Miniature inertial measurement unit

• US 4,841,773 A
• Filed: 05/01/1987
• Issued: 06/27/1989
• Est. Priority Date: 05/01/1987
• Status: Expired due to Term

• Current Assignee: Litton Systems Incorporated
• Original Assignee: Litton Systems Incorporated
• Inventors: Stewart, Robert E.
• Primary Examiner(s): CHAPMAN JR, JOHN E
• Application Number:
  US07/045,045
• Time in Patent Office: 788 Days
• Field of Search: 73/504, 73/505, 73/510, 73/517 R
• US Class Current: 73/510
• CPC Class Codes: G01C 19/00 Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
• CPC Class Codes: G01C 19/28 Pick-offs, i.e. devices for taking-off an indication of the displacement of the rotor axis

Abstract

A three axis inertial measurement unit (IMU) is shown with three pairs of accelerometers mounted upon a platform that is rotated about a single axis perpendicular to the plane of the platform. Each pair of accelerometers is mounted in parallel, at an angle to the platform and to the single axis and at the same distance from the axis. The rotational motion may be either an oscillation about a dither axis or spinning about a spin axis.

Claims

1. A three axis inertial measurement unit, comprising:

a platform mounted for rotary motion about a single axis with respect to an object whose motion is being measured;

a plurality of sensors mounted upon said platform, said sensors each having an input axis, an output axis, and a pendulous axis; and

said sensors mounted upon said platform such that said input axis of each sensor is at a predetermined angle to said single axis and said platform.

2. An inertial measurement unit, as claimed in claim 1, wherein:

said plurality of sensors are accelerometers.

3. An inertial measurement unit, as claimed in claim 2, wherein:

said accelerometers are solid state devices.

4. An inertial measurement unit, as claimed in claim 3, wherein:

said pendulous axes of said accelerometers are each arranged to lie within a plane which includes said single axis.

5. An inertial measurement unit, as claimed in claim 1, wherein:

said plurality of sensors includes three accelerometers for providing an inertial measurement in a vibration free environment.

6. An inertial measurement unit, as claimed in claim 1, wherein:

said plurality of sensors includes six accelerometers for providing an inertial measurement mounted upon said platform about said single axis; and

pairs of six accelerometers are mounted opposite one another upon said platform to provide common mode rejection to reduce errors induced by vibration of said object whose motion is being measured.

7. An inertial measurement unit, as claimed in claim 6, wherein:

said six accelerometers are mounted at an equal radius from said single axis and 60°

apart upon said platform.

8. An inertial measurement unit, as claimed in claim 2, wherein:

said rotary motion is an oscillating motion, and

said single axis is a dither axis.

9. An inertial measurement unit as claimed in claim 2, wherein:

said rotary motion is a spinning motion; and

said single axis is a spin axis.

10. An inertial measurement unit, as claimed in claim 8, wherein:

said platform is oscillated about said single dither axis by a sinusoidal velocity excitation.

11. An inertial measurement unit, as claimed in claim 6, additionally comprising:

circuit means connected to said accelerometers to generate signals representing the linear acceleration and angular velocity thereof;

summing circuit means for receiving said linear acceleration and angular velocity signals from said pairs of accelerometers arranged opposite one another for cancelling the angular velocity signals while retaining the linear acceleration signals; and

differencing circuit means for receiving said linear acceleration and angular velocity signals from said two accelerometers arranged opposite one another for cancelling the linear acceleration signals while retaining the angular velocity signals.

12. An inertial measurement unit, as claimed in claim 1, wherein:

said input axes of said plurality of sensors are each mounted at an angle to said platform to lie within a plane that includes said single axis.

13. A three axis inertial measurement unit, comprising:

a platform mounted for rotary motion about a single axis;

a plurality of accelerometers arranged in pairs mounted with respect to an object whose motion is being measured

said accelerometers mounted upon said platform such that said input axis of each accelerometer is at an angle to said single axis and said platform; and

said pairs of accelerometers are mounted opposite one another on said platform having said input, output and pendulous axes parallel to each other.

14. An inertial measurement unit, as claimed in claim 13, wherein:

said output axes of said plurality of sensors are arranged in a common plane perpendicular to said single axis.

15. An inertial measurement unit, as claimed in claim 13, wherein:

said pendulous axes of said plurality of sensors are each mounted at an angle to said platform to lie within a plane that includes said single axis.

16. An inertial measurement unit, as claimed in claim 15, wherein:

said angle of said pendulous axes to said platform is an angle greater than 0° and

less than 90°

.

17. An inertial measurement unit, as claimed in claim 15, wherein:

said angle of said pendulous axes to said platform is nominally 35.26°

.

18. An inertial measurement unit, as claimed in claim 13, wherein:

said input axes of said plurality of sensors are each mounted at an angle to said platform to lie within a plane that includes said single axis.

19. An inertial measurement unit, as claimed in claim 18, wherein:

said angle of said input axes to said platform is an angle greater than 0° and

less than 90°

.

20. An inertial measurement unit, as claimed in claim 18, wherein:

said angle of said input axes to said platform is nominally the complement of 35.26°

.

23. An inertial measurement unit, as claimed in claim 16, additionally comprising:

piezoelectric driving means mounted upon said plurality of vanes to drive said platform into said oscillation about said dither axis.

21. A three axis inertial measurement unit, comprising:

a platform mounted for an oscillating motion about a single dither axis;

a plurality of accelerometers mounted upon said platform, said accelerometers each having an input axis, an output axis, and a pendulous axis;

said accelerometers mounted upon said platform such that said input axis of each accelerometer is at an angle to said single dither axis and said platform; and

said platform mounted about said dither axis by a plurality of vanes radiating from said dither axis toward said platform.

22. An inertial measurement unit, as claimed in claim 21, additionally comprising:

a hub mounted about said dither axis;

said platform formed in the shape of a ring about said hub; and

said vanes joining said hub and said platform along a plurality of radials from said dither axis.