein said rotational bearing comprises:
a linear stage coupled to said base; and
a rotational stage coupled to said platform.

6. The system of claim 5 , wherein said linear stage comprises:
a spherical cup; and
a source of fluid under pressure;
wherein said source of fluid under pressure is in fluid communication with at least one aperture defined in a concave surface of said spherical cup.

7. The system of claim 6 , wherein said rotational stage comprises:
a spherical bearing member configured to engage with said spherical cup, said spherical bearing member configured to rest on and be supported by a cushion of fluid under pressure between said spherical cup and said spherical bearing member, said spherical bearing member being supported by said linear stage in a non-contacting manner.

8. The system of claim 5 , further comprising:
a passive isolating suspension disposed between said base and said linear stage.

9. The system of claim 8 , wherein said passive isolating suspension comprises an air spring coupled to an auxiliary air chamber via a conduit having an adjustable orifice.

10. The system of claim 8 , wherein said passive isolating suspension comprises a helical spring.

11. The system of claim 5 , wherein said host vehicle is configured as an autonomous underwater vehicle (AUV).

12. The system of claim 5 , wherein said host vehicle is configured as an airborne platform.

13. The system of claim 12 , wherein said airborne platform is a fixed wing aircraft.

14. The system of claim 1 , further comprising:
a second pair of accelerometers comprising a third accelerometer and a fourth accelerometer spatially separated to define a second baseline having a second baseline distance, the second baseline being substantially orthogonal to said first baseline between the accelerometers of said pair of accelerometers.

15. The system of claim 14 , wherein said processor is further configured to:
receive a third output signal from said third accelerometer;
receive a fourth output signal from said fourth accelerometer, wherein said third output signal and said fourth output signal are representative of a sum total of all accelerations sensed by the associated third accelerometer and fourth accelerometer, respectively, including plumb gravity and other non-gravity components of acceleration;
determine a difference of said third output signal and said fourth output signal and integrate over the second baseline distance to calculate a horizontal cross track-down gravity gradient;
remove identifiable non-gravity components from the third output signal to generate a third compensated output signal;
remove identifiable non-gravity components from the fourth output signal to generate a fourth compensated output signal;
third compensated output signal and said fourth compensated output signal to generate a second direct plumb gravity measurement;
generate a second enhanced plumb gravity measurement based on said second direct plumb gravity measurement and said horizontal cross track down-gravity gradient to calculate a final data gravity measurement.

16. In a gravimeter having a platform on which is disposed at least a pair of accelerometers spatially separated from each other to define a first baseline having a first baseline distance, a method for measuring the force due to gravity without using an inertial reference device comprising:
receiving, by a computer processor, at each of a plurality of locations along a linear survey path as the platform continuously moves in a direction parallel to the linear survey path, a first output signal from a first accelerometer of the pair of accelerometers and a second output signal from a second accelerometer of said pair of accelerometers that are representative of a sum total of all accelerations sensed by the associated first accelerometer and second accelerometer while being maintained parallel to the linear survey path, respectively, including plumb gravity and other non-gravity components of acceleration, the pair of accelerometers measuring plumb gravity along a sensitive axis aligned with gravity;
determining, by the computer processor, a difference of said first output signal and said second output signal and integrating over the first baseline distance to calculate a forward-down gravity gradient

Assignees

• Lockheed Corp

Inventors

• Meyer Thomas J

Classifications

• G01V7/16

  specially adapted for use on moving platforms, e.g. ship, aircraft · CPC title

• G01V7/02 Primary

  Details · CPC title