Linear dc motor vibration controller

• US 4,897,582 A
• Filed: 01/06/1987
• Issued: 01/30/1990
• Est. Priority Date: 01/06/1987
• Status: Expired due to Term

• Current Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Inventors: Johnson, Russell A., Shipley, John W., Anderson, Jeffery R., Otten, Thomas H., Miller, Warren H., Burton, Willie T. Jr.
• Primary Examiner(s): Salce, Patrick R.
• Assistant Examiner(s): REBSCH, DONALD
• Application Number:
  US07/000,773
• Time in Patent Office: 1,120 Days
• Field of Search: 244/164, 244/165, 244/170, 310/12, 310/13, 310/14, 310/15, 310/154, 318/114, 318/135, 318/489, 318/648, 318/649
• US Class Current: 318/135
• CPC Class Codes: B64G 1/36 using sensors, e.g. sun-sensors, horizon sensors
• CPC Class Codes: B64G 1/365 using horizon or Earth sensors
• CPC Class Codes: B64G 1/38 damping of oscillations, e.g. nutation dampers
• CPC Class Codes: H02K 41/031 of the permanent magnet type

Abstract

A linear force actuator system for stabilizing a support structure employs a linear dc motor whose primary winding is driven by a pulse width modulation control signal representative of a force input, through which the secondary member of the motor which acts as an inertial mass, is to be controllably translated. For improved control accuracy, the actuator system of the invention employs a pair of feedback loops, one of which monitors the current in the motor'"'"'s primary winding to maintain a constant force output to the secondary member and a secondary of which monitors long term deviations from the center of the secondary member and corrects for centering offsets. An opto-electronic position sensing arrangement monitors the movement of the secondary member whereby precise control of commutation of the coils of the primary winding and a smooth translation of the secondary member are obtained.

Claims

1. For use with a structure that is subject to vibrational movement, a system for imparting a controlled dampening force to said structure so as to counter said vibrational movement comprising:

a moveable mass to be translated in an oscillatory movement with respect to said structure and thereby impart to said structure a vibrational movement-compensating force against which said structure reacts, so that the vibrational movement thereof may be effectively countered by the controlled movement of said mass; and

first means, mechanically attached to said structure at a location whereat said vibrational movement may occur, for providing a rectilinear travel path for said mass to be translated there along in an oscillatory manner and for imparting a controlled force to said mass so as to cause said mass to oscillate along said rectilinear travel path; and

wherein

one of said movable mass and said first means comprises a winding of an electric motor and the other of said mass and said means comprises a linear magnetic field responsive element, magnetically interacting with said winding of said electric motor, so that said winding may impart a force to said element, and wherein

the oscillatory translation of said movable mass is controlled exclusively by controlled magnetic field interaction between said winding and said linear magnetic field responsive element.

2. A system according to claim 1, wherein said first means comprises a primary winding of a linear direct current motor magnetically coupled with said mass, for generating a magnetic field having a controlled characteristic, in response to which said mass is controllably rectilinearly oscillated with respect to said electric motor winding and said mass comprises a rectilinear secondary actuator element coupled with said primary winding and rectilinearly moved thereby along said rectilinear travel path in response to the generation of a controlled magnetic field by said primary winding.

3. A system according to claim 2, further including second means, coupled with said rectilinear secondary actuator element, for generating an output representative of the movement of said rectilinear secondary actuator element relative to a prescribed location on the travel path of said rectilinear secondary actuator element;

and

third means, coupled to said first and second means, for controlling the generation of said magnetic field by said primary winding and, consequently the rectilinear movement of said rectilinear secondary actuator element thereby, in response to a prescribed force input representative signal and in accordance with the output generated by said second means.

4. A system according to claim 1, further comprising second means for monitoring the displacement between said winding and said element on the travel path of the movable one thereof and measured the length of time that displacement therebetween is effectively positioned to one side of a predetermined location on said travel path and measuring the length of time that the displacement therebetween is effectively positioned to a second side of said predetermined location;

and

third means, coupled said winding and said second means, for adjusting the energization of said winding in accordance with a difference in the length of time measurement carried out by said second means over a prescribed time interval in excess of the period of the lowest frequency of oscillation imparted to said moveable mass.

5. A system according to claim 3, wherein said rectilinear secondary actuator element comprises an elongated low magnetic reluctance member having a plurality of magnetic pole pieces distributed along the periphery thereof in the direction of movement of said member and wherein said primary winding is arranged symmetrically with respect to the axis of travel of said member.

6. A system according to claim 5, wherein said primary winding has a core made of non-magnetic, non-conductive material.

7. A system according to claim 6, further including a low magnetic reluctance element disposed adjacent to the periphery of said primary winding for providing a low reluctance return path for the magnetic field generated by said primary winding and interacting with the pole pieces of said member.

8. A system according to claim 3, wherein said second means comprises a digitally encoded reflectance pattern disposed along said rectilinear secondary actuator element, and optical detector means, disposed at a prescribed location with respect to said primary winding, for detecting respective values of said digitally encoded reflectance pattern as said rectilinear secondary actuator element is rectilinearly moved by the controlled generation of said magnetic field by the primary winding of said motor.

9. A system according to claim 8, further including

fourth means, coupled with said rectilinear secondary actuator element, for generating an output representative of the position of said rectilinear secondary actuator element relative to a predetermined location on the travel path of said rectilinear secondary actuator element;

and

fifth means, coupled to said third and fourth means, for causing said third means to control the generation of said magnetic field by said first means in accordance with the output generated by said fourth means.

10. A system according to claim 3, wherein said third means includes means for generating a periodic pulse output signal the pulse width of which is representative of the magnitude of said prescribed force input.

11. A system according to claim 10, wherein said third means includes means for generating a signal representative of the direction of application of said prescribed force input to said rectilinear secondary actuator element.

12. A system according to claim 11, wherein said primary winding comprises a primary winding of a linear direct current motor and said rectilinear secondary actuator element comprises a moveable secondary member of said linear direct current motor magnetically coupled with said primary winding and rectilinearly moved thereby in response to the generation of a magnetic field controlled by said third means.

13. A system according to claim 12, wherein said third means includes means for controlling the generation of the magnetic field by said primary winding in accordance with said periodic pulse output signal and said direction of application representative signal.

14. A system according to claim 10, wherein said third means includes means, responsive to said prescribed force input representative signal, for generating a pulse width modulation signal in accordance with magnitude of said force input representative signal and a signal representative of the polarity of said force input representative signal.

15. A system according to claim 14, wherein said third means includes means for controlling the generation of said magnetic field by said primary winding in accordance with said pulse width modulation signal and said force polarity representative signal.

16. A system according to claim 3, wherein said third means includes means for controlling the generation of said magnetic field by said first means in accordance with the flow of current in said primary winding in response to said prescribed force input representative signal.

17. A system according to claim 16, wherein said third means includes means for generating a periodic pulse output signal the pulse width of which is representative of the magnitude of said prescribed force input.

18. A system according to claim 17, wherein said third means includes means, responsive to said prescribed force input representative signal, for generating a pulse width modulation signal in accordance with magnitude of said force input representative signal and a signal representative of the polarity of said force input representative signal.

19. A system according to claim 18, wherein said third means includes means for controlling the generation of said magnetic field by said primary winding in accordance with said pulse width modulation signal and said force polarity representative signal.

20. A system according to claim 19, wherein said third means includes means for adjusting said pulse width modulation signal in accordance with the flow of current in said primary winding.

21. For use with a space-deployed structure that is subject to vibrational movement, a system for imparting a controlled dampening force to said structure, so as to counter said vibrational movement comprising:

a linear direct current motor having a primary winding and a rectilinear secondary actuator element magnetically coupled therewith, so that, in response to the generation of a magnetic field by said primary winding, there is effective rectilinear oscillatory motion between said primary winding and said secondary actuator element;

wherein

one of said primary winding and said rectilinear secondary actuator element is attached to said structure while the other of said primary winding and said rectilinear secondary actuator element is freely translatable with respect to said structure, whereby, in response to the generation of a magnetic field by said primary winding, there is relative movement between the other of said primary winding and said rectilinear secondary actuator element and said structure, so that a vibrational movement compensating force, against which said structure reacts, may be generated by said linear direct current motor, to thereby impart a controlled dampening force to said structure, and wherein

relative movement between said other of said primary winding and said rectilinear secondary actuator element and said structure is controlled exclusive by controlled magnetic field interaction between said primary winding and said rectilinear secondary actuator elements.

22. A system according to claim 21, further comprising means for monitoring the displacement between said primary winding and said rectilinear secondary actuator element on the travel path of the movable one thereof and measuring the length of time that displacement therebetween is effectively positioned to one side of a predetermined location on said travel path and measuring the length of time that the displacement therebetween is effectively positioned to a second side of said predetermined location;

and

means, coupled to said primary winding and said monitoring means, for adjusting the energization of said winding in accordance with a difference in the length of time measurement carried out by said monitoring means over a prescribed time interval in excess of the period of the lowest frequency of oscillation imparted to the freely translatable one of said primary winding and said rectilinear secondary actuator element.

23. A method of controlling vibration of a mechanical structure comprising the steps of:

(a) coupling to said mechanical structure a linear direct current motor having a primary winding and a secondary member rectilinearly movable with respect to said primary winding, such that one of said primary winding and said secondary member is fixed with said mechanical structure and the other of said primary winding and said secondary member is movable with respect to said structure so as to be able to impart thereto a controlled linear inertial input by its movement;

(b) applying a prescribed force input representative signal to said primary winding so as to cause the movable one of said primary winding and said secondary member to undergo a prescribed oscillatory rectilinear movement with respect to said mechanical structure and thereby effectively compensate for destabilizing vibrations of said mechanical structure resulting from force inputs other than said prescribed force input;

(c) monitoring the relative movement between said primary winding and said secondary member on the rectilinear travel path of the movable one thereof and generating a signal representative of the location of displacement between said secondary member and said primary winding;

(d) controlling the energization of said primary winding in accordance with the signal generated in step (c);

(e) monitoring the displacement between said primary winding and said secondary member on the travel path of the moveable one thereof and measuring the length of time that the displacement between said primary winding and said secondary member is effectively positioned to one side of a predetermined location on said travel path and measuring the length of time that the displacement between said primary winding and said secondary member is effectively positioned to a second side of said predetermined location; and

(f) adjusting the energization of said primary winding in accordance with a difference in the length of time measurements carried out in step (e) over a prescribed time interval in excess of the period of the lowest frequency of oscillation of said prescribed force input representative signal.

24. A method according to claim 23, further including the steps of:

(g) controlling the energization of said primary winding in accordance with the flow of current in said primary winding in response to said prescribed force input representative signal.

25. A method according to claim 24, wherein step (b) comprises controllably applying a pulse width modulation signal to coils of said primary winding in accordance with prescribed force representative input signal and the signal generated in step (c).

26. A method according to claim 25, wherein step (c) comprises optically monitoring the relative movement between said primary winding and said secondary member.

27. A method according to claim 26, wherein step (e) comprises optically monitoring the relative displacement between said primary winding and said secondary member.

28. For use with a structure that is subject to vibrational movement, a method for imparting a controlled dampening force to said structure so as to counter said vibrational movement comprising the steps of:

(a) providing a moveable means to be translated in an oscillatory movement with respect to said structure and thereby impart to said structure a vibrational movement compensating force against which said structure reacts, so that the vibrational movement thereof may be effectively countered by the controlled movement of said means; and

(b) providing, at a location on said structure whereat said vibrational movement may occur, a rectilinear travel path of said moveable means to be translated therealong in an oscillatory manner;

(c) imparting a controlled force to said moveable means so as to cause said moveable means to oscillate along said rectilinear travel path; and

wherein one of said movable means and said rectilinear travel path comprises a winding of an electric motor and the other of said means and said rectilinear travel path comprises a linear magnetic field responsive element magnetically interacting with said winding of said electric motor, so that said winding may impart a force to said element, and wherein

the oscillatory translation of said moveable means is controlled exclusively by controlled magnetic field interaction between said winding and said linear magnetic field responsive element.

29. A method according to claim 28, further comprising the steps of

(d) monitoring the displacement between said winding and said element on the travel path of the movable one thereof and measuring the length of time that displacement therebetween is positioned to one side of a predetermined location on said travel path and measuring the length of time that the displacement therebetween is effectively positioned to a second side of said predetermined location;

and

(e) adjusting the energization of said winding in accordance with a difference in the length of time measurement carried out in step (d) over a prescribed time interval in excess of the period of the lowest frequency of oscillation imparted to said moveable means.