Post-Stall Aerodynamic Modeling and Gain-Scheduled Control Design-Reference-Cited by-同舟云学术

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Post-Stall Aerodynamic Modeling and Gain-Scheduled Control Design

Published:2005-06-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
language:
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Author:

Wu Fen¹,Gopalarathnam Ashok¹,Kim Sungwan²

Affiliation:

1. North Carolina State University

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6169

Reference29 articles.

1. Some Recent Developments in Airfoil Theory

2. 5Piszkin, S. T. and Levinsky, E. S. "Nonlinear Lifting Line Theory for Predicting Stalling Instabilities on Wings of Moderate Aspect Ratio," Tech. rep., General Dynamics Convair Report CASD-NSC-76-001, June 1976.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Design of Control Law of Post Stall Maneuver under Unsteady Aerodynamics Based on Improved Dynamic Inverse Method;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2019-06

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