Avionics for Scaled Remotely Operated Vehicles

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX08CC51P
Agency Tracking Number: 074091
Amount: $98,662.00
Phase: Phase I
Program: SBIR
Awards Year: 2008
Solicitation Year: 2007
Solicitation Topic Code: A1.09
Solicitation Number: N/A
Small Business Information
Coherent Technical Services, Inc.
46655 Expedition Drive, Suite 101, Lexington Park, MD, 20653-5120
DUNS: 619354488
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Ian Gallimore
 Principal Investigator
 (301) 880-3341
 Ian.Gallimore@goCTSi.com
Business Contact
 Tom Sanders
Title: Managing Director
Phone: (301) 880-3341
Email: Tom.Sanders@goCTSi.com
Research Institution
N/A
Abstract
The use of UAVs has increased exponentially since 1995, and this growth is expected to continue. Many of these applications require extensive Research and Development; however, the need to fund development of the UAV often competes with funding intended for the end-user application. Therefore, off the shelf, low cost, easily configurable integrated avionics systems will significantly reduce the budget impact for UAVs yet will support the wide range of applications for their use. CTSi and Virginia Commonwealth University are proposing the use of an integrated VCU developed avionics package with a user configurable autopilot system that will meet the needs of a wide range of experimental test bed UAVs. The system will include: 1. The ability for the safety pilot to take direct control of the aircraft using an on-board fail-safe control switch 2. A built-in autopilot to provide return-to-home capability upon failure of the RF links, safety/ground pilot assistance in performing research maneuvers, and limited upset recovery 3. An open-architecture hardware design enabling customer upgrade of sensors, actuators, and data links 4. An open-architecture software design enabling push-button auto-coding of control algorithms direct from Simulink 5. A flexible architecture allowing customer-developed control laws to be executed on ground-based computers via uplink and downlink telemetry or onboard the aircraft using an optional Advanced Adaptive Flight Control Processor.

* information listed above is at the time of submission.

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