METHOD FOR IMPROVING THE SPATIAL RESOLUTION IN AN INTEGRATED ADAPTIVE OPTICS APPARATUS
Assignee
Hughes Aircraft
Filed as: HUGHES AIRCRAFT COMPANY
Filed
May 20, 1986
Granted
Aug 27, 1991
Location
El Segundo CA (Aerospace Corp/TRW)
Abstract
Apparatus is disclosed for correcting wavefront errors in adaptive optics systems. A modified liquid crystal light valve is used as an integrated wavefront sensing and wavefront control system. A remote reference aberrated wavefront 10 first reflects off the liquid crystal substrate 20 and is then transferred by beam-splitters 14 and 15a, b and reflector 19 to the rear surface ofo the liquid crystal light valve 12. A one-to-one imaging system composed of lenses 70a, b and spatial filter 72 provide a new diffraction-limited optical transfer system which allows full use of the extremely high resolution capabilities of the liquid crystal light valve 12. The wavefront 10, after being imaged by the optical transfer system, is combined with a local reference plane 16, the interference pattern from which strikes the rear surface photoconductor 26. The photoconductor electrons liberated serve to alter the voltage across the liquid crystal at those points where the interference pattern has right maxima. Using a tunable birefringent liquid crystal layer 20, a voltage change causes a commensurate refractive index change in the liquid crystal substrate. These refractive index changes alter the optical path length of particular portions of the aberrated wavefront and the device's inherent negative feedback drives these phase errors to zero, at which point the wavefront 18 is completely corrected. A second laser beam 11 may be sent out of the device, reflecting off the corrective liquid crystal layer and predistorting it in order to correct for atmospheric path disturbances. The present invention provides an adaptive optics correction system possessing extraordinarily high spatial resolution.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Oct 29, 1987
Rescinded
Dec 31, 1990
Duration
3 years, 2 months
Inventor
- 1DAVID M. PEPPER
Sensitive facility: El Segundo CA (Aerospace Corp/TRW)
Record Details
- Patent number
- US 5042922
- Application
- 06865224
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
Hughes AircraftMore from this assignee
DIGITAL CIRCUIT WITH TRANSISTOR GEOMETRY AND CHANNEL STOPS PROVIDING CAMOUFLAGE AGAINST REVERSE ENGINEERING
Hughes Aircraft
MISSILE FIRE CONTROL SYSTEM
Hughes Aircraft
COORDINATE TRANSFORMATION SYSTEM
Hughes Aircraft
POLYROD ANTENNA WITH FLARED NOTCH FEED
Hughes Aircraft
NEAR-RANGE MICROWAVE DETECTION FOR FREQUENCY-MODULATION CONTINUOUS- WAVE AND STEPPED FREQUENCY RADAR SYSTEMS
Hughes Aircraft
LINEAR ARRAY LATERAL MOTION COMPENSATION METHOD
Hughes Aircraft
Related by domain
MISSILE GUIDANCE SYSTEM
Raytheon
APPARATUS FOR CONTROLLING THE POSITION AND DIRECTION OF A LASER BEAM
LASER ALONG BODY TRACKER (SABOT II)
TRW
LASER ALONG-BODY TRACKER (SABOT III)
TRW
ARTICLE COMPRISING A UNIPOLAR SUPERLATTICE LASER
LUCENT TECHNOLOGIES INC.
INTRACAVITY QUANTUM WELL PHOTODETECTOR INTEGRATED WITHIN A VERTICAL-CAVITY SURFACE-EMITTING LASER AND METHOD OF OPERATING SAME
CALIFORNIA, UNIVERSITY OF, THE, REGENTS OF, THE