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US4841773A Expired / Lapsed US ⏱️ 0.0 years remaining

Miniature inertial measurement unit

Assignee: Northrop Grumman Guidance and Electronics Co Inc
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Filing: 1987-05-01
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Granted: 1989-06-27
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Expires: 2007-05-01
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Abstract

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.

Inventors

  • 👤 Robert E. Stewart

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 20:50
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/02; G01C19/04; G01C19/28

Claims Analysis

Total Claims: 26
Claim 1
Independent Claim 76 words
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.
Claim 2
Dependent Claim 76 words
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.
Claim 3
Dependent Claim 16 words
An inertial measurement unit, as claimed in claim 1, wherein: said plurality of sensors are accelerometers.
Claim 4
Dependent Claim 16 words
An inertial measurement unit, as claimed in claim 2, wherein: said accelerometers are solid state devices.
Claim 5
Dependent Claim 29 words
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.
Claim 6
Dependent Claim 27 words
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.
Claim 7
Dependent Claim 62 words
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.
Claim 8
Dependent Claim 29 words
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.
Claim 9
Dependent Claim 25 words
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.
Claim 10
Dependent Claim 25 words
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.
Claim 11
Dependent Claim 24 words
An inertial measurement unit, as claimed in claim 8, wherein: said platform is oscillated about said single dither axis by a sinusoidal velocity excitation.
Claim 12
Dependent Claim 94 words
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.
Claim 13
Dependent Claim 37 words
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.
Claim 14
Dependent Claim 84 words
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.
Claim 15
Dependent Claim 84 words
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.
Claim 16
Dependent Claim 29 words
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.
Claim 17
Dependent Claim 37 words
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.
Claim 18
Dependent Claim 29 words
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°.
Claim 19
Dependent Claim 22 words
An inertial measurement unit, as claimed in claim 15, wherein: said angle of said pendulous axes to said platform is nominally 35.26°.
Claim 20
Dependent Claim 37 words
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.
Claim 21
Dependent Claim 29 words
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°.
Claim 22
Dependent Claim 25 words
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°.
Claim 23
Dependent Claim 88 words
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.
Claim 24
Dependent Claim 88 words
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.
Claim 25
Dependent Claim 48 words
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.
Claim 26
Dependent Claim 31 words
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.

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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1992-06-26 1992-12-26 1993-06-27 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1996-06-26 1996-12-26 1997-06-27 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2000-06-26 2000-12-26 2001-06-27 $7700.00 Window Closed / Lapsed

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