Zobrazeno 1 - 10
of 19
pro vyhledávání: '"Meßmann, David"'
Publikováno v:
In Acta Astronautica November 2024 224:546-557
Akademický článek
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Autor:
Cojocari, Ion, Meier, Matthias, Laurent, Philippe, Laviron, Adrien, Arrigucci, Marco, Carminati, Marco, Deda, Griseld, Fiorini, Carlo, Geigenberger, Katrin, Glas, Cynthia, Greiner, Jochen, Hindenberger, Peter, King, Pietro, Lechner, Peter, Losekamm, Martin, Mertens, Susanne, Meßmann, David, Rückerl, Sebastian, Toscano, Lorenzo, Walter, Ulrich, Willers, Michael
Publikováno v:
In Nuclear Inst. and Methods in Physics Research, A 11 January 2023 1046
Autor:
Volk, Lucien, Borrek, Rosalinde, Zischka, Nicolas, Koch, Johannes, Sharma, Isha, Nardini, Matteo, Holl, Linda, Gruber, Simon, Schummer, Florian, Kiesbye, Jonis, Messmann, David, Lülf, Martin
Publikováno v:
Small Satellite Conference
This paper covers the operations and lessons learned for the MOVE-II and MOVE-IIb satellites. Both are 1U CubeSats, with their purpose being hands-on education for students of all technical fields related to aerospace. The hardware of the spacecraft
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1459::574c37b871526f5213f5980eeb7558d7
https://digitalcommons.usu.edu/smallsat/2022/all2022/224
https://digitalcommons.usu.edu/smallsat/2022/all2022/224
Autor:
Qedar, Ran, Sridharan, Saish, Romanov-Chernigovksy, Ignaty, Messmann, David, Kiesbye, Jonis, Barrington-Brown, James
Publikováno v:
Small Satellite Conference
Objectives: Modular ADCS based on CubeSat flight experience, space heritage hardware and rad hard components for small satellites Project goal: Integration of independent modules based on electronic data sheets (EDS) configuration system Capabilities
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1459::17bc195d3e4a7e694bfa20868e5682e9
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4936&context=smallsat
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4936&context=smallsat
Autor:
Kiesbye, Jonis, Messmann, David, Preisinger, Maximilian, Reina, Gonzalo, Nagy, Daniel, Schummer, Florian, Mostad, Martin, Kale, Tejas, Langer, Martin
Publikováno v:
Aerospace
Volume 6
Issue 12
Volume 6
Issue 12
This article reports the ongoing work on an environment for hardware-in-the-loop (HIL) and software-in-the-loop (SIL) tests of CubeSats and the benefits gained from using such an environment for low-cost satellite development. The satellite tested fo
Autor:
Rueckerl, Sebastian, Meßmann, David, Appel, Nicolas, Kiesbye, Jonis, Schummer, Florian, Faehling, Markus, Krempel, Lucas, Kale, Tejas, Lill, Alexander, Reina, Gonzalo, Schnierle, Patrick, Wuerl, Sebastian, Langer, Martin, Luelf, Martin
Publikováno v:
Small Satellite Conference
MOVE-II (Munich Orbital Verification Experiment) is the second satellite of the Technical University of Munich’s educational CubeSat program. On December 3, 2018, the satellite was launched on the SSO-A SmallSat Express from the Vandenberg Air Forc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1459::d6c63910d5ec47579b1fa415dc22a9cf
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4348&context=smallsat
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4348&context=smallsat
Autor:
Kiesbye, Jonis, Messmann, David, Preisinger, Maximilian, Reina, Gonzalo, Nagy, Daniel, Schummer, Florian, Mostad, Martin, Kale, Tejas, Langer, Martin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od_______518::634f3658fecb86f087897693b4ec3ee6
https://mediatum.ub.tum.de/1543504
https://mediatum.ub.tum.de/1543504
Autor:
MESSMANN, David, GRUEBLER, Thomas, COELHO, Felipe, OHLENFORST, Torsten, VAN BRUEGGE, Jan, MAURACHER, Florian, DOETTERL, Moritz, PLAMAUER, Sebastian, SCHNIERLE, Patrick, SEIFERT, Marc, LANGER, Martin, KALE, Tejas, FUHRMANN, Arno, ULANOWSKI, Alexander, KARAGIANNIS, Eleftherios, LAUSENHAMMER, Thomas, MERANER, Andrea
MOVE-II (Munich Orbital Verification Experiment) will be the first CubeSat of the Technical University of Munich (TUM) utilizing a magnetorquer-based active attitude determination and control system (ADCS). The ADCS consists of six circuit boards (fi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::71e1b730b945716877aab89d511f594b
Autor:
MESSMANN, David, COELHO, Felipe, NIERMEYER, Philipp, LANGER, Martin, HUANG, He, WALTER, Ulrich
This paper presents the fundamental work on the attitude control design using solely magnetic actuation for the MOVE-II mission. Two control modes are primarily considered: detumbling and sun pointing control. Regarding the sun pointing control, two
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0abc4a330ecb690ad1778e6d1571ec5e