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| Author | : University of Michigan. Engineering Summer Conferences |
| Publisher | : |
| Total Pages | : 624 |
| Release | : 1966 |
| Genre | : Astrodynamics |
| ISBN | : |
| Author | : Frank J. Regan |
| Publisher | : AIAA |
| Total Pages | : 616 |
| Release | : 1993 |
| Genre | : Space vehicles |
| ISBN | : 9781600860461 |
| Author | : University of Michigan |
| Publisher | : |
| Total Pages | : |
| Release | : 1964 |
| Genre | : |
| ISBN | : |
| Author | : University of Michigan. Engineering Summer Conferences |
| Publisher | : |
| Total Pages | : 456 |
| Release | : 1965 |
| Genre | : Astrodynamics |
| ISBN | : |
| Author | : University of Michigan. Engineering Summer Conferences |
| Publisher | : |
| Total Pages | : 540 |
| Release | : 1964 |
| Genre | : Astrodynamics |
| ISBN | : |
| Author | : Frank J. Regan |
| Publisher | : |
| Total Pages | : 442 |
| Release | : 1984 |
| Genre | : Technology & Engineering |
| ISBN | : |
| Author | : Claus Weiland |
| Publisher | : Springer Science & Business Media |
| Total Pages | : 305 |
| Release | : 2010-06-29 |
| Genre | : Technology & Engineering |
| ISBN | : 3642135838 |
Themechanicsofspace?ightisan olddiscipline.Itstopicoriginallywasthemotion of planets, moons and other celestial bodies in gravitational ?elds. Kepler’s (1571 - 1630) observations and measurements have led to probably the ?rst mathematical description of planet’s motion. Newton (1642 - 1727) gave then, with the devel- ment of his principles of mechanics, the physical explanation of these motions. Since then man has started in the second half of the 20th centuryto capture ph- ically the Space in the sense that he did develop arti?cial celestial bodies, which he brought into Earth’s orbits, like satellites or space stations, or which he did send to planets or moons of our planetary system, like probes, or by which p- ple were brought to the moon and back, like capsules. Further he developed an advanced space transportation system, the U.S. Space Shuttle Orbiter, which is the only winged space vehicle ever in operation. In the last two and a half decades there were several activities in the world in order to succeed the U.S. Orbiter, like the HERMES project in Europe, the HOPE project in Japan, the X-33, X-34 and X-37 studies and demonstrators in the United States and the joint U.S. - European project X-38. However, all these projects were cancelled. The motion of these vehicles can be described by Newton’s equation of motion.
| Author | : Robert F. Stengel |
| Publisher | : Princeton University Press |
| Total Pages | : 914 |
| Release | : 2022-11-01 |
| Genre | : Science |
| ISBN | : 0691237042 |
An updated and expanded new edition of an authoritative book on flight dynamics and control system design for all types of current and future fixed-wing aircraft Since it was first published, Flight Dynamics has offered a new approach to the science and mathematics of aircraft flight, unifying principles of aeronautics with contemporary systems analysis. 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. Special attention is devoted to models and techniques for analysis, simulation, evaluation of flying qualities, and robust control system design. Using common notation and not assuming a strong background in aeronautics, Flight Dynamics will engage a wide variety of readers, including aircraft designers, flight test engineers, researchers, instructors, and students. It introduces principles, derivations, and equations of flight dynamics as well as methods of flight control design with frequent reference to MATLAB functions and examples. Topics include aerodynamics, propulsion, structures, flying qualities, flight control, and the atmospheric and gravitational environment. The second edition of Flight Dynamics features up-to-date examples; a new chapter on control law design for digital fly-by-wire systems; new material on propulsion, aerodynamics of control surfaces, and aeroelastic control; many more illustrations; and text boxes that introduce general mathematical concepts. Features a fluid, progressive presentation that aids informal and self-directed study Provides a clear, consistent notation that supports understanding, from elementary to complicated concepts Offers a comprehensive blend of aerodynamics, dynamics, and control Presents a unified introduction of control system design, from basics to complex methods Includes links to online MATLAB software written by the author that supports the material covered in the book
| Author | : Rama K. Yedavalli |
| Publisher | : John Wiley & Sons |
| Total Pages | : 554 |
| Release | : 2020-02-25 |
| Genre | : Technology & Engineering |
| ISBN | : 1118934458 |
Flight Vehicle Dynamics and Control Rama K. Yedavalli, The Ohio State University, USA A comprehensive textbook which presents flight vehicle dynamics and control in a unified framework Flight Vehicle Dynamics and Control presents the dynamics and control of various flight vehicles, including aircraft, spacecraft, helicopter, missiles, etc, in a unified framework. It covers the fundamental topics in the dynamics and control of these flight vehicles, highlighting shared points as well as differences in dynamics and control issues, making use of the ‘systems level’ viewpoint. The book begins with the derivation of the equations of motion for a general rigid body and then delineates the differences between the dynamics of various flight vehicles in a fundamental way. It then focuses on the dynamic equations with application to these various flight vehicles, concentrating more on aircraft and spacecraft cases. Then the control systems analysis and design is carried out both from transfer function, classical control, as well as modern, state space control points of view. Illustrative examples of application to atmospheric and space vehicles are presented, emphasizing the ‘systems level’ viewpoint of control design. Key features: Provides a comprehensive treatment of dynamics and control of various flight vehicles in a single volume. Contains worked out examples (including MATLAB examples) and end of chapter homework problems. Suitable as a single textbook for a sequence of undergraduate courses on flight vehicle dynamics and control. Accompanied by a website that includes additional problems and a solutions manual. The book is essential reading for undergraduate students in mechanical and aerospace engineering, engineers working on flight vehicle control, and researchers from other engineering backgrounds working on related topics.
| Author | : Wilbur L. Hankey |
| Publisher | : AIAA |
| Total Pages | : 160 |
| Release | : 1988 |
| Genre | : Space vehicles |
| ISBN | : 9781600861062 |
