Selected Advanced Aerodynamics and Active Controls Technology Concepts Development on a Derivative B-747 Aircraft

Selected Advanced Aerodynamics and Active Controls Technology Concepts Development on a Derivative B-747 Aircraft PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 62

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Selected Advanced Aerodynamics and Active Controls Technology Concepts Development on a Derivative B-747

Selected Advanced Aerodynamics and Active Controls Technology Concepts Development on a Derivative B-747 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 378

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

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NASA Reference Publication

NASA Reference Publication PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 770

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 320

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Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1980

Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1980 PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 252

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Scientific and Technical Information Output of the Langley Research Center for Calendar Year ...

Scientific and Technical Information Output of the Langley Research Center for Calendar Year ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 252

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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 84

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Modeling and Control for a Blended Wing Body Aircraft

Modeling and Control for a Blended Wing Body Aircraft PDF Author: Martin Kozek
Publisher: Springer
ISBN: 3319107925
Category : Technology & Engineering
Languages : en
Pages : 308

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Book Description
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.

Flight Dynamics

Flight Dynamics PDF Author: Robert F. Stengel
Publisher: Princeton University Press
ISBN: 1400866812
Category : Science
Languages : en
Pages : 864

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Book Description
Flight Dynamics takes a new approach to the science and mathematics of aircraft flight, unifying principles of aeronautics with contemporary systems analysis. While presenting traditional material that is critical to understanding aircraft motions, it does so in the context of modern computational tools and multivariable methods. Robert Stengel devotes particular attention to models and techniques that are appropriate for analysis, simulation, evaluation of flying qualities, and control system design. He establishes bridges to classical analysis and results, and explores new territory that was treated only inferentially in earlier books. This book combines a highly accessible style of presentation with contents that will appeal to graduate students and to professionals already familiar with basic flight dynamics. Dynamic analysis has changed dramatically in recent decades, with the introduction of powerful personal computers and scientific programming languages. Analysis programs have become so pervasive that it can be assumed that all students and practicing engineers working on aircraft flight dynamics have access to them. Therefore, this book presents the principles, derivations, and equations of flight dynamics with frequent reference to MATLAB functions and examples. By using common notation and not assuming a strong background in aeronautics, Flight Dynamics will engage a wide variety of readers. Introductions to aerodynamics, propulsion, structures, flying qualities, flight control, and the atmospheric and gravitational environment accompany the development of the aircraft's dynamic equations.