A Robust Flare Planning Logic for Unmanned Aerial Vehicle Applications

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX09CC02P
Agency Tracking Number: 084093
Amount: $99,996.00
Phase: Phase I
Program: SBIR
Awards Year: 2009
Solicitation Year: 2008
Solicitation Topic Code: A1.09
Solicitation Number: N/A
Small Business Information
9950 Wakeman Drive, Manassas, VA, 20110-2702
DUNS: 604717165
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Antonio Abad
 Principal Investigator
 (617) 500-7048
Business Contact
 Scott Hart
Title: Financial Analyst
Phone: (617) 500-0536
Email: shart@aurora.aero
Research Institution
Aurora Flight Sciences proposes to develop a flare planning logic that would provide aircraft guidance during this critical phase of flight. The algorithms that Aurora seeks to leverage address the reachability problem in the fields of Optimal Control and Hybrid Systems. Two competing technical approaches will beconsidered; Aurora collectively refers to them as "Safety Verification-based algorithms."To this end, Aurora proposes the innovation of applying a suitable version of these algorithms to the design of a flare maneuver guidance and planning logic. The planner will be capable of dynamically producing a flare maneuver guaranteed not to violate the aircraft flight envelope and other stipulated constraints. The planner will meet the robustness requirements stipulated in the topic solicitation; namely, it will apply to both impeded and unimpeded aircraft, and it will operate under significant weather disturbances. The main technical challenge in developing the planning logic is extending and applying the chosen control algorithms to 6-DOF aircraft dynamics models under the required variety of operating conditions. The ultimate goal of the Phase 1 effort is to explore the feasibility of applying Safety Verification-based optimal control algorithms to an appropriately sophisticated model of the aircraft dynamics during the flare maneuver.

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

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