Sadraey, Mohammad H.
Flight Stability and Control [electronic resource] / by Mohammad H. Sadraey. - 1st ed. 2022. - XII, 236 p. 78 illus., 59 illus. in color. online resource. - Synthesis Lectures on Mechanical Engineering, 2573-3176 . - Synthesis Lectures on Mechanical Engineering, .
Preface -- Aircraft Equations -- Trim -- Longitudinal Stability -- Lateral-directional Stability -- Longitudinal Control -- latera;-Directional Control.-Problems -- References.
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).
9783031187650
10.1007/978-3-031-18765-0 doi
Aerospace engineering.
Astronautics.
Mechanical engineering.
Control engineering.
Robotics.
Automation.
Aerospace Technology and Astronautics.
Mechanical Engineering.
Control and Systems Theory.
Control, Robotics, Automation.
TL1-4050
629.1
Flight Stability and Control [electronic resource] / by Mohammad H. Sadraey. - 1st ed. 2022. - XII, 236 p. 78 illus., 59 illus. in color. online resource. - Synthesis Lectures on Mechanical Engineering, 2573-3176 . - Synthesis Lectures on Mechanical Engineering, .
Preface -- Aircraft Equations -- Trim -- Longitudinal Stability -- Lateral-directional Stability -- Longitudinal Control -- latera;-Directional Control.-Problems -- References.
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).
9783031187650
10.1007/978-3-031-18765-0 doi
Aerospace engineering.
Astronautics.
Mechanical engineering.
Control engineering.
Robotics.
Automation.
Aerospace Technology and Astronautics.
Mechanical Engineering.
Control and Systems Theory.
Control, Robotics, Automation.
TL1-4050
629.1