The Resource Modeling and Control for a Blended Wing Body Aircraft : A Case Study, edited by Martin Kozek, Alexander Schirrer, (electronic resource)

Modeling and Control for a Blended Wing Body Aircraft : A Case Study, edited by Martin Kozek, Alexander Schirrer, (electronic resource)

Label
Modeling and Control for a Blended Wing Body Aircraft : A Case Study
Title
Modeling and Control for a Blended Wing Body Aircraft
Title remainder
A Case Study
Statement of responsibility
edited by Martin Kozek, Alexander Schirrer
Contributor
Editor
Editor
Subject
Language
  • eng
  • eng
Summary
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. Modeling and Control for a Blended Wing Body Aircraft presents research results in numeric modeling and control design for a large, flexible, civil BWB aircraft in the pre-design stage as developed within the EU FP7 research project ACFA 2020. It is a useful resource for aerospace and control engineers as it shows the complete BWB aircraft modeling and control design process, carried out with the most recent tools and techniques available. presents research results in numeric modeling and control design for a large, flexible, civil BWB aircraft in the pre-design stage as developed within the EU FP7 research project ACFA 2020. It is a useful resource for aerospace and control engineers as it shows the complete BWB aircraft modeling and control design process, carried out with the most recent tools and techniques available. Advances in Industrial Control aims to report and encourage the transfer of technology in control engineering. The rapid development of control technology has an impact on all areas of the control discipline. The series offers an opportunity for researchers to present an extended exposition of new work in all aspects of industrial control
Member of
Dewey number
  • 003.3
  • 620
  • 629.1
  • 629.8
http://bibfra.me/vocab/relation/httpidlocgovvocabularyrelatorsedt
  • 3gjkasgjgXQ
  • To7vkAtgKYo
Language note
English
LC call number
TJ212-225
Literary form
non fiction
Nature of contents
dictionaries
http://library.link/vocab/relatedWorkOrContributorName
  • Kozek, Martin.
  • Schirrer, Alexander.
Series statement
Advances in Industrial Control,
http://library.link/vocab/subjectName
  • Astronautics
  • Computer simulation
  • Control and Systems Theory
  • Aerospace Technology and Astronautics
  • Simulation and Modeling
Label
Modeling and Control for a Blended Wing Body Aircraft : A Case Study, edited by Martin Kozek, Alexander Schirrer, (electronic resource)
Instantiates
Publication
Note
Description based upon print version of record
Bibliography note
Includes bibliographical references and index
Carrier category
online resource
Carrier category code
  • cr
Content category
text
Content type code
  • txt
Contents
Overview and Motivation -- Conceptual Design -- Numerical Simulation Model -- Reduced-order Modeling -- Control Goals -- Feedback Control Designs -- Feed-Forward Control Designs -- Validation, Discussion and Outlook
Dimensions
unknown
Edition
1st ed. 2015.
Extent
1 online resource (308 p.)
Form of item
online
Isbn
9783319107929
Media category
computer
Media type code
  • c
Other control number
10.1007/978-3-319-10792-9
Specific material designation
remote
System control number
  • (CKB)3710000000268451
  • (EBL)1967690
  • (OCoLC)894509095
  • (SSID)ssj0001372491
  • (PQKBManifestationID)11787117
  • (PQKBTitleCode)TC0001372491
  • (PQKBWorkID)11304580
  • (PQKB)10057358
  • (DE-He213)978-3-319-10792-9
  • (MiAaPQ)EBC1967690
  • (EXLCZ)993710000000268451
Label
Modeling and Control for a Blended Wing Body Aircraft : A Case Study, edited by Martin Kozek, Alexander Schirrer, (electronic resource)
Publication
Note
Description based upon print version of record
Bibliography note
Includes bibliographical references and index
Carrier category
online resource
Carrier category code
  • cr
Content category
text
Content type code
  • txt
Contents
Overview and Motivation -- Conceptual Design -- Numerical Simulation Model -- Reduced-order Modeling -- Control Goals -- Feedback Control Designs -- Feed-Forward Control Designs -- Validation, Discussion and Outlook
Dimensions
unknown
Edition
1st ed. 2015.
Extent
1 online resource (308 p.)
Form of item
online
Isbn
9783319107929
Media category
computer
Media type code
  • c
Other control number
10.1007/978-3-319-10792-9
Specific material designation
remote
System control number
  • (CKB)3710000000268451
  • (EBL)1967690
  • (OCoLC)894509095
  • (SSID)ssj0001372491
  • (PQKBManifestationID)11787117
  • (PQKBTitleCode)TC0001372491
  • (PQKBWorkID)11304580
  • (PQKB)10057358
  • (DE-He213)978-3-319-10792-9
  • (MiAaPQ)EBC1967690
  • (EXLCZ)993710000000268451

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