HALE Modeling Tools for Real Time Hardware-Coupled Aeroservoelastic Simulations

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$69,982.00
Award Year:
2006
Program:
SBIR
Phase:
Phase I
Contract:
NND06AA29C
Award Id:
78004
Agency Tracking Number:
054621
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
34 Lexington Avenue, Ewing, NJ, 08618
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
096857313
Principal Investigator:
ToddQuackenbush
Principal Investigator
(609) 538-0444
todd@continuum-dynamics.com
Business Contact:
BarbaraAgans
Business Official
(609) 538-0444
barbara@continuum-dynamics.com
Research Institute:
n/a
Abstract
Ongoing work under NASA sponsorship is defining promising High Altitude Long Endurance (HALE) demonstration vehicle designs for remote sensing, communication relay, environmental monitoring, and other critical missions. Continuing challenges in preparing these vehicles for flight test include issues that will also be critical in the development of operational HALE vehicles: time-accurate simulation of aeroelastic effects; simulation-based design of flight control and propulsion systems for high efficiency, structural stability, and adequate control at all flight conditions; and effective, validated, full-vehicle dynamics analyses for aeroservoelastic applications. The proposed effort will address these needs by making available modular, state of the art modeling tools for use in full aircraft simulations to support vehicle assessment and control system design throughout the HALE flight test and development process. These tools will be operable in a range of modes with up to real-time turnaround and will feature a unique ability to support hardware-coupled ("hardware in the loop") simulation in conjunction with finite element-based aeroelastic modeling. This capability will support both near term flight demonstrations of prospective HALE vehicles and long-term design and analysis tasks for NASA HALE platforms.

* information listed above is at the time of submission.

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