The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 22, 2000

Filed:

Jan. 26, 1999
Applicant:
Inventors:

Richard S Jackson, Lakewood, CO (US);

Girard M Manke, Huntington Beach, CA (US);

Assignees:

Lockheed Martin Corporation, Bethesda, MD (US);

The Aerospace Corporation, El Segundo, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05B / ; H02K / ; G02B / ; B64G / ; F16H / ;
U.S. Cl.
CPC ...
318611 ; 318616 ; 318623 ; 318648 ; 318649 ; 318 37 ; 318 58 ; 318161 ; 700 60 ; 359199 ; 359213 ; 244165 ; 310 36 ; 310 74 ;
Abstract

A control system stabilizes the flexible body bending modes of a space, airborne, or ground-based system, while providing angular position control of an oscillating mass connected to a counter-oscillating counterbalance. The actuating mechanism uses two drive motors to exert torques on the mass and counterbalance, respectively, under the control of a feedback controller. The controller has a first control channel generating a first torque command signal for the first drive based on the angular position of the mass, and a second control channel generating a second torque command signal for the second drive based on the angular position of the counterbalance and a torque cross-feed signal from the first control channel. The second control channel includes a notch filter for removing input frequencies in a predetermined bandwidth about the frequency of the first torque command signal. The same controller can be used to control the system in oscillation and for large angle repositioning of the mass and counterbalance. The present invention provides a control system for a highly precise and efficient mechanical scanning device suitable for use in a space-based LIDAR system or other similar systems.


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