An Application of Equation Error Method to Aerodynamic Model Identification and Parameter Estimation of a Gliding Flight Vehicle-Reference-Cited by-同舟云学术

An Application of Equation Error Method to Aerodynamic Model Identification and Parameter Estimation of a Gliding Flight Vehicle

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
language:
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Author:

Kutluay Umit¹,Mahmutyazicioglu Gokmen¹,Platin Bulent²

Affiliation:

1. TÜBITAK-SAGE

2. Middle East Technical University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-5724

Reference7 articles.

1. Evolution of flight vehicle system identification

2. Automated Simulation Updates Based on Flight Data

3. Jategaonkar, R. V. "Flight Vehicle System Identification: A Time Domain Methodology", Progress in Astronautics and AeronauticsVolume216,AIAA,2006.

4. Application of System Identification to Aircraft at NASA Langley Research Center

5. Klein, V., Batterson, J. G. "Determination of Airplane Model Structure from Flight Data Using Splines and Stepwise Regression",NASA TP 2126,NASA,1983.

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