000			04336nam a22003975i 4500
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008			141027s2015 gw | s |||| 0|eng d
020			_a9783319107929
024	7		_a10.1007/978-3-319-10792-9 _2doi
040			_bspa _dES-MaUEC
050		4	_aTL672 _b2015 EB
245	1	0	_aModeling and Control for a Blended Wing Body Aircraft _bA Case Study _cedited by Martin Kozek, Alexander Schirrer.
264		1	_aCham _bSpringer International Publishing _c2015
300			_a1 recurso en línea (XIV, 301 páginas 200 ilustraciones, 158 ilustraciones a color.)
336			_2rdacontent _aTexto (visual) _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
490	0		_aAdvances in Industrial Control, _x1430-9491
490	0		_aEngineering (Springer-11647)
505	0		_aOverview and Motivation -- Conceptual Design -- Numerical Simulation Model -- Reduced-order Modeling -- Control Goals -- Feedback Control Designs -- Feed-Forward Control Designs -- Validation, Discussion and Outlook.
520	3		_aThis 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.
988			_aEBSPRINGER_2018
650		7	_aAviones _2embne _9138154
700	1		_aKozek, Martin. _eeditor literario _4edt _4http://id.loc.gov/vocabulary/relators/edt _0http://id.loc.gov/authorities/names/no2015010314 _1http://viaf.org/viaf/313500296/
700	1		_aSchirrer, Alexander. _eeditor literario _4edt _4http://id.loc.gov/vocabulary/relators/edt _0http://id.loc.gov/authorities/names/no2015010366 _1http://viaf.org/viaf/313500340/
776	0	8	_iEdición impresa: _z9783319107936
776	0	8	_iEdición impresa: _z9783319107912
776	0	8	_iEdición impresa: _z9783319343402
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-319-10792-9 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
998			_b03/2019 _dz _zSI _eIG