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Feedback controlled optics with wavefront compensationThe sensitivity model of a complex optical system obtained by linear ray tracing is used to compute a control gain matrix by imposing the mathematical condition for minimizing the total wavefront error at the optical system's exit pupil. The most recent deformations or error states of the controlled segments or optical surfaces of the system are then assembled as an error vector, and the error vector is transformed by the control gain matrix to produce the exact control variables which will minimize the total wavefront error at the exit pupil of the optical system. These exact control variables are then applied to the actuators controlling the various optical surfaces in the system causing the immediate reduction in total wavefront error observed at the exit pupil of the optical system.
Document ID
19940015832
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Breckenridge, William G.
(Jet Propulsion Lab. California Inst. of Tech., Pasadena., United States)
Redding, David C.
(Jet Propulsion Lab. California Inst. of Tech., Pasadena., United States)
Date Acquired
August 16, 2013
Publication Date
November 23, 1993
Subject Category
Optics
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-700379
Patent Number: NASA-CASE-NPO-18194-1-CU
Patent Number: US-PATENT-5,265,034
Accession Number
94N20305
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-NPO-18194-1-CU|US-PATENT-5,265,034
Patent Application
US-PATENT-APPL-SN-700379
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