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Titlebook: Dynamics of Flexible Spacecraft; Department of Genera Peter W. Likins,Robert E. Roberson,Jens Wittenburg Book 1971 CISM Udine 1971 Dynamics

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發(fā)表于 2025-3-21 17:41:25 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
書目名稱Dynamics of Flexible Spacecraft
副標(biāo)題Department of Genera
編輯Peter W. Likins,Robert E. Roberson,Jens Wittenburg
視頻videohttp://file.papertrans.cn/285/284081/284081.mp4
叢書名稱CISM International Centre for Mechanical Sciences
圖書封面Titlebook: Dynamics of Flexible Spacecraft; Department of Genera Peter W. Likins,Robert E. Roberson,Jens Wittenburg Book 1971 CISM Udine 1971 Dynamics
出版日期Book 1971
關(guān)鍵詞Dynamics; Spacecraft; dynamics; mechanics
版次1
doihttps://doi.org/10.1007/978-3-7091-2908-1
isbn_softcover978-3-211-81199-3
isbn_ebook978-3-7091-2908-1Series ISSN 0254-1971 Series E-ISSN 2309-3706
issn_series 0254-1971
copyrightCISM Udine 1971
The information of publication is updating

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https://doi.org/10.1007/978-3-7091-2908-1Dynamics; Spacecraft; dynamics; mechanics
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發(fā)表于 2025-3-22 12:42:15 | 只看該作者
Introductory remarks,many purposes during the last two decades it has been possible to model the spacecraft as a rigid bodies or gyrostats, or perhaps simple two-body systems. However, even from the earliest days of real satellites, cases have been known where non-rigid characteristics have dominated the dynamical behavior.
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發(fā)表于 2025-3-22 12:58:16 | 只看該作者
Betilde Mu?oz-Pogossian,Tyler FinnAny portion of a vehicle which can reasonably be idealized as linearly elastic and for which “small” oscillatory deformations may be anticipated (perhaps in combination with large steady-state deformations) is called a ..
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Barycentric Vectors and Related Topics,The last equation of the previous lecture shows, with minor differences in notation, the form taken by Eq. 3 of lecture 10 when Eq. 1 of that lecture is solved for a and the result used to eliminate the attachment interaction forces from the rotational equations.
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