Lockheed Martin Corporation

Samuel George Williams

Ich V Pham

An adaptive optics system comprises a beamsplitter configured to divide an incoming beam with an aberrated wave front into a first input beam and a second input beam, a microelectromechanical system configured to reflect the first input beam onto an image plane, and a self-reference wave front generator configured to spatially filter the second input beam to form a reference beam, and to interfere the reference beam with the first input beam on the image plane to form a hologram. The system further comprises an imaging device configured to capture an image of the hologram on the image plane, and one or more processors. The one or more processors are configured to perform the steps of Fourier transforming the captured image to generate a transform including a first object image, a conjugate object image, and an auto-correlation image, truncating the transform to exclude the conjugate object image and the auto-correlation image, inverse Fourier transforming the truncated transform to generate amplitude and phase information about the aberrated wave front, generating control signals for mitigating aberrations in the aberrated wave front via phase conjugation based on the amplitude and phase information, and providing the control signals to the microelectromechanical system.

High performance adaptive optics with a reconstructed coherent wave front

A system for precisely determining directionality of an output beam includes a beam source and a body position identifier facing opposite directions, with a grating rhomb positioned to provide an attenuated sample beam from the beam source into the oppositely directed body positioned identifier. In the preferred embodiment, the beam source is a pulsed laser source and the body position identifier is a star tracker for forming a stellar map. The grating rhomb includes first and second grating members. The first grating member extends across the optical path of the output beam and has a geometry to diffract a minor portion of the output beam intensity while passing a major portion of the output beam for continued propagation in a first direction. The second grating member is positioned to traverse the field of view of the body position identifier. In the preferred embodiment, the first grating member traverses the optical axis of the output beam and the second grating member is at the intersection of the optical axis of the body position identifier and the optical axis of the diffracted sample beam from the first grating member. The system also includes an auto-collimator that is used to monitor the orientation of the two grating members. When used in a space application, the system also includes a Global Positioning System receiver.

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Cupertino, CA, United States of America

Samuel George Williams