Rapid Estimation of Aircraft Performance Models using Differential Vortex Panel Method and Extended Kalman Filter

Award Information
Agency:
National Aeronautics and Space Administration
Amount:
$100,000.00
Program:
SBIR
Contract:
NNX08CA50P
Solitcitation Year:
2007
Solicitation Number:
N/A
Branch:
N/A
Award Year:
2008
Phase:
Phase I
Agency Tracking Number:
075446
Solicitation Topic Code:
A1.04
Small Business Information
Optimal Synthesis, Inc.
868 San Antonio Road, Palo Alto, CA, 94303-4622
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
Y
Duns:
829385509
Principal Investigator
 P. K. Menon
 Principal Investigator
 (650) 213-8585
 menon@optisyn.com
Business Contact
 P. Menon
Title: Business Official
Phone: (650) 213-8585
Email: menon@optisyn.com
Research Institution
N/A
Abstract
Estimation of aerodynamic models for the control of damaged aircraft using an innovative differential vortex lattice method tightly coupled with an extended Kalman filter is proposed. The approach exploits prior knowledge about the undamaged aircraft to reduce the order of the estimation problem. Test maneuvers will be designed to improve the observability of the system dynamics. The derived performance model will then be used to determine the aircraft flight envelope, performance parameters and the maneuver limits. The objective is to develop an aircraft performance model online to permit the derivation of viable landing guidance laws for damaged aircraft. Phase I research will demonstrate the feasibility of the proposed concept using a NASA-supplied aircraft simulation. Complete aircraft performance estimation system will be developed during the Phase II research and evaluated in real-time, high-fidelity simulations.

* information listed above is at the time of submission.

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