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

Author: Martin Kozek; Alexander Schirrer
Publisher: Cham : Springer, [2014] ©2015
Series: Advances in industrial control.
Edition/Format:   eBook : Document : EnglishView all editions and formats
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  Read more...
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Genre/Form: Electronic books
Additional Physical Format: Print version:
Kozek, Martin.
Modeling and Control for a Blended Wing Body Aircraft : A Case Study.
Cham : Springer International Publishing, ©2014
Material Type: Document, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: Martin Kozek; Alexander Schirrer
ISBN: 9783319107929 3319107925 3319107917 9783319107912
OCLC Number: 894509095
Notes: Includes index.
Description: 1 online resource (xiv, 301 pages) : illustrations (some color).
Contents: Series Editors' Foreword; Foreword; Preface; Contents; Acronyms; 1 Overview and Motivation; 1.1 Greening Air Transport; 1.2 The ACARE 2020 Vision; 1.3 The ACFA 2020 Project; 1.3.1 Overview and Deliverables; 1.3.2 Main Deliverable 1: Solutions for Active MIMO Control for BWB-Type Aircraft; 1.3.3 Main Deliverable 2: ACFA 2020 Aircraft Configuration (Predesign of an Ultra-Efficient 450 Passenger BWB-Type Aircraft); 1.3.4 Consortium and Figures; 1.4 Recent Developments in New Aircraft Configurations; 1.5 Recent European Research Activity on the BWB. 1.6 Recent Developments in Aircraft Conceptual Design Modeling and Simulation Methods1.6.1 Overall Design; 1.6.2 Propulsion; 1.6.3 Aerodynamics; 1.7 Flight Control Design; 1.7.1 General Goals; 1.7.2 Loads Alleviation; 1.7.3 Handling Qualities; 1.7.4 ACFA 2020 Control Design Challenges; References; Part IAircraft Design and Modeling; 2 Conceptual Design; 2.1 Introduction; 2.2 Requirements and Mission Definition; 2.2.1 Operational Performance; 2.2.2 Passenger Cabin and Landing Gear Definition; 2.2.3 Lifting Surface Requirements; 2.2.4 Fuel Capacity; 2.3 Design Process; 2.3.1 Structural Weight. 2.3.2 Aerodynamics and Control2.3.3 Engine; 2.4 Multidisciplinary Design Optimization in the Structural Design Process; 2.5 Configuration Selection; 2.5.1 Results; 2.5.2 Aircraft Selection; 2.5.3 Conclusion and Outlook; References; 3 Numerical Simulation Model; 3.1 Introduction; 3.2 Preliminary Structural Modeling; 3.2.1 Testing FEM Structure; 3.3 ACFA BWB Structural Modeling; 3.3.1 Overview on Structural Modeling; 3.3.2 ACFA Geometry; 3.3.3 Material Properties; 3.3.4 Load Cases; 3.3.5 Structural Concepts; 3.3.6 Nonstructural Masses; 3.3.7 Finite Element Calculation; 3.3.8 Mass Estimation. 3.3.9 Conclusion3.4 Aerodynamic Modeling; 3.4.1 Numerical Methods; 3.4.2 Steady Simulation Results; 3.4.3 Unsteady Simulation Results; 3.4.4 Conclusions; 3.5 Integrated Flight Dynamics and Aeroelastic Modeling; 3.5.1 Structural Dynamics; 3.5.2 Aerodynamic Database; 3.5.3 Modification of GAF by Higher-Order Analysis Results; 3.5.4 Approximation of Aerodynamic Forces in the Laplace Domain; 3.5.5 Structural Outputs; 3.5.6 Equations of Motion; 3.5.7 State-Space Model; References; 4 Reduced-Order Modeling; 4.1 Model Order Reduction. 4.1.1 General Process of Generation of Parameterized Reduced-Order Models for Control Design4.1.2 Modal Reduction of Full Structural Model; 4.1.3 Reduction of Complete Aeroelastic Model; 4.1.4 Balanced Reduction; 4.1.5 Parameterization of Aircraft Models; 4.1.6 Spline Interpolation; 4.1.7 Conclusion; 4.2 Linear Fractional Representation of Parametrized Models; 4.2.1 Linear Fractional Transformation; 4.2.2 Process of LFR Modeling; 4.2.3 Generation of LFRs for the ACFA 2020 BWB Aircraft; 4.2.4 Summary; References; Part IIControl Design; 5 Control Goals; 5.1 Analysis of Aircraft Dynamics.
Series Title: Advances in industrial control.
Responsibility: Martin Kozek, Alexander Schirrer, editor.

Abstract:

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.

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