Flight Mechanics Modeling And Analysis
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Flight Mechanics Modeling and Analysis
Flight Mechanics Modeling and Analysis comprehensively covers flight mechanics and flight dynamics using a systems approach. This book focuses on applied mathematics and control theory in its discussion of flight mechanics to build a strong foundation for solving design and control problems in the areas of flight simulation and flight data analysis. The second edition has been expanded to include two new chapters and coverage of aeroservoelastic topics and engineering mechanics, presenting more concepts of flight control and aircraft parameter estimation. This book is intended for senior undergraduate aerospace students taking Aircraft Mechanics, Flight Dynamics & Controls, and Flight Mechanics courses. It will also be of interest to research students and R&D project-scientists of the same disciplines. Including end-of-chapter exercises and illustrative examples with a MATLAB®-based approach, this book also includes a Solutions Manual and Figure Slides for adopting instructors. Features: Covers flight mechanics, flight simulation, flight testing, flight control, and aeroservoelasticity Features artificial neural network- and fuzzy logic-based aspects in modeling and analysis of flight mechanics systems: aircraft parameter estimation and reconfiguration of control Focuses on a systems-based approach Includes two new chapters, numerical simulation examples with MATLAB®-based implementations, and end-of-chapter exercises Includes a Solutions Manual and Figure Slides for adopting instructors
Fundamentals of Airplane Flight Mechanics
Author: David G. Hull
language: en
Publisher: Springer Science & Business Media
Release Date: 2007-01-20
Flight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. This text is concerned with the derivation of analytical solutions of airplane flight mechanics problems associated with flight in a vertical plane. Algorithms are presented for calculating lift, drag, pitching moment, and stability derivatives. Flight mechanics is a discipline. As such, it has equations of motion, acceptable approximations, and solution techniques for the approximate equations of motion. Once an analytical solution has been obtained, numbers are calculated in order to compare the answer with the assumptions used to derive it and to acquaint students with the sizes of the numbers. A subsonic business jet is used for these calculations.
Atmospheric and Space Flight Dynamics
Author: Ashish Tewari
language: en
Publisher: Springer Science & Business Media
Release Date: 2007-11-15
Modern aerospace vehicles, such as the space shuttle, other launch vehicles, and long-range ballistic missiles, do not discriminate between atmospheric and space flight. Most texts on flight dynamics, however, make this artificial distinction and therefore do not simultaneously cover aircraft and spacecraft. Bridging this gap in the literature, Atmospheric and Space Flight Dynamics is a unified presentation, demonstrating that the two disciplines have actually evolved from the same set of physical principles. Key features inclue an introduction to a broad range of modern topics in an accessible, yet mathematically rigorous presentation; many numerical examples and simulations utilizing MATLAB® and Simulink®; software used as an instructional, hands-on tool, moving away from the "cookbook" approach found in other works; and numerous illustrations and end-of-chapter exercises. Primarily useful as a textbook for advanced undergraduate and beginning graduate-level students, the work is also an excellent reference or self-study guide for researchers and practitioners in aerospace engineering, aviation, mechanical engineering, dynamics, astrodynamics, aeronautics, and astronautics.