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Flight Stability and Automatic Control, by Robert Nelson
Free Ebook Flight Stability and Automatic Control, by Robert Nelson
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The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
- Sales Rank: #707159 in Books
- Published on: 1997-10-01
- Original language: English
- Number of items: 1
- Dimensions: 9.50" h x 1.00" w x 6.50" l, 1.66 pounds
- Binding: Hardcover
- 456 pages
Most helpful customer reviews
6 of 7 people found the following review helpful.
Good Fundamentals Book by a Talented Writer
By dcoppo.
This is an excellent book for the modern fundamentals of aircraft control design. Most subjects are clearly treated with just the right amount of illustrations and examples. The author makes good effort of explaining procedures without resorting to function calls from some software package. The last of the book devotes relatively little space to modern control theory. I would hope this talented writer would create something more advanced in the future that would expand on his treatment of the state observer and the use of the cost function.
10 of 10 people found the following review helpful.
Sloppy
By Student of Prandtl
If this is a required text, as it was for me then buy it. The information isnt bad, and gives a good coverage of the subject, but the errata list I receieved from my professor spanned at least 20 pages, front and back. You'll learn controls with the right professor, but expect the book to confuse you with changing subscripts, even changing values in example problems. For example, the area of a wing in one example problem is listed as 945 ft^2 and yet the problem solves using the area of 965 ft^2. Equations will be missing subscripts entirely, or duplicate them. For example, in one end of the chapter section of problems, the 2-D coefficient of lift for the tail is listed twice as opposed to giving you one value for the tail, and another for the wing as they should have. Expect to make assumptions like they have never been made before either. So much will not be given to you, it will be up to you to decide what value is reasonable that youll use. Good luck to you if this is a required text.
12 of 13 people found the following review helpful.
A lot of info on aircraft control in a small textbook.
By M1B2Bland@aol.com
I found this textbook to include a large amount of concisely presented material on all aspects of aircraft stability and control and feedback control system design. It covers everything from the atmosphere, to development of forces and moments and equations of motion, to estimation of stability derivatives, analysis of dynamics and modes of motion, and handy reduced degrees of freedom. It also includes many examples of designing autopilots and stability augmentation systems. I really liked the examples which included both classical and state variable methods. Each chapter also has several interesting example problems. I would recommend this text for anyone in the field of aircraft or missile flight controls. The only dissappointing aspect of the text is what I consider an excessive number of typographical errors. I would caution anyone not to use the equations or formulas without first checking the derivation. The derivations are clear and concise enough that the reader should be able to find these errors.
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