Development of Nonlinear Aerodynamic Models from Flight Data and Evaluation of Tabulated Aerodynamic Models-Reference-Cited by-同舟云学术

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Development of Nonlinear Aerodynamic Models from Flight Data and Evaluation of Tabulated Aerodynamic Models

Published:2003-06-22 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
Short-container-title:

Author:

Lan Chuan-Tau¹,Brandon Jay²

Affiliation:

1. University of Kansas

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5696

Reference31 articles.

1. Wang, Z.; Lan, C. E. and Brandon, J. M. "Fuzzy-Logic Modeling of Nonlinear Unsteady Aerodynamics," AIAA Paper 98-4351, Aug.

2. Fuzzy logic modeling of lateral-directional unsteady aerodynamics

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1. Nonlinear aerodynamics of an unmanned aircraft in wind shear;Aircraft Engineering and Aerospace Technology;2017-01-03

2. Examination of excessive fuel consumption for transport jet aircraft based on fuzzy-logic models of flight data;Fuzzy Sets and Systems;2015-06

3. Performance Diagnosis for Turbojet Engines Based on Flight Data;Journal of Aerospace Engineering;2014-01

4. Stability Characteristics for Transport Aircraft Response to Clear-Air Turbulence;Journal of Aerospace Engineering;2010-07

5. Estimation of Nonlinear Aerodynamic Roll Models for Identification Of Uncommanded Rolling Motions;Journal of Aircraft;2008-05

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