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Titlebook: Dynamics of Satellites / Dynamique des Satellites; Symposium Paris, May Maurice Roy Conference proceedings 1963 Springer-Verlag Berlin Heid

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樓主
發(fā)表于 2025-3-21 20:08:06 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
書目名稱Dynamics of Satellites / Dynamique des Satellites
副標(biāo)題Symposium Paris, May
編輯Maurice Roy
視頻videohttp://file.papertrans.cn/285/284171/284171.mp4
叢書名稱IUTAM Symposia
圖書封面Titlebook: Dynamics of Satellites / Dynamique des Satellites; Symposium Paris, May Maurice Roy Conference proceedings 1963 Springer-Verlag Berlin Heid
出版日期Conference proceedings 1963
關(guān)鍵詞Libration; Variation; celestial mechanics; computer; dynamics; mechanics; nature; relativity; satellite; sate
版次1
doihttps://doi.org/10.1007/978-3-642-48130-7
isbn_softcover978-3-642-48132-1
isbn_ebook978-3-642-48130-7
copyrightSpringer-Verlag Berlin Heidelberg 1963
The information of publication is updating

書目名稱Dynamics of Satellites / Dynamique des Satellites影響因子(影響力)




書目名稱Dynamics of Satellites / Dynamique des Satellites影響因子(影響力)學(xué)科排名




書目名稱Dynamics of Satellites / Dynamique des Satellites網(wǎng)絡(luò)公開度




書目名稱Dynamics of Satellites / Dynamique des Satellites網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Dynamics of Satellites / Dynamique des Satellites被引頻次




書目名稱Dynamics of Satellites / Dynamique des Satellites被引頻次學(xué)科排名




書目名稱Dynamics of Satellites / Dynamique des Satellites年度引用




書目名稱Dynamics of Satellites / Dynamique des Satellites年度引用學(xué)科排名




書目名稱Dynamics of Satellites / Dynamique des Satellites讀者反饋




書目名稱Dynamics of Satellites / Dynamique des Satellites讀者反饋學(xué)科排名




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沙發(fā)
發(fā)表于 2025-3-21 23:43:48 | 只看該作者
Scott L. Newstok,Ayanna Thompsonance coefficient and hence the retardation of the satellite in its onward motion along the orbit. There are other problems requiring knowledge of the satellite orientation in space. Investigation of the satellite motion about the centre of mass is also of independent interest.
板凳
發(fā)表于 2025-3-22 02:09:37 | 只看該作者
Discussion of atmospheric heat sources based on the analysis of satellite drag datarom the solar corpuscular radiation and the solar wind. If an additional heat source is used, which has a maximum at about 9. local time and a flux of 1 erg cm. sec., a time-dependent model of the upper atmosphere is obtained that is in good agreement with the observed densities.
地板
發(fā)表于 2025-3-22 07:30:00 | 只看該作者
Some problems of motion of artificial satellites about the centre of massance coefficient and hence the retardation of the satellite in its onward motion along the orbit. There are other problems requiring knowledge of the satellite orientation in space. Investigation of the satellite motion about the centre of mass is also of independent interest.
5#
發(fā)表于 2025-3-22 12:41:55 | 只看該作者
A comparison of astronomical and ballistic traditions in orbit correctionular interest is that of differential formulae, which are useful in the mathematical differential correction of an approximate orbit into better agreement with observation, in the physical or thrust differential correction of a non–rendezvous trajectory into one that intercepts its target, in guidance, in error analysis, and in optimization.
6#
發(fā)表于 2025-3-22 16:01:22 | 只看該作者
Ziele staatlicher Wirtschaftspolitiks observed by ., is noted..The process of eliminating spurious observational data on the basis of these preliminary orbits and through the use of a filtering technique is considered in detail. The potential advantages of the Gibbsian method for correlating observed data are also noted.
7#
發(fā)表于 2025-3-22 18:49:44 | 只看該作者
Theorie wirtschaftspolitischer Reformenon of long range lunar effects over an interval of many years. Numerous examples are computed and plotted. The long range solar effects are treated by averaging the disturbing function over the orbit of the satellite..The effects in the motion of a 24 hour satellite caused by the ellipticity of Earth’s equator are treated using a resonance theory.
8#
發(fā)表于 2025-3-22 21:32:40 | 只看該作者
Michael Shamiyeh,DOM Research Laboratoryrection technique. In this procedure the observation times and angles are weighted according to a priori estimates of their accuracy. In addition to the estimates of the orbital parameters, estimates of their variances and covariances are also determined.
9#
發(fā)表于 2025-3-23 05:17:55 | 只看該作者
10#
發(fā)表于 2025-3-23 07:40:48 | 只看該作者
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