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
Now updated and expanded, this authoritative book by award-winning aeronautics engineer Robert Stengel presents traditional material in the context of modern computational tools and multivariable methods.
Introduction to Aircraft Flight Dynamics
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics.
Based on this, one may define control margins such as the elevator trim margin. ... Similar to the elevator trim margin, one may define a corresponding control margin, the elevator manoeuvre margin and the so-called manoeuvre point ...
DYNAMICS OF FLIGHT: Stability and Control
HANDBOOK OF FLIGHT DYNAMICS: Principles and Practices
Performance, Stability, Dynamics, and Control of Airplanes
For example, the fourth-order Adams–Bashforth method is given by yn+1 = yn + h 24(55fn − 59fn−1 + 37fn−2 − 9fn−2) (2.50) In numerical methods, the computation of yn+1 can be treated as a predictor, enabling fn+1 to be computed to ...
This book offers a unified presentation that does not discriminate between atmospheric and space flight.
This book provides extensive coverage of individual topics within flight mechanics, including overviews of aerodynamics and propulsion.