Intersatellite Links and Relative Navigation: Pre-conditions for Formation Flights with Pico- and Nanosatellites

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• 作者：Michael Marszalek^* ; ^{m.marszalek@telematik-zentrum.de" class="auth_mail" title="E-mail the corresponding author} ; ^{m.drentschew@telematik-zentrum.de" class="auth_mail" title="E-mail the corresponding author} ; Oliver Kurz^** ; ^{oliver.kurz@iis.fraunhofer.de" class="auth_mail" title="E-mail the corresponding author} ; Maximilian Drentschew^* ; ^{schmidt.marco@informatik.uni-wuerzburg.de" class="auth_mail" title="E-mail the corresponding author} ; ^{schi@informatik.uni-wuerzburg.de" class="auth_mail" title="E-mail the corresponding author} ; Marco Schmidt^*** ; Klaus Schilling^***
• 刊名：IFAC-PapersOnLine
• 出版年：2011
• 出版时间：January 2011
• 年：2011
• 卷：44
• 期：1
• 页码：3027-3032
• 全文大小：562 K

文摘

A group of satellites can be classified as a constellation, formation or cluster. Multiple coordinated satellites are described as a formation, if a closed-loop control is adjusted, thus providing a coordinated motion control on basis of their relative positions to preserve the topology (Schilling [2009]). This technology enables various application scenarios, for example, interferometry or in-orbit servicing and it is subject to multiple technological requirements related to formation flying, limited resources or scientific payloads. In the framework of the feasibility study NaKoFo, this paper discusses the potential benefits, drawbacks and problems associated with intersatellite links and relative navigation with pico- and nanosatellites. The requirements of an intersatellite link are analyzed based on frequency, modulation, antenna, power and network protocol. A short overview of adequate communication systems for pico- and nanosatellites is also presented. Technologies for relative position determination are presented and discussed regarding their applicability in small satellite systems as well as their requirements on an intersatellite link.