Lunar soft landing trajectory optimization in a 6DoF dynamical model
Lunar soft landing trajectory optimization in a 6DoF dynamical model
978-88-96427-42-2
1211-1220
Armellin, Roberto
61950d5c-3dcf-45f5-b391-7e8c6ffb8e6f
Dowlat, D.
e13a2330-6a22-4c60-809a-66793126f029
Lavagna, M.
3741b245-5b67-4371-b539-e9ba65e6c862
2011
Armellin, Roberto
61950d5c-3dcf-45f5-b391-7e8c6ffb8e6f
Dowlat, D.
e13a2330-6a22-4c60-809a-66793126f029
Lavagna, M.
3741b245-5b67-4371-b539-e9ba65e6c862
Armellin, Roberto, Dowlat, D. and Lavagna, M.
(2011)
Lunar soft landing trajectory optimization in a 6DoF dynamical model.
In Conference of the European Aerospace Socities (CEAS) 2011 Post-Conference Proceedings.
Con-fine.
.
Record type:
Conference or Workshop Item
(Paper)
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More information
Published date: 2011
Venue - Dates:
Conference of the European Aerospace Socities (CEAS) 2011, Venice, Italy, 2011-10-23 - 2011-10-27
Organisations:
Aeronautics, Astronautics & Comp. Eng
Identifiers
Local EPrints ID: 360571
URI: http://eprints.soton.ac.uk/id/eprint/360571
ISBN: 978-88-96427-42-2
PURE UUID: 619a8583-5644-49ab-a968-2b28ba13d21a
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Date deposited: 13 Dec 2013 14:39
Last modified: 08 Jan 2022 00:24
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Contributors
Author:
D. Dowlat
Author:
M. Lavagna
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