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Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control (Aiaa Education
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This textbook is based on a 15-year successful approach to teaching aircraft flight mechanics at the U.S. Air Force Academy. It explains all the concepts and derivations of equations for aircraft flight mechanics. It covers; aircraft performance, static stability, aircraft dynamics stability, and feedback control. The chapters present real world applications and contain problems. Each year the Academy's students are placed with industry, NASA, and Air Force labs and test organizations, and the student reviews are outstanding, illustrating the quality of the author's approach.
- Sales Rank: #763327 in Books
- Brand: Brand: AIAA (American Institute of Aeronautics Ast
- Published on: 2003-05
- Original language: English
- Number of items: 1
- Dimensions: 9.00" h x 6.25" w x 1.25" l, 2.60 pounds
- Binding: Hardcover
- 634 pages
- Used Book in Good Condition
Most helpful customer reviews
1 of 1 people found the following review helpful.
Great detail in equations of motion development
By Captain J
The book does a great job deriving equations of motion. It goes step by step in explaining axis systems, through Newton's 2nd Law to come up with E.O.M. The author then describes in detail how linear perturbation works, with step by step instructions.
I use this book in conjunction with Nelson's flight stability textbook for my Aerospace grad courses and thesis.
2 of 2 people found the following review helpful.
Amazing...
By Tyler Russell
Dr. Yechout was my professor at the US Air Force Academy and I have to say that after nearly a decade since this course, I still remember how enjoyable the course and book were. The equations are laid out in simple, easy to understand approach that would be valuable to any student.
0 of 0 people found the following review helpful.
Three Stars
By Stef
Great for concepts, awful for notations, eqns, and problems
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