Astrodynamics Network AstroNet-II
The Final Conference
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Beschreibung
These are the proceedings of the "AstroNet-II International Final Conference". This conference was one of the last milestones of the Marie-Curie Research Training Network on Astrodynamics "AstroNet-II", that has been funded by the European Commission under the Seventh Framework Programme.
The aim of the conference, and thus this book, is to communicate work on astrodynamics problems to an international and specialised audience. The results are presented by both members of the network and invited specialists. The topics include: trajectory design and control, attitude control, structural flexibility of spacecraft and formation flying.
The book addresses a readership across the traditional boundaries between mathematics, engineering and industry by offering an interdisciplinary and multisectorial overview of the field.
These are the proceedings of the "AstroNet-II International Final Conference". This conference was one of the last milestones of the Marie-Curie Research Training Network on Astrodynamics "AstroNet-II", that has been funded by the European Commission under the Seventh Framework Programme.
The aim of the conference, and thus this book, is to communicate work on astrodynamics problems to an international and specialised audience. The results are presented by both members of the network and invited specialists. The topics include: trajectory design and control, attitude control, structural flexibility of spacecraft and formation flying.
The book addresses a readership across the traditional boundaries between mathematics, engineering and industry by offering an interdisciplinary and multisectorial overview of the field.
Presents recent and new advances in trajectory design and control, attitude control, and formation flight Proceedings of an international conference at the end of a Marie-Curie Research Training Network on Astrodynamics
Autor*in
Gerard Gómez
Themen in »Astrodynamics Network AstroNet-II«
AstroNet-II International Final Conference Astrodynamics problems Attitude control Extended mission ranges Formation flying of spacecraft Minimized fuel use Structural flexibility of spacecraft Trajectory design and control