Modeling and Control for a Blended Wing Body Aircraft: A Case Study
This book demonstrates the potential of the blended wing body (BWB) concept for significant improvement in both fuel efficiency and noise reduction and addresses the considerable challenges raised for control engineers because of characteristics like open-loop instability, large flexible structure,...
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2015
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oai:scholar.dlu.edu.vn:DLU123456789-577102023-11-11T05:51:16Z Modeling and Control for a Blended Wing Body Aircraft: A Case Study Kozek, Martin Schirrer, Alexander Engineering Computer simulation Wings Airplanes Mathematical models This book demonstrates the potential of the blended wing body (BWB) concept for significant improvement in both fuel efficiency and noise reduction and addresses the considerable challenges raised for control engineers because of characteristics like open-loop instability, large flexible structure, and slow control surfaces. This text describes state-of-the-art and novel modeling and control design approaches for the BWB aircraft under consideration. The expert contributors demonstrate how exceptional robust control performance can be achieved despite such stringent design constraints as guaranteed handling qualities, reduced vibration, and the minimization of the aircraft’s structural loads during maneuvers and caused by turbulence. As a result, this innovative approach allows the building of even lighter aircraft structures, and thus results in considerable efficiency improvements per passenger kilometer. The treatment of this large, complex, parameter-dependent industrial control problem highlights relevant design issues and provides a relevant case study for modeling and control engineers in many adjacent disciplines and applications. 2015-08-21T06:57:30Z 2015-08-21T06:57:30Z 2015 Book 978-3-319-10792-9 https://scholar.dlu.edu.vn/thuvienso/handle/DLU123456789/57710 en application/pdf Springer |
| institution |
Thư viện Trường Đại học Đà Lạt |
| collection |
Thư viện số |
| language |
English |
| topic |
Engineering Computer simulation Wings Airplanes Mathematical models |
| spellingShingle |
Engineering Computer simulation Wings Airplanes Mathematical models Kozek, Martin Schirrer, Alexander Modeling and Control for a Blended Wing Body Aircraft: A Case Study |
| description |
This book demonstrates the potential of the blended wing body (BWB) concept for significant improvement in both fuel efficiency and noise reduction and addresses the considerable challenges raised for control engineers because of characteristics like open-loop instability, large flexible structure, and slow control surfaces. This text describes state-of-the-art and novel modeling and control design approaches for the BWB aircraft under consideration. The expert contributors demonstrate how exceptional robust control performance can be achieved despite such stringent design constraints as guaranteed handling qualities, reduced vibration, and the minimization of the aircraft’s structural loads during maneuvers and caused by turbulence. As a result, this innovative approach allows the building of even lighter aircraft structures, and thus results in considerable efficiency improvements per passenger kilometer. The treatment of this large, complex, parameter-dependent industrial control problem highlights relevant design issues and provides a relevant case study for modeling and control engineers in many adjacent disciplines and applications. |
| format |
Book |
| author |
Kozek, Martin Schirrer, Alexander |
| author_facet |
Kozek, Martin Schirrer, Alexander |
| author_sort |
Kozek, Martin |
| title |
Modeling and Control for a Blended Wing Body Aircraft:
A Case Study |
| title_short |
Modeling and Control for a Blended Wing Body Aircraft:
A Case Study |
| title_full |
Modeling and Control for a Blended Wing Body Aircraft:
A Case Study |
| title_fullStr |
Modeling and Control for a Blended Wing Body Aircraft:
A Case Study |
| title_full_unstemmed |
Modeling and Control for a Blended Wing Body Aircraft:
A Case Study |
| title_sort |
modeling and control for a blended wing body aircraft:
a case study |
| publisher |
Springer |
| publishDate |
2015 |
| url |
https://scholar.dlu.edu.vn/thuvienso/handle/DLU123456789/57710 |
| _version_ |
1782550156029198336 |