Effects of Structural Failure on the Safe Flight Envelope of Aircraft-Reference-Cited by-同舟云学术

Effects of Structural Failure on the Safe Flight Envelope of Aircraft

Published:2018-06 Issue:6 Volume:41 Page:1257-1275
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Nabi H. N.¹,Lombaerts T.²,Zhang Y.³,van Kampen E.³,Chu Q. P.³,de Visser C. C.³

Affiliation:

1. Polytechnic University of Milan, 20156 Milan, Italy

2. NASA Ames Research Center, Moffett Field, California 94035

3. Delft University of Technology, 2629 HS Delft, The Netherlands

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.G003184

Reference37 articles.

1. “Statistical Summary of Commercial Jet Airplane Accidents—Worldwide Operations 1959–2015,” Aviation Safety, Boeing Commercial Airplanes, TR, Seattle, WA, 2016, http://www.boeing.com/news/techissues/pdf/statsum.pdf [retrieved 31 Aug. 2017].

2. Nonlinear Analysis of Aircraft Loss of Control

3. A review of uncertainty in flight vehicle structural damage monitoring, diagnosis and control: Challenges and opportunities

4. LombaertsT. J. J. “Fault Tolerant Flight Control: A Physical Model Approach,” Ph.D. Dissertation, Faculty of Aerospace Engineering, Delft Univ. of Technology, Delft, The Netherlands, May 2010, http://repository.tudelft.nl/view/ir/uuid%3A538b0174-fe84-43af-954d-02f256b2ec50/ [retrieved 2018].

5. Piloted Simulator Evaluation of New Fault-Tolerant Flight Control Algorithms for Reconstructed Accident Scenarios

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