Control of Commercial Aircraft with Vertical Tail Loss-Reference-Cited by-同舟云学术

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Control of Commercial Aircraft with Vertical Tail Loss

Published:2004-06-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA 4th Aviation Technology, Integration and Operations (ATIO) Forum
language:
Short-container-title:

Author:

Crider Leah¹

Affiliation:

1. General Electric Global Research

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-6293

Reference7 articles.

1. Stengel,RobertF.AircraftFlightDynamics(tobepublished),Chaps.1-6,Eq.4.1-100and4.1-101.

2. McLean,Donald.AutomaticFlightControlSystems,PrenticeHall,NewYork,1990,p.34,159-61

3. Stengel,RobertF.OptimalControlandEstimation,DoverPublications,NewYork,1986.Chap.6.

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1. Real-Time Vision-Based Aircraft Vertical Tail Damage Detection and Parameter Estimation;IETE Journal of Research;2022-02-23

2. Sliding Mode Robust Control for Maximum Allowable Vertical Tail Damage to Aircraft Based on Linear Matrix Inequality;Journal of Aerospace Engineering;2021-07

3. Fault Detection and Basic In-Flight Reconfiguration of a Small UAV Equipped with Elevons;IFAC-PapersOnLine;2018

4. Active fault tolerant control for vertical tail damaged aircraft with dissimilar redundant actuation system;Chinese Journal of Aeronautics;2016-10

5. Fly-by-wire robustness to flight dynamics change under horizontal stabiliser damage;The Aeronautical Journal;2016-05-10

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