Aerodynamic Parameter Estimation from Flight Data Applying Extended and Unscented Kalman Filter-Reference-Cited by-同舟云学术

Aerodynamic Parameter Estimation from Flight Data Applying Extended and Unscented Kalman Filter

Published:2006-06-25 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
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Author:

Chowdhary Girish¹,Jategaonkar Ravindra¹

Affiliation:

1. DLR Institute for Flight Systems

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6146

Reference26 articles.

1. Jategaonkar, R.V.,FlightVehicle System Identification:A TimeDomain Methodology,AIAAProgressinAeronauticsand Astronautics,Vol.216,AIAA,Reston,VA,Aug2006.

2. Chowdhary, G., and Lorenz, S, "Control of a VTOL UAV using Online Parameter Identification", AIAA-2005-6409, August2005.

3. Buckland, J. H., Musgrave, J. L., and Walker, B. K. "On-Line Implementation of nonlinear Parameter Estimation for the SpaceShuttleMainEngine",NASATM-106097,1992.

4. Dittirich J., Bernartz A., and Thielecke F. "Intelligent Systems Research using a Small Autonomous Rotorcraft Testbed", AIAA-2003-6561,September2003.

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