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:
Dec. 28, 2004

Filed:

Jul. 03, 2002
Applicant:
Inventor:

David A. Osterberg, Phoenix, AZ (US);

Assignee:

Honeywell International Inc., Morristown, NJ (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16M 1/00 ;
U.S. Cl.
CPC ...
F16M 1/00 ;
Abstract

A method and system for calculating a control function for a structural system ( ) that can be used to determine an appropriate control force to apply to an active member ( ) within a stationary member ( ) on the structural system ( ). An active member ( ) and a stationary member ( ) are defined as a two-mass system in which the active member ( ) and the stationary member ( ) move in opposite directions. The stationary member ( ) is mounted to an isolation subsystem ( ) that is composed of six isolators ( ) at multiple degrees of freedom. The isolation subsystem ( ) is softer than the stationary member ( ), active member ( ) and a spacecraft surface ( ) due to a damping element ( ) of the isolation subsystem ( ). The isolation subsystem ( ) is mounted to the spacecraft ( ) and decouples the spacecraft ( ) from the stationary member ( ) and thus the active member ( ). An accurate control force for the active member ( ) can be determined based upon the above structure ( ).


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