Apparatus and method for leveling a gravity measurement device

• US 4,935,883 A
• Filed: 05/17/1988
• Issued: 06/19/1990
• Est. Priority Date: 05/17/1988
• Status: Expired due to Fees

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Sundstrand Data Control, Inc.
• Inventors: Hulsing, Rand H. II
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): Cosimano, Edward R.
• Application Number:
  US07/194,888
• Time in Patent Office: 763 Days
• Field of Search: 33/302, 73/382 R, 73/382 G, 175/45, 364/422, 364/434, 364/559, 364/571.01
• US Class Current: 700/302
• CPC Class Codes: G01V 7/00 Measuring gravitational fields or waves; Gravimetric prospecting or detecting

Abstract

Apparatus and method for establishing a level plane and with respect to the level plane, vertically aligning an acceleration sensitive axis of a gravity measurement device (10). The gravity measurement device includes an accelerometer (68), which is rotatably mounted on a gimbal shaft (62) within a gimbal frame (54). The gimbal frame is also rotatable about a longitudinal axis that is preferably oriented at a right angle to the longitudinal axis of the gimbal shaft. A stepping motor (20) is connected through an antibacklash gear (30), an idler gear (32) and an antibacklash gear (48) to a drive shaft (50). Rotation of this drive shaft causes the accelerometer to rotate about the gimbal shaft. In a similar fashion, a stepping motor (22) is drivingly connected to a drive shaft (56), used to rotate the gimbal frame. A control (140) selectively energizes the stepping motors, so that the acceleration sensitive axis of the accelerometer is rotated until an output signal from the acceleometer indicates that the acceleration of gravity is zero and thus that the sensitive axis is level at two cross axis positions, thereby determining a level reference plane. The control then causes the accelerometer to be rotated 90° relative to the reference plane, so that the acceleration sensitive axis is vertically aligned, thereby enabling the accelerometer to measure the local acceleration of gravity with minimal error due to vertical alignment.

Claims

1. In a device for measuring the acceleration of gravity using an accelerometer, an apparatus for vertically orienting an acceleration sensitive axis of the accelerometer, comprising:

(a) first means for rotating the accelerometer about a first axis that is orthogonal to the acceleration sensitive axis;

(b) second means for rotating the accelerometer about a second axis that is angularly displaced from the first axis;

(c) drive means, connected to the first and the second means, for selectively driving the first and the second means to orient the acceleration sensitive axis of the accelerometer in a plurality of substantially horizontal directions, defining a level plane; and

(d) processor means, responsive to a signal produced by the accelerometer indicative of the acceleration of gravity, for controlling the drive means as a function of said signle in order to establish the level plane, and further operative to vertically align the acceleration sensitive axis of the accelerometer relative to the level plane.

2. The apparatus of claim 1, wherein the drive means are spatially separated from the accelerometer to minimize heat transfer therebetween.

3. The apparatus of claim 1, wherein the first means comprise a shaft on which the accelerometer is rotatably mounted.

4. The apparatus of claim 3, wherein the second means comprise a rotatable frame in which the shaft is mounted, the first means being rotatable within the frame.

5. The apparatus of claim 4, wherein the drive means comprise a first and a second stepping motor and gear means for drivingly connecting the first and the second stepping motors to the frame and to the shaft.

6. The apparatus of claim 1, wherein the processor means is operative to energize the drive means, causing:

(a) the first and the second means to rotate the accelerometer to a first and a second position in which the signal produced by the accelerometer indicates that the acceleration of gravity acting along the acceleration sensitive axis is substantially zero, the acceleration sensitive axis thus being substantially horizontal in the first and the second positions; and

(b) the first and the second means to rotate the accelerometer to a third position in which the acceleration sensitive axis is substantially orthogonal to its horizontal disposition in both the first and the second positions of the accelerometer, the acceleration sensitive axis being substantially vertically aligned in said third position.

7. The apparatus of claim 6, wherein the processor means is further operative to energize the drive means, causing the accelerometer to rotate to a fourth position in which the acceleration sensitive axis is substantially vertically aligned in the opposite direction, relative to its disposition in the third position.

8. The apparatus of claim 6, wherein the angle subtended by the acceleration sensitive axis when the accelerometer is in the first and the second positions is substantially ninety degrees.

9. In a gravity measurement device, an apparatus for determining a level disposition that is orthogonal to a gravitational acceleration, comprising:

(a) a first gimbal, mounted on the gravity measurement device and rotatable about a first axis;

(b) a second gimbal, mounted on the first gimbal and rotatable about a second axis, which is disposed at a substantial angular displacement relative to the first axis and intersects it;

(c) means for sensing acceleration along an acceleration sensitive axis and producing a signal indicative of the acceleration, said means being mounted on the second gimbal so that the acceleration sensitive axis is disposed at a right angle relative to the second axis, being rotatable about both the first and second axes; and

(d) means for incrementally rotating the first and the second gimbals to orient the acceleration sensitive axis to a first position and then to a second position at which the signal produced by the acceleration sensing means indicates substantially a minimum acceleration due to gravity, said first and second positions defining a level plane for the first and the second gimbals, so that the acceleration sensitive axis may be oriented vertically relative to the level plane.

10. The apparatus of claim 9, wherein the means for incrementally rotating the first and the second gimbals comprise a first stepping motor, a second stepping motor, and control means connected to receive the signal produced by the acceleration sensing means, for controlling the first and the second stepping motors as a function of said signal.

11. The apparatus of claim 10, wherein the control means is operative to selectively energize the first and the second stepping motors, incrementally rotating the first and the second gimbals about their respective first and second axes, one rotational step of each stepping motor corresponding to a predetermined incremental angle.

12. The apparatus of claim 11, wherein the control means is operative to rotate the acceleration sensing means about the first and second axes, until the acceleration sensitive axis lies within the level plane in two different orientations and thus to determine the number of steps of the first and second stepping motors required in driving the first and the second gimbals, respectively, to vertically orient the acceleration sensitive axis, relative to said level plane.

13. The apparatus of claim 10, wherein the means for incrementally rotating the first and the second gimbals further comprise first gear means for drivingly connecting the first stepping motor to the first gimbal, and second gear means for drivingly connecting the second stepping motor to the second gimbal.

14. The apparatus of claim 13, wherein the first gear means comprise a first drive gear and at least one antibacklash gear, and the second gear means comprise a second drive gear, at least one antibacklash gear and two bevel gears.

15. The apparatus of claim 14, wherein the first axis defines a right angle with the second axis and wherein the first gimbal comprises an outer ring, connected to a first drive shaft that is aligned with the first axis, the antibacklash gear of the first gear means being mounted on the first drive shaft, and wherein the one of the bevel gears is attached to the second gimbal, concentric to the second axis, the other bevel gear being mounted on a second drive shaft that is aligned with the first axis, and drivingly engaging said one bevel gear, said second drive shaft being rotatably driven by the antibacklash gear of the second gear means, said first and second drive gears respectively drivingly connecting the first and second stepping motors to the antibacklash gears.

16. The apparatus of claim 15, wherein the first and second gear means each further comprise a rotatably mounted idler shaft on which are mounted another antibacklash gear and an idler gear, the first and second drive gears each engaging one of said other antibacklash gears and thus drivingly rotating the idler gear, said idler gear engaging the one antibacklash gear and transmitting rotational motion to it.

17. In a device for measuring the acceleration of gravity using an accelerometer having an acceleration sensitive axis, a method for vertically orienting the acceleration sensitive axis of the accelerometer, comprising the steps of:

(a) rotating the accelerometer about a first axis to a first position in which the acceleration sensitive axis is horizontally disposed;

(b) rotating the accelerometer about a second axis, orthogonal to the first, to a second position in which the acceleration sensitive axis is horizontally disposed; and

(c) rotating the accelerometer about the first and the second axes to a third position in which the acceleration sensitive axis is displaced by substantially ninety degrees relative to its disposition at the first and the second positions, said third position of the accelerometer orienting the acceleration sensitive axis vertically.

18. The method of claim 17, further comprising the step of rotating the accelerometer about one of the first and the second axes to a fourth position in which the acceleration sensitive axis is oriented vertically in the opposite direction from that in which it is disposed in the third position.

19. In a precision gravity measurement device having an accelerometer for sensing the acceleration of gravity along a sensitive axis and producing a signal indicative thereof, a method for determining a level disposition that is orthogonal to the acceleration of gravity, comprising the steps of:

(a) incrementally rotating the accelerometer about a first axis that is at right angles to the acceleration sensitive axis, to a position at which the signal the accelerometer produces indicates substantially a zero component of the acceleration of gravity along the sensitive axis, thereby defining a first level point associated with the first axis;

(b) rotating the accelerometer through an angle of ninety degrees about the first axis to a position where its sensitive axis is generally oriented vertically;

(c) incrementally rotating the accelerometer about a second axis that is angularly displaced relative to the first axis, to a position at which the signal the accelerometer produces indicates substantially a zero component of the acceleration of gravity along the sensitive axis, thereby defining a second level point associated with the second axis; and

(d) incrementally rotating the accelerometer about at least one of the first and the second axes, through an angle determined relative to the first and the second level points, respectively, so that the acceleration sensitive axis is substantially vertical, and so that the accelerometer accurately measures the acceleration of gravity with minimal vertical alignment errors.

20. The method of claim 19, further comprising the steps of first orienting the acceleration sensitive axis precisely vertical relative to the first and second level points, and then rotating the accelerometer through 180 degrees about one of the first and the second axes so that the acceleration of gravity is measured in an opposite vertical disposition of the acceleration sensitive axis.

21. The method of claim 19, wherein the accelerometer is mounted on orthogonally rotatable first and second gimbals having a first axis and a second axis of rotation coincident with the first and second axes, respectively.

22. The method of claim 21, wherein the accelerometer is mounted on one of the first and the second gimbals, and wherein the first and second gimbals are respectively rotated by a first and a second stepping motor, the relationship between the first and second level points and the vertical orientation of the acceleration sensitive axis corresponding to a predetermined number of steps of the stepping motors.