Assembly of linear accelerometers mounted on a rigid body remote from the center of mass measuring three dimensional movements

• US 5,408,879 A
• Filed: 02/10/1993
• Issued: 04/25/1995
• Est. Priority Date: 02/11/1992
• Status: Expired due to Fees

• Current Assignee: Fokker Space BV
• Original Assignee: Fokker Aircraft, B.V.
• Inventors: Vreeburg, Johannes P. B., Huijser, Ronald H.
• Primary Examiner(s): Chilcot, Jr., Richard E.
• Assistant Examiner(s): FELBER, JOSEPH LEON
• Application Number:
  US08/015,786
• Time in Patent Office: 804 Days
• Field of Search: 73/510, 73/517 A, 73/517 R, 73/514, 33/321
• US Class Current: 73/514.35
• CPC Class Codes: G01P 15/18 in two or more dimensions

Abstract

The invention provides an assembly of accelerometers for use in a system for measuring the three dimensional movements of a rigid body comprising nine linear accelerometers which are connected to said rigid body in a spacial configuration with reference to an imaginary orthogonal coordinate system. At a first position on the X-axis at a predetermined distance from the origin two accelerometers are installed, the sensitive directions thereof being parallel to the Y-axis and to the Z-axis respectively. At a second position on the Y-axis of the coordinate system at a predetermined distance from the origin two accelerometers are installed, the sensitive directions being parallel to the X-axis and to the Z-axis respectively. At a third position on the Z-axis at a predetermined distance from the origin two accelerometers are installed, the sensitive directions being parallel to the X-axis and to the Y-axis respectively. Three further accelerometers are installed midway on the edges between the first, second and third positions, the sensitive axes of these further accelerometers each coinciding with a line through the origin of the coordinate system.

Claims

1. An assembly of accelerometers for use in a system for measuring the three dimension movements of a rigid body comprising nine linear accelerometers which are connected to said rigid body in a spacial configuration with reference to an imaginary orthogonal coordinate system whereby at a first position on the X-axis of the coordinate system displaced from the origin a first and second accelerometer are installed, the sensitive direction of the first accelerometer being parallel to the Y-axis of the coordinate system and the sensitive direction of the second accelerometer being parallel to the Z-axis of the coordinate system, at a second position on the Y-axis of the coordinate system displaced from the origin a third and fourth accelerometer are installed, the sensitive direction of the third accelerometer being parallel to the X-axis and the sensitive direction of the fourth accelerometer being parallel to the Z-axis, and at a third position on the Z-axis of the coordinate system displaced from the origin a fifth and sixth accelerometer are installed, the sensitive direction of the fifth accelerometer being parallel to the X-axis and the sensitive direction of the sixth accelerometer being parallel to the Y-axis, wherein a seventh accelerometer is installed at a fourth position midway on a line between the first and second positions, the sensitive axis of the seventh accelerometer coinciding with a line through said fourth position and the origin of the coordinate system, an eighth accelerometer is installed at a fifth position midway on a line between the second and third position, the sensitive axis of the eighth accelerometer coinciding with a line through said fifth position and the origin of the coordinate system and a ninth accelerometer is installed at a sixth position midway on a line between the third and first position, the sensitive axis of the ninth accelerometer coinciding with a line through said sixth position and the origin of the coordinate system.

2. An assembly of accelerometers according to claim 1, wherein the first, second and third positions are displaced equal distances from the origin.

3. An assembly of accelerometers according to claim 2 in combination with a supporting triangular frame having three sides meeting at three vertexes, wherein the nine accelerometers are installed on the triangular frame with two accelerometers at each of its vertexes and one accelerometer midway on each of its sides.

4. An assembly of accelerometers according to claim 1 in combination with a supporting triangular frame having three sides meeting at three vertexes, wherein the nine accelerometers are installed on the triangular frame with two accelerometers at each of its vertexes and one accelerometer midway on each of its sides.

5. An assembly of accelerometers according to claim 4, wherein the triangular frame consists of three elongated subassemblies the length of each subassembly corresponds to the length of a side of the frame, each subassembly comprising two accelerometers at an end and one accelerometer midway between both ends.

6. A system for measuring the three dimensional movements of a rigid body comprising an assembly of accelerometers according to claim 5 and electronic circuitry to amplify and shape the accelerometer signals to obtain signals which are suitable for transmission to a processor at least partially installed within the triangular frame.

7. A system for measuring the three dimensional movements of a rigid body comprising an assembly of accelerometers according to claim 4, and electronic circuitry to amplify and shape the accelerometer signals to obtain signals which are suitable for transmission to a processor at least partially installed within the triangular frame.

8. An assembly of accelerometers for determining rotational and translational movements of a rigid body in three dimensions with reference to an imaginary orthogonal coordinate system having an origin at a center of inertia of said rigid body, said assembly comprising:

a) multiple opposed X-axis accelerometers having directions of sensitivity lying in a mutual X-axis accelerometer plane and passing through an X-axis point displaced along said X-axis to be in a physically more accessible location than is said origin;

b) multiple opposed Y-axis accelerometers having directions of sensitivity lying in a mutual Y-axis accelerometer plane perpendicular to said X-axis accelerometer plane and passing through a Y-axis point displaced along said Y-axis to be in a physically more accessible location than is said origin;

c) multiple opposed Z-axis accelerometers having directions of sensitivity lying in a mutual Z-axis accelerometer plane perpendicular to said X-axis and Y-axis accelerometer planes and passing through a Z-axis point displaced along said Z-axis to be in a physically more accessible location than is said origin;

d) multiple origin-oriented accelerometers each having a direction of sensitivity passing through said origin;

wherein one of each direction of sensitivity of said origin-oriented accelerometers passes through an intermediate point between said X-axis point and said Y-axis point, between said Y-axis point and said Z-axis point and between said Z-axis point and said X-axis point.

9. An assembly of accelerometers according to claim 8, wherein said intermediate points are midway between the respective axis points.

10. An assembly of accelerometers according to claim 9 comprising a pair of X-axis accelerometers, a pair of Y-axis accelerometers and a pair of Z-axis accelerometer, in combination with a support frame, the accelerometers of each said pair being disposed on said support frame with their axes of sensitivity aligned to define said origin at a point externally of said frame and said origin-oriented accelerometers being mounted on said support frame between said pairs of accelerometers.