Switching Control Architecture with Parametric Optimization for Aircraft Upset Recovery-Reference-Cited by-同舟云学术

Switching Control Architecture with Parametric Optimization for Aircraft Upset Recovery

Published:2019-09 Issue:9 Volume:42 Page:2055-2068
ISSN:1533-3884
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Yildiz Anil¹,Akcal M. Ugur¹,Hostas Batuhan¹,Ure N. Kemal¹

Affiliation:

1. Istanbul Technical University, Istanbul 34469, Turkey

Funder

Türkiye Bilimsel ve Teknolojik Araştirma Kurumu

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.G004180

Reference37 articles.

1. “Statistical Summary of Commercial Jet Airplane Accidents, Worldwide Operations 1959–2012,” Aviation Safety, Boeing Commercial Airplanes TR, Seattle, WA, 2010, http://www.boeing.com/news/techissues/pdf/statsum.pdf.

2. Aircraft Loss-of-Control Accident Analysis

3. Analysis of Control Strategies for Aircraft Flight Upset Recovery

4. Future Integrated Systems Concept for Preventing Aircraft Loss-of-Control Accidents

5. “Stall Prevention and Recovery Training, Advisory Circular 120-109A, CNG 1,” Federal Aviation Administration TR 120-109A, Dept. of Transportation, Nov. 2015, https://www.faa.gov/documentLibrary/media/Advisory_Circular/AC_120-109A_CHG_1.pdf.

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