Flight Stability and Automatic Control | Date: 05 May 2011, 15:36
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This edition of this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Product Description
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.
From the Publisher
Many more worked examples and end-of-chapter problems, some of which require computer solutions, are integrated throughout the text.
An expanded section on automatic control theory and its application to flight control system design is now included.
Chapters covering the topics of static stability, flight control, aircraft dynamics, and flying qualities have been improved.
Problems that require the use of a computer are now clearly identified.
Material is introduced by way of simple exercises so students can see how the design process is applied without a lot of mathematical complexity.
Interesting historical notes are presented throughout the text.
The text provides an integrated treatment of aircraft stability, flight control, and autopilot design.
Reviews
By DCop (Houston, Texas United States):
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.
By Keiichi Ito (Japan):
The best aspect of this book is the simplicity in the exposition of ideas and concepts while giving more than enough information for an introductory book. Fully worked out examples are frequent throughout the chapters and helps even further in getting good grasp of new materials. If the reader has taken introductory courses in Vibration and/or Feedback Control, the book should be an easy read. The book is roughly divided into two parts: The flight dynamics part and control part. In the flight dynamics part, the explanation smoothly leads the reader from equation of motion to the concept of stability derivatives and how they relate to dynamic stability. The derivatives are very well explained and then summarized in tables for a quick reference. In the control part, the author starts from the classic linear feed back control and proceeds to the modern state space method and introduces optimal control design using linear quadratic regulator. The control part is an amazing time saver. I have never seen a more efficient introduction to optimal control as applied to aircraft dynamics. If the reader wants a full fledged treatment of optimal control of aircraft, the materials presented here are far from enough, but as an introductory book, this is an excellent exposition that lets the reader get to pace quickly and have straight forward perspective on the subject. Although there were some blatant typos, it is an excellent work and I highly recommend the book.
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