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Titlebook: Distributed Space Missions for Earth System Monitoring; Marco D‘Errico Book 2013 Springer Science+Business Media New York 2013 Earth obser

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書(shū)目名稱(chēng)Distributed Space Missions for Earth System Monitoring
編輯Marco D‘Errico
視頻videohttp://file.papertrans.cn/282/281951/281951.mp4
概述A definitive reference in its field, this book provides an extensive description of studies of Earth using remote sensing missions that build on formation flying.Focuses on distributed space missions
叢書(shū)名稱(chēng)Space Technology Library
圖書(shū)封面Titlebook: Distributed Space Missions for Earth System Monitoring; Marco D‘Errico Book 2013 Springer Science+Business Media New York 2013 Earth obser
描述This title analyzes distributed Earth observation missions from different perspectives. In particular, the issues arising when the payloads are distributed on different satellites are considered from both the theoretical and practical points of view. Moreover, the problems of designing, measuring, and controlling relative trajectories are thoroughly presented in relation to theory and applicable technologies. Then, the technological challenges to design satellites able to support such missions are tackled. An ample and detailed description of missions and studies complements the book subject.
出版日期Book 2013
關(guān)鍵詞Earth observation; Formation flying; GPS-based navigation; RF-based navigation; Radar sensors; Radar syst
版次1
doihttps://doi.org/10.1007/978-1-4614-4541-8
isbn_softcover978-1-4899-9053-2
isbn_ebook978-1-4614-4541-8Series ISSN 0924-4263 Series E-ISSN 2542-8896
issn_series 0924-4263
copyrightSpringer Science+Business Media New York 2013
The information of publication is updating

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Multistatic Radar Systemsre discussed, with an emphasis on single- and multi-baseline interferometric techniques, deriving lower and upper bounds to the required spacecraft separation. Several multistatic formation concepts (Cartwheel, Helix, etc.) are discussed within the general framework provided by the Clohessy-Wiltshir
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Relative Trajectory Designm the first Hill’s schematization (circular orbit, close satellites) is described, considering the inclusion of chief’s orbit eccentricity and orbital perturbations. In particular, the inclusion of J.-secular effects is treated in depth considering various approaches in literature. Literature is als
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GPS Based Relative Navigation-flying satellites in low Earth orbit. Similar to terrestrial applications, the relative navigation benefits from a high level of common error cancellation. Furthermore, the integer nature of double-difference carrier phase ambiguities can be exploited in carrier phase differential GPS (CDGPS). Both
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Radio Frequency-Based Relative Navigationin certain boundaries. This knowledge can be obtained using an autonomous relative navigation system based on radio frequency (RF) signals. The design aspects of such a system are detailed in this chapter. As all RF-based relative navigation systems are based on GNSS technology, the discussion is li
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Communication in Distributed Satellite Systemst overall performance. This section provides further details for the special situation of network nodes consisting of several satellites and ground stations. Via the communication system partially autonomous functions at each satellite are to be coordinated to enable joint observations. Such self-or
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