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Non-Mechanical Dual-Mode Beam Control System for LiDARs

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: 80NSSC19C0481
Agency Tracking Number: 193556
Amount: $124,970.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: Z7
Solicitation Number: SBIR_19_P1
Timeline
Solicitation Year: 2019
Award Year: 2019
Award Start Date (Proposal Award Date): 2019-08-19
Award End Date (Contract End Date): 2020-02-18
Small Business Information
1300 Lee Rd.
Orlando, FL 32810-5851
United States
DUNS: 959414327
HUBZone Owned: No
Woman Owned: Yes
Socially and Economically Disadvantaged: No
Principal Investigator
 Anna Tabirian
 (407) 734-5222
 anna@beamco.com
Business Contact
 Morris Hicks
Phone: (228) 813-6325
Email: Morris.hicks@nasa.gov
Research Institution
N/A
Abstract

The objective of the proposal is exploring an opportunity for developing a versatile beam control system for LiDARs with both Doppler and time-of-flight measurement capability for enhanced navigation precision and reliability. New generation optics and electro-optics capabilities will be studied, adapted and customized to prove the feasibility of new generation LIDARs that could combine Doppler principles for object velocity measurements, and time-of-flight principles for direct altitude measurements. The system will be characterized by: 1) absence of mechanically moving parts, 2) a few millimeter thick planar structure even for large aperture sizes, 3) weighing grams only, 4) consuming a few milliwatts of electrical power, 5) controlled with voltages as small as 10V, 6) with millisecond, potentially, microsecond switching speeds, 7) ability to adapt to a wide range of ambient temperatures, and 8) resistance to mechanical shock and dust. The technology will enhance the dynamic range due to large area capability using thin and planar diffractive waveplate optics for controlling key propagation properties of both pulsed and cw laser beams. The Phase 1 objective is to develop the architectures and demonstrate feasibility of such a beam control system for the parameter range to be met for space vehicle landing applications.

* Information listed above is at the time of submission. *

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