Linear precision actuator with accelerometer feedback

• US 4,922,159 A
• Filed: 05/09/1988
• Issued: 05/01/1990
• Est. Priority Date: 05/09/1988
• Status: Expired due to Term

• Current Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Inventors: Kessler, Keith E., Shipley, John W., Hyland, Dave, Phillips, Douglas J.
• Primary Examiner(s): Salce, Patrick R.
• Assistant Examiner(s): Rebsch, D. L.
• Application Number:
  US07/191,368
• Time in Patent Office: 722 Days
• Field of Search: 73/517 AV, 73/517 B, 244/158 R, 244/164, 244/170, 310/13, 310/15, 310/51, 318/128, 318/135, 381/71
• US Class Current: 318/128
• CPC Class Codes: B64G 1/22 Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
• CPC Class Codes: F16F 15/02 Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems F16F15/005 takes precedence ; layered products B32B; suppression of vibration in ships B63; relieving load on bearings, using magnetic means F16C39/06
• CPC Class Codes: F16F 7/1011 by electromagnetic means

Abstract

A high precision linear actuator for compensating short stroke, high frequency vibrations in a space deployed structure comprises a set of cylindrical magnetic pole pieces affixed to respective ones of a pair of graphite flexures, that are mounted to a thermally conductive cylindrical housing, which is to be affixed to the space deployed structure. Reaction against the "proof mass" pole pieces is achieved by a magnetic field produced by set of stationary magnetic coils that surround the pole pieces and are energized by a vibration compensation reaction current supplied from a sense/control processor. Coaxial with and mounted integrally with the cylindrical pole pieces of the proof mass is an internal accelerater, which generates an output signal representative of the force to which the proof mass is subjected. This output signal is monitored by the sense/control processor to close a force feedback loop and effectively reduce both the inherent resonance imparted by the spiral support flexures and non-linearities in the magnetic field, against which the "proof mass" cylindrical pole pieces react in the course of operation of the actuator. The vibration compensation drive signal that is supplied by the sense/control processor may be based upon the output of a second accelerometer that is mounted integrally with the cylindrical housing, but external to the flexures, by way of which the "proof mass" pole pieces, associated drive coils and internal accelerometer are supported.

Claims

1. An actuator comprising:

a housing, adapted to be to be attached to a structure, vibration of which is to be compensated;

a displaceable proof mass supported within said housing by elastically deformable means for constraining the displacement of said proof mass;

means, coupled to said housing, for causing an acceleration of said proof mass against which said housing and any structure attached thereto react;

force measurement means, integrally coupled with said proof mass, for measuring characteristics of the force produced in the course of the acceleration of said proof mass, and generating an output signal representative thereof; and

means, responsive to said output signal, for controlling the manner in which said acceleration causing means causes the acceleration of said proof mass.

2. An actuator according to claim 1, wherein said controlling means includes a force feedback loop coupled to said force measurement means through which the operation of said acceleration causing means is controlled in accordance with prescribed characteristics of said output signal.

3. An actuator according to claim 2, wherein said controlling means includes means for controlling the operation of said acceleration causing means so as to reduce the magnitude of prescribed characteristics of said output signal.

4. An actuator according to claim 3, wherein said displaceable proof mass comprises a magnetic field responsive element and said acceleration causing means comprises means for generating a controlled magnetic field in response to which said magnetic field responsive element is accelerated.

5. An actuator according to claim 4, wherein said housing has a generally cylindrical configuration and said magnetic field responsive element comprises a first pair of generally cup-shaped pole pieces and a second pair of generally cup-shaped pole pieces coaxial with and having a diameter different than said first pair of pole pieces so as to form a generally cylindrical space therebetween, and wherein said magnetic field generating means comprises a pair of electrical coils supported within said generally cylindrical space.

6. An actuator according to claim 5, wherein said elastically deformable means comprises a pair of flexures, affixed to longitudinally spaced apart portions of said housing, to which said first and second pairs of cup-shaped poles pieces are connected so as to be supported thereby in an axially translatable configuration.

7. An actuator according to claim 6, wherein said magnetic field generating means comprises a generally cylindrical support member affixed to said housing within said generally cylindrical space and around which said pair of electrical coils are wound.

8. An actuator according to claim 7, wherein each of said flexures comprises a multi-curve legged graphite flexure.

9. An actuator according to claim 1, wherein said force measurement means comprises a first accelerometer integrally coupled with said proof mass, and further including a second accelerometer coupled with said housing for measuring vibrations in a structure to which said housing is attached and producing a vibration representative output signal.

10. An actuator according to claim 9, further including means for controlling the operation of said acceleration causing means in accordance with the vibration representative signal.