Three axis inertial measurement unit with counterbalanced mechanical oscillator

• US 4,996,877 A
• Filed: 04/30/1990
• Issued: 03/05/1991
• Est. Priority Date: 02/24/1989
• Status: Expired due to Term

• Current Assignee: Litton Systems Incorporated (Northrop Grumman Corporation)
• Original Assignee: Litton Systems Incorporated (Northrop Grumman Corporation)
• Inventors: Stewart, Robert E., Fersht, Samuel N.
• Primary Examiner(s): CHAPMAN JR, JOHN E
• Application Number:
  US07/518,075
• Time in Patent Office: 309 Days
• Field of Search: 73/505, 73/510, 73/517 R
• US Class Current: 73/510
• CPC Class Codes: G01C 19/5705 using masses driven in reciprocating rotary motion about an axis

Abstract

An inertial measurement unit capable of providing information relating to all six degrees of freedom in an orthogonal three axis system is shown having a mechanical oscillator constructed from two counterbalanced platforms which form a single unit for rotation about a single torsional axis. A plurality of accelerometers are mounted upon at least one of the counterbalanced platforms. Each accelerometer has an input axis, an output axis, and a pendulous axis. Each accelerometer is mounted such that the input axis is at a predetermined angle to the single axis of rotation and the counterbalanced platform. The accelerometers are used to measure angular rate along the pendulous axis and linear acceleration along the input axis. These signals may then be electronically separated to produce acceleration and angular rate outputs for a three axis orthogonal system.

Claims

1. A three axis inertial measurement unit, comprising:

two counterbalanced mechanisms each mounted for mechanical oscillation at a natural frequency about a single axis wherein one mechanism counterbalances the other;

said two counterbalanced mechanisms mounted by mounting means for imparting rotational motion thereto only in a respective plane of rotation perpendicular to said single axis;

a plurality of accelerometers mounted on at least one of said counterbalanced mechanisms;

each accelerometer having at least an input axis;

said plurality of accelerometers mounted upon said at least one counterbalanced mechanism such that said input axis of each acceleromoter is at a predetermined angle to said single axis and to said single plane of rotation of said counterbalanced mechanisms.

2. The inertial measurement unit of claim 1, additionally comprising:

said rotational motion of said counterbalanced mechanisms is a dithered rotational motion;

said single axis is a torsional axis; and

drive means for driving each of said counterbalanced mechanisms at a dithered oscillation that is 180°

out of phase.

3. The inertial measurement unit of claim 2, additionally comprising:

said plurality of accelerometers mounted upon said at least one counterbalanced mechanism include three accelerometers mounted upon said at least one mechanism for providing inertial measurements in a vibration-free environment.

4. The inertial measurement unit of claim 2, additionally comprising:

said plurality of accelerometers mounted upon at least one counterbalanced mechanism include six accelerometers with three accelerometers mounted upon each counterbalanced mechanism for providing inertial measurements in a vibrating environment.

5. The inertial measurement unit of claim 4, additionally comprising:

said three accelerometers mounted upon one of said two counterbalanced mechanisms form matched pairs with said three accelerometers mounted upon the second of said counterbalanced mechanisms, such that said input axis of each matched accelerometer pair is parallel to one another and at a predetermined angle to said single torsional axis.

6. The inertial measurement unit of claim 2, additionally comprising:

said accelerometers are silicon accelerometers; and

said drive means are piezoelectric strips mounted upon said mounting means for said counterbalanced mechanisms.

10. The inertial measurement unit of claim 1, additionally comprising:

said accelerometers each having an input axis, an output axis, and a pendulous axis.

7. A three axis inertial measurement unit, comprising:

two counterbalanced platforms each mounted for mechanical oscillation at a natural frequency about a single torsional axis wherein the first platform counterbalances the second;

a plurality of accelerometers mounted on at least one of said platforms;

each accelerometer having at least an input axis,

said plurality of accelerometers mounted upon said at least one platform such that said input axis of each accelerometer is at a predetermined angle to said single torsional axis and said platform;

said two counterbalanced platforms each having;

a Y-shaped mounting member;

a rotor member surrounding said Y-shaped mounting member; and

web members joining said Y-shaped mounting member to said rotor member;

said accelerometers mounted upon said at least one of said platforms mounted upon said rotor member thereof at said predetermined angle.

8. The inertial measurement unit of claim 7, additionally comprising:

said plurality of accelerometers include six accelerometers having three each mounted 120°

apart upon each rotor member and arranged in matched pairs with said input, output, and pendulous axes of each pair mounted in parallel to each other and at predetermined angles to said single torsional axis.

9. The inertial measurement unit of claim 7, additionally comprising:

piezoelectric drivers mounted upon said web means to drive said two counterbalanced platforms 180°

out of phase from each other during said dithered rotation thereof.

11. The inertial measurement unit of claim 7, additionally comprising:

said accelerometers each having an input axis, an output axis, and a pendulous axis.