My Library

University LibraryCatalogue

Limit search to items available for borrowing or consultation
Result Page: Previous Next
Can't find that book? Try BONUS+
Look for full text

Search Discovery

Search CARM Centre Catalogue

Search Trove

Add record to RefWorks

Cover Art

Title Modeling and control for a blended wing body aircraft : a case study / Martin Kozek, Alexander Schirrer, editor.

Published Cham : Springer, [2014]


Location Call No. Status
Physical description 1 online resource (xiv, 301 pages) : illustrations (some color).
Series Advances in Industrial Control, 1430-9491
Advances in industrial control.
Springer English/International eBooks 2015 - Full Set
Notes Includes index.
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.
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 author Kozek, Martin, editor.
Schirrer, Alexander, editor.
SpringerLink issuing body.
Subject Airplanes -- Wings -- Mathematical models.
Airplanes -- Wings -- Computer simulation.
Electronic books.
ISBN 9783319107929