Flight Stability and Control

By:

Mohammad H. Sadraey

Format:

Paperback / softback

Series:

Synthesis Lectures on Mechanical Engineering

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Description

Aircraft safety is a function of several parameters including flight stability and control. An air vehicle must be stable if it is to remain in flight. Moreover, it must be controllable as well as trimmable. This book delivers the fundamental concepts of stability and control, as well as their associated areas. It explains airworthiness, dynamic and static stability, longitudinal, lateral, and directional control, flight measurement devices and sensors, and control surfaces which are necessary topics to be considered during the aircraft design process. This book is mainly focused on air vehicles' stability features and control capabilities. The aircraft addressed in this book is a rigid-body point mass object. Describing the complete motion of a rigid-body aircraft, this book covers equations of motion with six degrees of freedom (DOF)

Author Biography:

Mohammad Sadraey has over twenty years of teaching experience at a number of institutions including Southern New Hampshire University, Daniel Webster College, and the University of Kansas. He has both an M.Sc. and Ph.D. in Aerospace Engineering in 2006. He is a senior member of the American Institute of Aeronautics and Astronautics (AIAA), member of Sigma Gamma Tu, and the American Society for Engineering Education (ASEE).

Release date NZ

January 4th, 2024

Author

Mohammad H. Sadraey

Audience

Professional & Vocational

Edition

1st ed. 2022

Illustrations

59 Illustrations, color; 19 Illustrations, black and white; XII, 236 p. 78 illus., 59 illus. in color.

Pages

236

Series

Synthesis Lectures on Mechanical Engineering

ISBN-13

9783031187674

Product ID

38488610

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