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Titlebook: Computational Space Flight Mechanics; Claus Weiland Book 2010 Springer-Verlag Berlin Heidelberg 2010 Athmospheric Re-entry.Celestial mecha

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书目名称Computational Space Flight Mechanics
编辑Claus Weiland
视频video
概述Presents numerical solutions of the governing equations of space flight mechanics.Enables the reader to understand the compicated physics behing.Incl. FORTRAN and MATLAB codes as well as solutions to
图书封面Titlebook: Computational Space Flight Mechanics;  Claus Weiland Book 2010 Springer-Verlag Berlin Heidelberg 2010 Athmospheric Re-entry.Celestial mecha
描述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. -
出版日期Book 2010
关键词Athmospheric Re-entry; Celestial mechanics; Consitent derivation of Governing Equations; FORTRAN; Kepler
版次1
doihttps://doi.org/10.1007/978-3-642-13583-5
isbn_softcover978-3-642-43211-8
isbn_ebook978-3-642-13583-5
copyrightSpringer-Verlag Berlin Heidelberg 2010
The information of publication is updating

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Durdana Ovais,Richi Simon,Shumayela HasanThe simulation of flight trajectories of space vehicles requires the knowledge of the various forces and moments which act on these vehicles. Forces and moments are produced by aerothermodynamics, propulsion and reaction control systems, and gravitational fields.
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https://doi.org/10.1007/978-3-030-39149-2Our planetary system, with the Sun as central body, embraces nine planets. The characteristic data and orbital elements of these planets are very different. In Tables A.1 and A.2 a selection of this data, mainly taken from [1] to [4], are listed.
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The Two-Body Problem,Gravitational forces dominate the orbital motion of celestial bodies and unpowered vehicles. All the stars, planets, moons and dark matters, moving around in the universe, contribute mutually to the field of gravitational forces.
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