Modeling and control for a blended wing body aircraft : a case study /

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Bibliographic Details
Imprint:Cham : Springer, [2014]
©2015
Description:1 online resource (xiv, 301 pages) : illustrations (some color).
Language:English
Series:Advances in Industrial Control, 1430-9491
Advances in industrial control.
Subject:
Format: E-Resource Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/11089119
Hidden Bibliographic Details
Other authors / contributors:Kozek, Martin, editor.
Schirrer, Alexander, editor.
ISBN:9783319107929
3319107925
9783319107912
Notes:Includes index.
Online resource; title from PDF title page (SpringerLink, viewed November 24, 2014).
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 guar.
Other form:Print version: Kozek, Martin. Modeling and Control for a Blended Wing Body Aircraft : A Case Study. Cham : Springer International Publishing, ©2014 9783319107912