Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Jonathan Aziz"'
Publikováno v:
Journal of Guidance, Control, and Dynamics. 42:963-975
This paper presents the application of differential dynamic programming to low-thrust trajectory optimization in the three-body problem along with supporting techniques. A penalty method is suggest...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c765553ac29a2d48473d8536ea7266cc
https://doi.org/10.2514/1.g003617
https://doi.org/10.2514/1.g003617
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 17:181-188
Solar electric propulsion (SEP) is the dominant design option for employing low-thrust propulsion on a space mission. Spacecraft solar arrays power the SEP system but are subject to blackout periods during solar eclipse conditions. Discontinuity in p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::98a2537a482048c1cee937cd61a9c56e
https://doi.org/10.2322/tastj.17.181
https://doi.org/10.2322/tastj.17.181
Publikováno v:
The Journal of the Astronautical Sciences. 65:205-228
Low-thrust trajectories about planetary bodies characteristically span a high count of orbital revolutions. Directing the thrust vector over many revolutions presents a challenging optimization problem for any conventional strategy. This paper demons
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4c3dd2bbf162538e2a3bc085a8750d71
https://doi.org/10.1007/s40295-017-0122-8
https://doi.org/10.1007/s40295-017-0122-8
Autor:
Christopher P. McKay, Anthony Colaprete, Jonas Jonsson, Jonathan Aziz, Andres Dono-Perez, Chad R. Frost, David Mauro, Michael Nayak, Jason Swenson, D. W. G. Sears, Jan Stupl, Michael Soulage, Fan Yang Yang
Publikováno v:
Advances in Space Research. 57:1133-1146
We present a mission concept designed at NASA Ames Research Center for a two-probe mission to the dwarf planet Ceres, utilizing a set of small low-cost spacecraft. The primary spacecraft will carry both a mass and an infrared spectrometer to characte
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::83ee4106f4f38847f65d8c254dc05607
https://doi.org/10.1016/j.asr.2015.12.028
https://doi.org/10.1016/j.asr.2015.12.028
Publikováno v:
2018 Space Flight Mechanics Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::598de057480e6cc940931df0b3ee6816
https://doi.org/10.2514/6.2018-2223.c1
https://doi.org/10.2514/6.2018-2223.c1
Publikováno v:
2018 Space Flight Mechanics Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f62c18c841fd917131c291944e666b1b
https://doi.org/10.2514/6.2018-2223
https://doi.org/10.2514/6.2018-2223