Výsledky vyhledávání - "Lange, Jonathan"

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Publikováno v: Lange, Jonathan Leifsson de. Utvisning av EØS-borgere. Master thesis, University of Oslo, 2023

Externí odkaz: http://hdl.handle.net/10852/102876

Lessons learned when developing a high performance attitude controlled platform to achieve microgravity for low-cost experiments

Autor: Wolnievik, Andreas, Janes, Noel, Pérez Cámara, Flavia, Dengel, Ric, Delley, Diane, Hartmann, Anne, Maestro Redondo, Paloma, Llamas Lanza, Miguel, Samuelsson, Erik, Chacartegui Rojo, Íñigo de Loyola, Lange, Jonathan, Fernández Bravo, Elena, Hiemstra, Cornelis Peter, Scholz, Sebastian, Isberg, Henning, Kull, Tõnis, Gouvalas, Spyridon

Publikováno v: UPCommons. Portal del coneixement obert de la UPC
Universitat Politècnica de Catalunya (UPC)

Available Attitude Control Systems are often targeted at orbital flights, and therefore manoeuvre slowly. As such, these solutions are suboptimal for sounding rocket experiments, as experiments such as those conducted on free falling units have restr

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::929e984ea4c9472bfc2581570e2b1d38
https://hdl.handle.net/2117/370876

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Dissertation/ Thesis

The effects of low, moderate, and high self-disclosure on electromyographic, psychogalvanic, and attitudinal response

Autor: Lange, Jonathan I.

Publikováno v: Dissertations and Theses.

This is a study of the effects of three different levels of intimate self-disclosure, low, moderate, and high, on electromyographic, psychogalvanic, and attitudinal response. The electromyography (EMG) and psychogalvanometer (GSR) are both devices wh

Externí odkaz: https://pdxscholar.library.pdx.edu/open_access_etds/2500
https://pdxscholar.library.pdx.edu/cgi/viewcontent.cgi?article=3505&context=open_access_etds

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Project ASTER: True Microgravity during Free-Fall with Attitude Stabilisation

Autor: Cámara, Flavia Pérez, Janes, Noel, Lange, Jonathan

Publikováno v: Small Satellite Conference

The verification of a spacecraft component’s functionality under microgravity conditions is an important topic for the low-cost development of CubeSat components. The testing and verification of new components is often carried out on technological

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______1459::057f37c3677866ebe9a8228443efd970
https://digitalcommons.usu.edu/smallsat/2020/all2020/102

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