Three axis inertial measurement unit with counterbalanced, low inertia mechanical oscillator

• US 5,065,627 A
• Filed: 10/11/1990
• Issued: 11/19/1991
• Est. Priority Date: 03/20/1990
• Status: Expired due to Fees

• 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:
  US07/595,531
• Time in Patent Office: 404 Days
• Field of Search: 73/505, 73/510, 73/517 R
• US Class Current: 73/504.04
• CPC Class Codes: G01C 19/5705 using masses driven in reciprocating rotary motion about an axis
• CPC Class Codes: G01C 19/5783 Mountings or housings not specific to any of the devices covered by groups G01C19/5607 - G01C19/5719

Abstract

A three axis inertial measurement unit is shown having a low inertia mechanical oscillator formed from two platforms counterbalanced against each other. Each platform is dithered at its natural frequency about a single torsional axis. A plurality of accelerators are mounted upon at least one of the counterbalanced platforms with each accelerometer having at least an input axis mounted at a predetermined angle to the torsional axis and to the platform. Each platform has a three legged, Y-shaped mounting member with a rotor member positioned between the legs of the mounting member. Web members which form the legs of the mounting member join the rotor member to the Y-shaped mounting member. Additionally, driving webs are mounted on each side of the web members for further joining the mounting member to the rotary member.

Claims

1. A three axis inertial measurement unit, comprising:

two platforms counterbalanced against each other mounted as a mechanical oscillator for dithered rotation at a natural frequency of said platforms about a single torsional axis;

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 platforms each having;

a three legged, Y-shaped mounting member;

a rotor member positioned between the legs of said mounting member;

web members forming said legs of said Y-shaped mounting member to join said rotor member; and

driving webs mounted on each side of said web members for further joining said 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.

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

said plurality of accelerometers include six accelerometers with three accelerometers mounted 120°

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

3. The inertial measurement unit of claim 1, wherein:

the cross-sectional dimensions of said web members may be changed to adjust the torsional stiffness of said rotor member, and

the cross-sectional dimensions of said driving webs may be changed to adjust the torque required for said dithered rotation of said rotor member independent of said adjustment of said web members.

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

piezoelectric drivers mounted upon said driving webs to drive said two counterbalanced platforms 180°

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

5. The inertial measurement unit of claim 1, wherein:

said plurality of accelerometers each include said input axis and an output axis and a pendulous axis.