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This book demonstrates that eigenstructure control theory can be easily adapted and infused into aircraft industry's stringent design practices. Thus practicing flight control engineers will find it useful to explore the use of the new design concepts discussed in the book. The book, being interdisciplinary in nature, encompassing control theory and flight dynamics should be of interest to both control and aeronautical engineers. In particular control researchers may find it interesting to explore extension of the theory to new multivariable control problem formulations. Finally the book should be of interest to graduate/doctoral students, keen on learning a multivariable control technique that is useful to design practical control systems.
- Sales Rank: #3015167 in Books
- Published on: 2011-01-16
- Original language: English
- Number of items: 1
- Dimensions: 9.00" h x 6.00" w x .75" l, 1.30 pounds
- Binding: Hardcover
- 250 pages
About the Author
Dr Srinathkumar holds BE (Bangalore University, India, 1960), MS (University of Hawaii, 1973) and PhD (Oklahoma State University, 1976) degrees in electrical engineering. He has spent all his professional life as a scientist at the National Aerospace Laboratories (NAL), India (1961-71, 1978-2000). During 1993-2000 he served as Head of the Flight Mechanics and Control Division at NAL. He has spent two sabbaticals at NASA Langley Research Center, Virginia, USA, under the USA National Research Council Fellowship program. During his tenures at NASA, he was involved in pioneering application of eigenstructure control techniques for aircraft flight control (1976-78) plus the design and successful experimental demonstration of active flutter control of a flexible wing (1987-89). His current interest continues to be in the application of modern control techniques to aircraft and rotorcraft handling-quality design problems.
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Eigenstructure assignment is a effective design method for helicopter control ...
By Junfeng Yang
Eigenstructure assignment is a effective design method for helicopter control. particularly this method allows us design close-loop handling quality in a straightforward maner although you have to check the stability margin which is not inherently guaranteed by the method. Decoupling is a major course in helicopter control, both feedback decoupling and feed-forward decoupling are discussed in this book.
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