The Boeing Company

National Technology & Engineering Solutions of Sandia, LLC

Sandia Corporation

David Bossert

Steven Fulton Griffin

Charles A Walker

Peter Schwindt

Jongmin Lee

Dennis Rossbach

Aaron M Ison

Daniel Paul Gillund

Karl N Schrader

Garry R Marions

Kyle H Fuerschbach

A compact grating-mirror magneto-optical trap (GMOT) cold atom inertial sensor head is disclosed. To make the sensor head compatible with the high vibration levels encountered in dynamic environments, the number of optical ports in the vacuum chamber is minimized and various components, including fixed optical components and a reflective grating chip, are hard mounted within the vacuum chamber. The use of the reflective grating chip reduces the number of optical ports required for cooling beams from six to one. The number of optical ports is further reduced by time multiplexing multiple beams passing through a given optical port.

Compact grating magneto-optical trap sensor head for inertial navigation in dynamic environments

Technologies pertaining to a multi-aperture optical imaging system are described herein. The multi-aperture optical system comprises an afocal optical telescope and a plurality of sub-apertures that receive light from the telescope. Each sub-aperture comprises a focusing optic that creates a full-field image onto an individual image sensor that outputs data indicative of an intensity of light received at the sensor. Image processing techniques can be used to combine the sensor outputs for spectral discrimination, to improve dynamic range or to enhance resolution of a scene.

Multi-aperture optical system for high-resolution imaging

An imaging Doppler lidar (IDL) enables the measurement of the velocity distribution of a large volume, in parallel, and at high spatial resolution in the wake of a wind turbine. Because the IDL is non-scanning, it can be orders of magnitude faster than conventional coherent lidar approaches. Scattering can be obtained from naturally occurring aerosol particles. Furthermore, the wind velocity can be measured directly from Doppler shifts of the laser light, so the measurement can be accomplished at large standoff and at wide fields-of-view.

Imaging doppler lidar for wind turbine wake profiling

The present embodiment provides a system and method for lowering the saturated gain level of a thin-disk laser oscillator by multipassing each gain generator in such a way to cancel some of the wavefront error contributions from the disk surfaces. Wavefront aberrations introduced on one pass of the gain disk are canceled through symmetry on successive passes. The reduced wavefront error significantly improves design space for single-mode resonators. Maximum effectiveness is achieved by rotating the gain disk so that the fold plane-of-symmetry reverses the largest wavefront error or specifically chosen functional forms.

Re-entrant structure for thin disk resonators

A laser beam correction system and related methods of use and manufacture are provided. In one example, a laser beam correction system includes a mirror having a first surface and a second surface. An actuator comprising a piezoelectric ceramic disk and a plurality of conductive electrodes on substantially opposing sides of the disk is bonded to the second surface of the mirror. The actuator includes an aperture in a center portion. A wave-front sensor is adapted to measure optical wave-front characteristics of a laser beam received by the mirror and provide electronic signals corresponding to the wave-front characteristics.

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Albuquerque, NM, United States of America

David Bossert