METHOD FOR ADAPTIVE CORRECTION OF THE PHASE NON-UNIFORMITY OF A LIQUID CRYSTAL LIGHT VALVE
Assignee
Hughes Aircraft
Filed as: HUGHES AIRCRAFT COMPANY, A CORP OF DE
Filed
Dec 24, 1986
Granted
Sep 17, 1991
Location
LOS ANGELES CA US
Abstract
Apparatus for compensating for inherent distortions in a modified liquid crystal light valve used in an integrated wavefront sensing and wavefront control system for laser optics. A main wavefront sensing and control system utilizes a liquid crystal light valve selected for response speed but having inherent surface non-linearities. A beam from an auxiliary laser is intermittently applied, while the main laser is blocked, to both the fast response LCLV of the main system and to a slower response LCLV of an associated correction system. The second LCLV system corrects for the non-linearities in the surface of the first LCLV and then maintains the stored correction signal for a decay interval which corresponds to several response times of the main LCLV, thus permitting the main LCLV system to perform fast correction of atmospheric aberrations in the laser beam wavefront unaffected by inherent surface non-linearities.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Sep 18, 1987
Rescinded
Aug 6, 1990
Duration
2 years, 10 months
Inventor
- 1UZI EFRON
Record Details
- Patent number
- US 5048935
- Application
- 06947575
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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