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Robust Rotorcraft Flight Control by Gorder Peter (20 results)
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Seller: Ria Christie Collections, Uxbridge, United Kingdom
Seller rating 5 out of 5 stars
Condition: New. In.
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
Condition: New.
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Published by Creative Media Partners, LLC Mai 2025, 2025
ISBN 10: 1025159721 ISBN 13: 9781025159720
Language: English
Taschenbuch. Condition: Neu. Neuware.
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Published by Creative Media Partners, LLC Mai 2025, 2025
ISBN 10: 1025155173 ISBN 13: 9781025155173
Language: English
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 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.
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
Condition: As New. Unread book in perfect condition.
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Published by Creative Media Partners, LLC Mär 2013, 2013
ISBN 10: 1288916132 ISBN 13: 9781288916139
Language: English
Taschenbuch. 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 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.
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Paperback. Condition: Like New. Like New. book.
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Condition: As New. Unread book in perfect condition.
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Published by Creative Media Partners, LLC, 2025
ISBN 10: 1025159721 ISBN 13: 9781025159720
Language: English
PAP. Condition: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Published by Creative Media Partners, LLC, 2025
ISBN 10: 1025159721 ISBN 13: 9781025159720
Language: English
Seller: PBShop.store UK, Fairford, GLOS, United Kingdom
Seller rating 5 out of 5 stars
PAP. Condition: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Published by Creative Media Partners, LLC, 2025
ISBN 10: 1025155173 ISBN 13: 9781025155173
Language: English
HRD. Condition: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
-
A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Published by Creative Media Partners, LLC, 2025
ISBN 10: 1025155173 ISBN 13: 9781025155173
Language: English
Seller: PBShop.store UK, Fairford, GLOS, United Kingdom
Seller rating 5 out of 5 stars
HRD. Condition: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
-
PAP. Condition: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
-
A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Seller: PBShop.store UK, Fairford, GLOS, United Kingdom
Seller rating 5 out of 5 stars
PAP. Condition: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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Condition: New. Print on Demand.
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Condition: New. PRINT ON DEMAND.
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A Robust Rotorcraft Flight Control System Design Methodology Utilizing Quantitative Feedback Theory
Seller: THE SAINT BOOKSTORE, Southport, United Kingdom
Seller rating 5 out of 5 stars
Paperback / softback. Condition: New. This item is printed on demand. New copy - Usually dispatched within 5-9 working days 511.
