Flight Dynamics Principles.

Cook, M. V.

ISBN 10: 0340632003 / ISBN 13: 9780340632000

Published by Oxford (u.a.): Butterworth-Heinemann, 1997

About this Item

Zust: Gutes Exemplar. Mit Abbildungen, XVIII, 379 S. Englisch 678g.

Seller Inventory # 488622

Bibliographic Details

• Title: Flight Dynamics Principles.
• Publisher: Oxford (u.a.): Butterworth-Heinemann
• Publication Date: 1997
• Language: English
• ISBN 10: 0340632003
• ISBN 13: 9780340632000
• Binding: Broschiert
• Condition: Sehr gut
• Weight: 678 grams
• Seller catalogs:
  • Technik

About this title

Synopsis

Flight dynamicists today need not only a thorough understanding of the classical stability and control theory of aircraft, but also a working appreciation of flight control systems and consequently a grounding in the theory of automatic control. In this text the author fulfils these requirements by developing the theory of stability and control of aircraft in a systems context.

The key considerations are introduced using dimensional or normalised dimensional forms of the aircraft equations of motion only and through necessity the scope of the text will be limited to linearised small perturbation aircraft models. The material is intended for those coming to the subject for the first time and will provide a secure foundation from which to move into non-linear flight dynamics, simulation and advanced flight control. Placing emphasis on dynamics and their importance to flying and handling qualities it is accessible to both the aeronautical engineer and the control engineer.

Emphasis on the design of flight control systems
Intended for undergraduate and postgraduate students studying aeronautical subjects and avionics, systems engineering, control engineering
Provides basic skills to analyse and evaluate aircraft flying qualities

From the Publisher

This thorough discussion of the classical stability and control theory of aircraft helps readers gain an appreciation of flight control systems. They will learn how to analyze and evaluate aircraft flying qualities and initiate preliminary augmentation design, as well as develop a foundation from which to move onto non-linear flight dynamics, simulation, and flight control.