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Tools and Methods Toward the Advancement of Flight Control for Flexible Aircraft.

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Tools and Methods Toward the Advancement of Flight Control for Flexible Aircraft./
作者:	Quenzer, Jake D.
出版者:	Ann Arbor : ProQuest Dissertations & Theses, : 2019,
面頁冊數:	138 p.
附註:	Source: Dissertations Abstracts International, Volume: 80-10, Section: B.
Contained By:	Dissertations Abstracts International80-10B.
標題:	Aerospace engineering. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=13811841
ISBN:	9781392072813

Tools and Methods Toward the Advancement of Flight Control for Flexible Aircraft.
Quenzer, Jake D.

Tools and Methods Toward the Advancement of Flight Control for Flexible Aircraft. - Ann Arbor : ProQuest Dissertations & Theses, 2019 - 138 p.

Source: Dissertations Abstracts International, Volume: 80-10, Section: B.

Thesis (Ph.D.)--University of Washington, 2019.

This item must not be added to any third party search indexes.

Flight control of a flexible aircraft is a challenge that has become increasingly relevant over the last several decades. For the large twin-aisle commercial aircraft of today, automatic flight control systems are tasked not only with the traditional obligations of safe and stable flight with agreeable handling qualities for pilots, but are now additionally tasked with the mitigation of structural excursions (where objectives include load alleviation from disturbances including atmospheric turbulence and commanded maneuvers), as well as structural modal suppression (for improving ride quality and decreasing airframe fatigue), and may soon be responsible for the active suppression of aeroelastic flutter. These challenges strain or break the suitability of traditional system design and remedy-driven research efforts have been hampered by the scarcity of dynamics models in the public-domain as well as the cost, complexity, and delicate nature of corresponding experimental test beds. With regard to analysis, the multi-controller system architecture is a natural approach to many of the challenges described. In this work we investigate the robustness of stability guarantees for multi-controller systems via the switched system framework and quadratic common Lyapunov function. With regard to model scarcity, we present the development of the Generic Wide Body aircraft model and its simulation and evaluation environment. Finally, with regard to experimental cost and complexity, we present the development, fabrication, and validation of a low cost aeroelastic test bed.

ISBN: 9781392072813Subjects--Topical Terms:

686400
Aerospace engineering.
Subjects--Index Terms:

Aeroelastic

Tools and Methods Toward the Advancement of Flight Control for Flexible Aircraft.
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300 $a 138 p.
500 $a Source: Dissertations Abstracts International, Volume: 80-10, Section: B.
500 $a Publisher info.: Dissertation/Thesis.
500 $a Advisor: Morgansen, Kristi.
502 $a Thesis (Ph.D.)--University of Washington, 2019.
506 $a This item must not be added to any third party search indexes.
506 $a This item must not be sold to any third party vendors.
520 $a Flight control of a flexible aircraft is a challenge that has become increasingly relevant over the last several decades. For the large twin-aisle commercial aircraft of today, automatic flight control systems are tasked not only with the traditional obligations of safe and stable flight with agreeable handling qualities for pilots, but are now additionally tasked with the mitigation of structural excursions (where objectives include load alleviation from disturbances including atmospheric turbulence and commanded maneuvers), as well as structural modal suppression (for improving ride quality and decreasing airframe fatigue), and may soon be responsible for the active suppression of aeroelastic flutter. These challenges strain or break the suitability of traditional system design and remedy-driven research efforts have been hampered by the scarcity of dynamics models in the public-domain as well as the cost, complexity, and delicate nature of corresponding experimental test beds. With regard to analysis, the multi-controller system architecture is a natural approach to many of the challenges described. In this work we investigate the robustness of stability guarantees for multi-controller systems via the switched system framework and quadratic common Lyapunov function. With regard to model scarcity, we present the development of the Generic Wide Body aircraft model and its simulation and evaluation environment. Finally, with regard to experimental cost and complexity, we present the development, fabrication, and validation of a low cost aeroelastic test bed.
590 $a School code: 0250.
650 4 $a Aerospace engineering. $3 686400
653 $a Aeroelastic
653 $a Flight control
653 $a Switched systems
690 $a 0538
710 2 $a University of Washington. $b Aeronautics and Astronautics. $3 1178958
773 0 $t Dissertations Abstracts International $g 80-10B.
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793 $a English
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