Zobrazeno 1 - 7
of 7
pro vyhledávání: '"A. Bakr Elhady"'
Publikováno v:
International Journal for Simulation and Multidisciplinary Design Optimization, Vol 3, Iss 1, Pp 289-296 (2009)
Solar array rotation mechanism provides a hinged joint between the solar panel and satellite body, smooth rotation of the solar array into deployed position and its fixation in this position. After unlocking of solar panel (while in orbit), rotation
Externí odkaz:
https://doaj.org/article/4b3f976cc6d840a6b37d17d7af2ad505
Publikováno v:
International Journal for Simulation and Multidisciplinary Design Optimization, Vol 3, Iss 1, Pp 289-296 (2009)
Int. J. Simul. Multidisci. Des. Optim., 3, 1, January 2009
Int. J. Simul. Multidisci. Des. Optim., 3, 1, January 2009
Solar array rotation mechanism provides a hinged joint between the solar panel and satellite body, smooth rotation of the solar array into deployed position and its fixation in this position. After unlocking of solar panel (while in orbit), rotation
Publikováno v:
2014 IEEE Aerospace Conference; 2014, p1-40, 40p
Publikováno v:
2014 IEEE Aerospace Conference; 2014, p1-39, 39p
Autor:
Ali-Akbari, Hossein Ramezani
This paper presents an innovative method to control the rotational speed of a satellite solar panel during its deployment phase. A brushed DC motor has been utilized in the passive spring driven deployment mechanism to reduce the deployment speed. In
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5743728904f2c238e4662e7af6cedeba
Publikováno v:
2014 IEEE Aerospace Conference; 2014, pc1-c1, 1p
Designing satellite structures poses an ongoing challenge as the interaction between analysis, experimental testing, and manufacturing phases is underdeveloped. Finite Element Analysis for Satellite Structures: Applications to Their Design, Manufactu