Efficient control of formation flying spacecraft
Research output: Contributions to collected editions/works › Contributions to collected editions/anthologies › Research › peer-review
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Efficient control of formation flying spacecraft. / Dellnitz, Michael; Junge, Oliver; Krishnamurthy, Arvind et al.
New Trends in Parallel & Distributed Computing: within the scope of the DFG Collaborative Research Centre 376 Massively Parallel Computing: Algorithms, Design Methods, Applications. ed. / Friedhelm Meyer auf der Heide; Burkhard Monien. Paderborn : Heinz Nixdorf Institut, 2006. p. 235-247 (HNI-Verlagsschriftenreihe; Vol. 181).Research output: Contributions to collected editions/works › Contributions to collected editions/anthologies › Research › peer-review
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TY - CHAP
T1 - Efficient control of formation flying spacecraft
AU - Dellnitz, Michael
AU - Junge, Oliver
AU - Krishnamurthy, Arvind
AU - Ober-Bloebaum, Sina
AU - Padberg, Kathrin
AU - Preis, Robert
N1 - Conference code: 6
PY - 2006/1/1
Y1 - 2006/1/1
N2 - Several upcoming European and American space missions will be operated using a number of spacecraft flying in formation. The associated scientific challenges are demanding, both with respect to the construction of the spacecraft as well as to the mission design. For instance, energy efficient trajectories and corresponding control laws that enable precision formation flying over long periods of time have to be con- structed. The stabilization of the group on its nominal trajectory has to be made robust with respect to failures of individual spacecraft. Correspondingly, robust and efficient inter-spacecraft communication topologies have to be designed. Finally, in view of visionary missions with hundreds of participating micro- or nano-satellites, geometric configurations have to be found which enable these communication topologies and which scale well with an increasing number of spacecraft. In this contribution we report on our investigations concerning these questions, in particular with respect to the design of energy efficient trajectories and robust communication topologies
AB - Several upcoming European and American space missions will be operated using a number of spacecraft flying in formation. The associated scientific challenges are demanding, both with respect to the construction of the spacecraft as well as to the mission design. For instance, energy efficient trajectories and corresponding control laws that enable precision formation flying over long periods of time have to be con- structed. The stabilization of the group on its nominal trajectory has to be made robust with respect to failures of individual spacecraft. Correspondingly, robust and efficient inter-spacecraft communication topologies have to be designed. Finally, in view of visionary missions with hundreds of participating micro- or nano-satellites, geometric configurations have to be found which enable these communication topologies and which scale well with an increasing number of spacecraft. In this contribution we report on our investigations concerning these questions, in particular with respect to the design of energy efficient trajectories and robust communication topologies
KW - Mathematics
UR - https://d-nb.info/97818727X/04
M3 - Contributions to collected editions/anthologies
SN - 978-3-939350-00-2
T3 - HNI-Verlagsschriftenreihe
SP - 235
EP - 247
BT - New Trends in Parallel & Distributed Computing
A2 - Meyer auf der Heide, Friedhelm
A2 - Monien, Burkhard
PB - Heinz Nixdorf Institut
CY - Paderborn
T2 - 6. International Heinz Nixdorf Symposium - 2006
Y2 - 17 January 2006 through 18 January 2006
ER -