You are here

Aerodynamics and Flight Control Design for Hovering MUAVs

Award Information
Agency: Department of Defense
Branch: Defense Advanced Research Projects Agency
Contract: N/A
Agency Tracking Number: 32531
Amount: $98,463.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Solicitation Year: N/A
Award Year: 1996
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
9950 Wakeman Drive,
Manassas, VA 20110
United States
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Ben Motazed
 (703) 369-3633
Business Contact
Phone: () -
Research Institution

Aurora Flight Sciences, with expertise in designing and manufacturing low Reynolds number high-altitude aircraft, proposes to develop new aerodynamics computational tools and flight control solutions to enable the development of 15cm and smaller hovering micro unmanned aerial vehicles (MUAV)s. The objective of this project is to validate the analytical approach, and refine the proposed MUAV design by proof-of-concept experiments and demonstrations. The Phase I project will result in the development of an aerodynamically efficient hovering MAUV, augmented by a passive stabilization control scheme, to exhibit functional hovering and control performance to accommodate the integration of miniaturized electronic subcomponents in Phase II.

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

US Flag An Official Website of the United States Government