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Unmanned Aerial Vehicles (UAV) Precision Geolocation

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA9453-07-C-0035
Agency Tracking Number: A052-089-4021
Amount: $749,505.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: A05-089
Solicitation Number: 2005.2
Timeline
Solicitation Year: 2005
Award Year: 2007
Award Start Date (Proposal Award Date): 2007-02-23
Award End Date (Contract End Date): 2009-05-22
Small Business Information
700 Research Center Blvd.
Fayetteville, AR 72701
United States
DUNS: 044870363
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 TERRY TIDWELL
 Sr. Research Specialist I
 (479) 251-8229
 ttidwell@spacephotonics.com
Business Contact
 Charles Chalfant
Title: CEO
Phone: (479) 575-5316
Email: cchalfant@spacephotonics.com
Research Institution
N/A
Abstract

In order to realize the benefits of formation flying multi-spacecraft clusters, four key elements must be present: 1. Broadband inter-spacecraft communications to enable the transport of high resolution sensor data. 2. Precision inter-spacecraft timing synchronization to enable precise multi-sensor sampling throughout the cluster. 3. Precision inter-spacecraft relative range to enable the determination of precise spacecraft and sensor spacing within the cluster. 4. Precision inter-spacecraft relative position to enable the determination of precise cluster and sensor plane orientation. An inter-spacecraft laser communications network is the only integrated subsystem that can provide all four of these key elements. The proposed SBIR Phase II effort will leverage several existing SPI programs to extend the models and designs from the Phase I effort, and produce fully-functional prototype hardware at a minimum cost. Space Photonics will develop the algorithms, calibration processes, and VHDL code for the inter-spacecraft ranging, timing synchronization and inter-spacecraft position determination; and, will demonstrate these functions in our gimbal-less, free space optical, lasercom testbed. However, the algorithms, calibration processes, and VHDL code developed for this program can be applied to any gimbaled or gimbal-less lasercom crosslink system.

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

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