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Global Radius of Curvature Estimation and Control System for Segmented MirrorsAn apparatus controls positions of plural mirror segments in a segmented mirror with an edge sensor system and a controller. Current mirror segment edge sensor measurements and edge sensor reference measurements are compared with calculated edge sensor bias measurements representing a global radius of curvature. Accumulated prior actuator commands output from an edge sensor control unit are combined with an estimator matrix to form the edge sensor bias measurements. An optimal control matrix unit then accumulates the plurality of edge sensor error signals calculated by the summation unit and outputs the corresponding plurality of actuator commands. The plural mirror actuators respond to the actuator commands by moving respective positions of the mixor segments. A predetermined number of boundary conditions, corresponding to a plurality of hexagonal mirror locations, are removed to afford mathematical matrix calculation.
Document ID
20060050060
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Rakoczy, John M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 23, 2013
Publication Date
May 23, 2006
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Number: NASA-Case-MFS-31807-1
Patent Application Number: US-Patent-Appl-SN-637085
Patent Number: US-Patent-7,050,161
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-MFS-31807-1|US-Patent-7,050,161
Patent Application
US-Patent-Appl-SN-637085
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