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Title Details:
Aircraft control systems
Authors: Spathopoulos, Vasileios
Reviewer: Seferlis, Panagiotis
Subject: ENGINEERING AND TECHNOLOGY > TECHNOLOGICAL SCIENCES AND ENGINEERING > AIRCRAFT TECHNOLOGY AND ENGINEERING
ENGINEERING AND TECHNOLOGY > TECHNOLOGICAL SCIENCES AND ENGINEERING > AIRCRAFT TECHNOLOGY AND ENGINEERING > AERODYNAMICS
ENGINEERING AND TECHNOLOGY > TECHNOLOGICAL SCIENCES AND ENGINEERING > AIRCRAFT TECHNOLOGY AND ENGINEERING > FLIGHT TEST AND RESEARCH
ENGINEERING AND TECHNOLOGY > TECHNOLOGICAL SCIENCES AND ENGINEERING > AIRCRAFT TECHNOLOGY AND ENGINEERING > AVIATION INSTRUMENTATION
ENGINEERING AND TECHNOLOGY > TECHNOLOGICAL SCIENCES AND ENGINEERING > AIRCRAFT TECHNOLOGY AND ENGINEERING > STABILITY AND CONTROL
ENGINEERING AND TECHNOLOGY > TECHNOLOGICAL SCIENCES AND ENGINEERING > AIRCRAFT TECHNOLOGY AND ENGINEERING > AIRCRAFT DESIGN
ENGINEERING AND TECHNOLOGY > TECHNOLOGICAL SCIENCES AND ENGINEERING > AIRCRAFT TECHNOLOGY AND ENGINEERING > FLIGHT MECHANICS
Keywords:
Stability And Control
Aircraft Instruments
Flight Dynamics
Flying Qualities
Description:
Abstract:
Aircraft control systems, whether conventional or automatic, are an integral part of aircraft design. Everyone involved in aircraft design or maintenance must have at least a basic understanding of how these systems work. The purpose of the textbook "Aircraft Control Systems" is to convey this knowledge in a comprehensive and understandable manner. The first chapter provides an overview of the basic principles of aerodynamics necessary for a complete understanding of the operating mechanisms of control systems. The second chapter presents the conventional methods of aircraft control through the movement of appropriate surfaces. The third chapter thoroughly analyzes static longitudinal and lateral-directional stability and the factors that determine it. The fourth chapter defines the linear and non-linear equations of aircraft motion. The fifth chapter presents the modeling of motion through aircraft transfer functions together with the characteristics of dynamic stability. The sixth chapter briefly describes the concept of flight performance. The seventh chapter presents a summary of the basic concepts of classical automatic control theory with an emphasis on the root locus method. The eighth chapter provides examples of adding artificial stability to improve flight performance. The ninth chapter presents the design of simple automatic pilots and describes the basic principles of the ILS system. The tenth chapter analyzes the basic concepts of state space modeling. The eleventh and final chapter applies these concepts to aircraft motion modeling and the design of automatic control systems.
Type: Undergraduate textbook
Creation Date: 09-10-2015
Item Details:
ISBN 978-618-82124-3-5
License: http://creativecommons.org/licenses/by-nc-nd/3.0/gr
DOI http://dx.doi.org/10.57713/kallipos-881
Handle http://hdl.handle.net/11419/120
Bibliographic Reference: Spathopoulos, V. (2015). Aircraft control systems [Undergraduate textbook]. Kallipos, Open Academic Editions. https://dx.doi.org/10.57713/kallipos-881
Language: Greek
Consists of:
1. Introductory concepts
2. Control and balance
3. Static stability aircraft
4. Aircraft equations of motion
5. Aircraft transfer kits
6. Flying skills
7. Basic automatic control theory
8. Adding artificial stability
9. Autopilot design
10. Modelling in state space
11. Modelling and control of aircraft in state space
Number of pages 200
Publication Origin: Kallipos, Open Academic Editions
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