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Performance, Stability, Dynamics, and Control of Airplanes, Third Edition (AIAA Education Series), by Bandu N. Pamadi
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A comprehensive and integrated exposure to airplane performance, stability, dynamics, and flight control featuring basic aerodynamics, dynamics, and linear control systems. Chapters 1 through 3 present basic principles of aerodynamics, aircraft performance, and static equilibrium and control in steady flight. Chapter 4 deals with aircraft dynamics and decoupled equations for longitudinal and lateral motion, and it introduces the concept of stability derivatives. Chapter 5 discusses design of stability augmentation systems and autopilots. Chapter 6 discusses aircraft response and methods of closed-loop control of aircraft, while Chapters 7 and 8 discuss problems of inertial coupling, aircraft spin, and high angle of attack. The third edition features updates throughout along with a new chapter 9 on stability, control issues, and challenges of unmanned aerial vehicles.
- Sales Rank: #1432818 in Books
- Published on: 2015-08-01
- Original language: English
- Number of items: 1
- Dimensions: 9.30" h x 1.90" w x 6.40" l, .0 pounds
- Binding: Hardcover
- 708 pages
About the Author
Bandu N. Pamadi is a senior aerospace engineer at NASA Langley Research Center. He was a German academic exchange fellow at the University of Stuttgart from 1973-1975 and an NRC-NASA Research Associate at NASA Langley from 1981-1983. Before returning to NASA Langley in 1986, he was a professor of aeronautical engineering at the Indian Institute of Technology, Bombay. He holds degrees from Karnatak University, the Indian Institute of Science, Bangalore, and the Indian Institute of Technology, Bombay.
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