Anbieter: HPB-Emerald, Dallas, TX, USA
hardcover. Zustand: Very Good. Connecting readers with great books since 1972! Used books may not include companion materials, and may have some shelf wear or limited writing. We ship orders daily and Customer Service is our top priority!
Anbieter: GreatBookPrices, Columbia, MD, USA
Zustand: New.
Anbieter: GreatBookPrices, Columbia, MD, USA
Zustand: As New. Unread book in perfect condition.
Anbieter: GreatBookPrices, Columbia, MD, USA
Zustand: As New. Unread book in perfect condition.
Anbieter: GreatBookPrices, Columbia, MD, USA
Zustand: New.
Anbieter: Anybook.com, Lincoln, Vereinigtes Königreich
EUR 24,29
Anzahl: 1 verfügbar
In den WarenkorbZustand: Good. Volume 16. This is an ex-library book and may have the usual library/used-book markings inside.This book has hardback covers. In good all round condition. Please note the Image in this listing is a stock photo and may not match the covers of the actual item,650grams, ISBN:9780824748692.
Anbieter: GreatBookPricesUK, Woodford Green, Vereinigtes Königreich
EUR 28,23
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In den WarenkorbZustand: New.
Anbieter: GreatBookPricesUK, Woodford Green, Vereinigtes Königreich
EUR 32,83
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In den WarenkorbZustand: As New. Unread book in perfect condition.
Anbieter: GreatBookPricesUK, Woodford Green, Vereinigtes Königreich
EUR 38,80
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In den WarenkorbZustand: New.
Anbieter: GreatBookPricesUK, Woodford Green, Vereinigtes Königreich
EUR 42,85
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In den WarenkorbZustand: As New. Unread book in perfect condition.
Sprache: Englisch
Verlag: Springer-Verlag, Berlin New York Tokyo, 1985
ISBN 10: 3540156100 ISBN 13: 9783540156109
Anbieter: Don's Book Store, Albuquerque, NM, USA
Hard Back. Zustand: Near Fine. Zustand des Schutzumschlags: No Dust Jacket. Bell, C. (illustrator). 594 Pages Indexed. Previous owner's name label and seal on front endpaper. Illustrated with 152 figures. No defects noted. Interior text pages are flawless. The first German edition of this book appeared in 1972, and in Polish translation in 1976. It covered the analysis and synthesis of sampled-data systems. The second German edition of 1983 extended the scope to design, in particular design for robustness of control system properties with respect to uncertainty of plant parameters. This book is a revised translation of the second German edition. The revisions concern primarily a new treatment of the finite effect sequences and the use of nice numerical properties of Hessenberg forms. Contents in Nine Chapters: Introduction, Continuous Systems, Modelling and Analysis of Sampled-Data Systems, Controllability Choice of Sampling POeriod and Pole Assignment, Observability and Observers, Control Loop Synthesis, Geometric Stability Investigation and JPole Region Assignment, Design of Robust Control Systems, and Multivariable Systems.
Anbieter: GreatBookPrices, Columbia, MD, USA
Zustand: New.
Zustand: New. Third edition Includes bibliographical references and index.
Anbieter: GreatBookPrices, Columbia, MD, USA
Zustand: As New. Unread book in perfect condition.
ISBN 13: 9798278536895
Anbieter: GreatBookPrices, Columbia, MD, USA
Zustand: As New. Unread book in perfect condition.
EUR 59,26
Anzahl: 1 verfügbar
In den WarenkorbZustand: New.
ISBN 13: 9798278536895
Anbieter: GreatBookPrices, Columbia, MD, USA
Zustand: New.
Zustand: New.
Anbieter: Zubal-Books, Since 1961, Cleveland, OH, USA
Zustand: Good. 596 pp., hardcover, ex library else text clean and binding tight. - If you are reading this, this item is actually (physically) in our stock and ready for shipment once ordered. We are not bookjackers. Buyer is responsible for any additional duties, taxes, or fees required by recipient's country.
Anbieter: Studibuch, Stuttgart, Deutschland
hardcover. Zustand: Sehr gut. 313 Seiten; 9780824797393.2 Gewicht in Gramm: 1.
Sprache: Englisch
Verlag: Marcel Dekker Inc, Monticello, New York, U.S.A., 2003
ISBN 10: 0824748697 ISBN 13: 9780824748692
Anbieter: Reader's Corner, Inc., Raleigh, NC, USA
Hardcover. Zustand: New. No Jacket. Second Edition, Revised and Expanded. This is a new hardcover copy of the second edition, slick light yellow binding.
Anbieter: THE SAINT BOOKSTORE, Southport, Vereinigtes Königreich
EUR 62,56
Anzahl: 1 verfügbar
In den WarenkorbOther book format. Zustand: New. New copy - Usually dispatched within 4 working days.
Anbieter: GreatBookPricesUK, Woodford Green, Vereinigtes Königreich
EUR 62,54
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In den WarenkorbZustand: New.
Anbieter: GreatBookPricesUK, Woodford Green, Vereinigtes Königreich
EUR 65,18
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In den WarenkorbZustand: As New. Unread book in perfect condition.
EUR 74,46
Anzahl: Mehr als 20 verfügbar
In den WarenkorbZustand: New. In.
Sprache: Englisch
Verlag: LAP Lambert Academic Publishing, 2019
ISBN 10: 6200101787 ISBN 13: 9786200101785
Anbieter: Books Puddle, New York, NY, USA
Zustand: New.
Verlag: Marcel Dekker, 1996
Anbieter: Librodifaccia, Alessandria, AL, Italien
Zustand: Buone. inglese Condizioni dell'esterno: copertina leggermente logorata e macchiata Condizioni dell'interno: Ottime.
Sprache: Englisch
Verlag: Creative Media Partners, LLC Mai 2025, 2025
ISBN 10: 1025159721 ISBN 13: 9781025159720
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Taschenbuch. Zustand: Neu. Neuware.
Anbieter: Revaluation Books, Exeter, Vereinigtes Königreich
EUR 96,32
Anzahl: 2 verfügbar
In den WarenkorbPaperback. Zustand: Brand New. 3rd edition. 320 pages. 9.18x6.12x9.21 inches. In Stock.
Sprache: Englisch
Verlag: Creative Media Partners, LLC Mai 2025, 2025
ISBN 10: 1025155173 ISBN 13: 9781025155173
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Buch. Zustand: Neu. Neuware - Rotorcraft flight control systems present design challenges which often exceed those associated with fixed-wing aircraft. First, large variations in the response characteristics of the rotorcraft result from the wide range of airspeeds of typical operation (hover to over 100 kts). Second, the assumption of vehicle rigidity often employed in the design of fixed-wing flight control systems is rarely justified in rotorcraft where rotor degrees of freedom can have a significant impact on the system performance and stability. This research was intended to develop a methodology for the design of robust rotorcraft flight control systems. Quantitative Feedback Theory (QFT) was chosen as the basis for the investigation. Quantitative Feedback Theory is a technique which accounts for variability in the dynamic response of the controlled element in the design robust control systems. It was developed to address a Multiple-Input Single-Output (MISO) design problem, and utilizes two degrees of freedom to satisfy the design criteria. Two techniques were examined for extending the QFT MISO technique to the design of a Multiple-Input-Multiple-Output (MIMO) flight control system (FCS) for a UH-60 Black Hawk Helicopter. In the first, a set of MISO systems, mathematically equivalent to the MIMO system, was determined. QFT was applied to each member of the set simultaneously. In the second, the same set of equivalent MISO systems were analyzed sequentially, with closed loop response information from each loop utilized in subsequent MISO designs. The results of each technique were compared, and the advantages of the second, termed Sequential Loop Closure, were clearly evident.