Compact inertial measurement unit

• US 20020011106A1
• Filed: 03/09/2001
• Published: 01/31/2002
• Est. Priority Date: 07/28/2000
• Status: Active Grant

• Current Assignee: Israel Aerospace Industries Limited (Government of Israel)
• Original Assignee: Israel Aerospace Industries Limited (Government of Israel)
• Inventors: Hevroni, Benjamin, Barkai, Joseph
• Granted Patent: US 6,412,346 B2
• Time in Patent Office: Days
• US Class Current: 73/493
• CPC Class Codes: G01C 21/166 Mechanical, construction or arrangement details of inertial navigation systems

Abstract

An inertial measurement unit mountable on a vehicle, comprising a housing accommodating three solid state sensor couples, each couple comprising a gyro member and an associated accelerometer. The housing is in the shape of a triangular pyramid, with a base fitted with true position and fixation arrangements for positioning and fixing the housing at a predetermined relation with respect to an axis of the vehicle. Each of the solid state sensor couples is fitted on a respective face of the housing.

Claims

1. An inertial measurement unit mountable on a moving vehicle, said system comprising a housing accommodating three solid state sensor couples, each couple comprising a gyro member and an associated accelerometer;

said housing being in the shape of a triangular pyramid, with a base thereof fitted with true position and fixation means for positioning and fixing the housing at a predetermined relation with respect to an axis of the vehicle; and

where each of said solid state sensor couple is fitted on a respective face of the housing.

2. An inertial measurement unit according to claim 1, wherein the solid state sensor couples are mounted on receptive faces of the housing for measuring acceleration and rotation in three respective main axes orthogonal to one another, and wherein the axes coincide.

3. An inertial measurement unit according to claim 1, wherein the housing is in the shape of a truncated triangular pyramid.

4. An inertial measurement unit according to claim 1, wherein the solid state sensor couples are directly mounted on the housing.

5. An inertial measurement unit according to claim 1, wherein the gyros of the solid state sensor couples are fiber optic gyros (FOB) or ring laser gyros (RLG).

9. An inertial measurement unit according to claim 1, wherein each of the gyros is received within a cylindrical cover at a respective face of the housing, said platform being formed with suitable openings for passage of a wiring from each gyro into a confined space of the platform.

10. An inertial measurement unit according to claim 9, wherein the openings are formed at walls of the cylindrical housings.

11. An inertial measurement unit according to claim 9, wherein the cylindrical housings are covered with a cylindrical cover normally extending from a face of the platform.

12. An inertial measurement unit according to claim 1, wherein the fixation means is two or more apertures formed at the base of the housing, for securing to the moving vehicle by suitable fasteners.

13. An inertial measurement unit according to claim 12, wherein the apertures are formed at respective edges of faces of the housing.

14. An inertial measurement unit according to claim 1, wherein one or more of the edges of the pyramid is truncated at a bottom portion thereof, adjacent the base of the housing.

15. An inertial measurement unit according to claim 1, wherein the gyros are integrally received within their cylindrical covers.

16. An inertial measurement unit according to claim 1, wherein the housing further accommodates a circuitry printed board extending adjacent a base of the housing and being electrically connected to the solid state sensor couples by a suitable harness;

said circuitry printed board comprising an externally accessible socket.

17. An inertial measurement unit according to claim 1, wherein the moving vehicle is an airborne vehicle.

6. A housing for an inertial measurement unit, the housing being in the shape of a truncated triangular pyramid, and where each face thereof is fitted with a solid state sensor couple, each couple comprising a gyro member and an associated accelerometer.

7. A housing according to claim 6, wherein the solid state sensor couples are mounted on the housing with an essentially orthogonal relation between them, with the axes of the couples coinciding.

8. A housing according to claim 6, wherein a base of the pyramid is fitted with true position fixation means for positioning and fixing the housing at a predetermined calculable orientation with respect to an axis of a moving vehicle.