Robust Control System Design (108 results)
- Hardcover
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hardcover. Condition: 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.
A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
National Aeronautics And Space Admini, National Aeronautics And Space Admini
- Softcover
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
National Aeronautics And Space Admini, National Aeronautics And Space Admini
- Softcover
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
National Aeronautics And Space Admini, National Aeronautics And Space Admini
- Hardcover
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
National Aeronautics And Space Admini, National Aeronautics And Space Admini
- Hardcover
Seller: GreatBookPrices, Columbia, MD, U.S.A.GreatBookPrices
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- Hardcover
Seller: Anybook.com, Lincoln, United KingdomAnybook.com
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Condition: 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.
A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
National Aeronautics And Space Admini, National Aeronautics And Space Admini
- Softcover
Seller: GreatBookPricesUK, Woodford Green, United KingdomGreatBookPricesUK
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
National Aeronautics And Space Admini, National Aeronautics And Space Admini
- Softcover
Seller: GreatBookPricesUK, Woodford Green, United KingdomGreatBookPricesUK
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
National Aeronautics And Space Admini, National Aeronautics And Space Admini
- Hardcover
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
National Aeronautics And Space Admini, National Aeronautics And Space Admini
- Hardcover
Seller: GreatBookPricesUK, Woodford Green, United KingdomGreatBookPricesUK
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- Hardcover
Seller: Don's Book Store, Albuquerque, NM, U.S.A.Don's Book Store
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Hard Back. Condition: Near Fine. No Dust Jacket. 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 synth…esis 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. Bell, C. (illustrator).
- Softcover
Seller: GreatBookPrices, Columbia, MD, U.S.A.GreatBookPrices
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- Softcover
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Condition: New. Third edition Includes bibliographical references and index.
- Softcover
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- Softcover
Seller: Majestic Books, Hounslow, , United KingdomMajestic Books
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- Softcover
Seller: Biblios, frankfurt am main, HESSE, GermanyBiblios
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- Hardcover
Seller: Studibuch, Stuttgart, GermanyStudibuch
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hardcover. Condition: Sehr gut. 313 Seiten; 9780824797393.2 Gewicht in Gramm: 1.
Language: English
Published by Marcel Dekker Inc, Monticello, New York, U.S.A. 2003
- Hardcover
Seller: Reader's Corner, Inc., Raleigh, NC, U.S.A.Reader's Corner, Inc.
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Hardcover. Condition: New. No Jacket. Second Edition, Revised and Expanded. This is a new hardcover copy of the second edition, slick light yellow binding.
- Hardcover
Seller: Zubal-Books, Since 1961, Cleveland, OH, U.S.A.Zubal-Books, Since 1961
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Condition: 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.
- Softcover
Seller: THE SAINT BOOKSTORE, Southport, , United KingdomTHE SAINT BOOKSTORE
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- Softcover
Seller: GreatBookPricesUK, Woodford Green, United KingdomGreatBookPricesUK
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- Softcover
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- Softcover
Seller: Ria Christie Collections, Uxbridge, United KingdomRia Christie Collections
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- Softcover
Seller: Books Puddle, New York, NY, U.S.A.Books Puddle
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Published by Marcel Dekker 1996
Seller: Librodifaccia, Alessandria, AL, ItalyLibrodifaccia
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Condition: Buone. inglese Condizioni dell'esterno: copertina leggermente logorata e macchiata Condizioni dell'interno: Ottime.
- Softcover
Seller: AHA-BUCH GmbH, Einbeck, GermanyAHA-BUCH GmbH
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Taschenbuch. Condition: Neu. Neuware.
- Softcover
Seller: Revaluation Books, Exeter, , United KingdomRevaluation Books
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Paperback. Condition: Brand New. 3rd edition. 320 pages. 9.18x6.12x9.21 inches. In Stock.
- Hardcover
Seller: AHA-BUCH GmbH, Einbeck, GermanyAHA-BUCH GmbH
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Buch. Condition: 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 assu…mption 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.
