Zobrazeno 1 - 10
of 140
pro vyhledávání: '"Peter M. Bainum"'
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 42:158-164
LEO(Low Earth Orbit) Satellite which is discarded should be reentered to atmosphere in 25 years by `25 years rule` of IADC(Inter-Agency Space Debris Coordination Committee) Guidelines. If the parts of satellite are survived from severe aerothermodyna
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::483f582f46be210cba3559e9c38c6fe6
https://doi.org/10.5139/jksas.2014.42.2.158
https://doi.org/10.5139/jksas.2014.42.2.158
Autor:
Kyeum-Rae Cho, Hae-dong Kim, Peter M. Bainum, Dae-Woo Lee, Jang-Sik Yang, Seung-Woo Baek, Sun-mi Han
Publikováno v:
Acta Astronautica. 68:1396-1402
In this paper, a scheduling optimization algorithm is developed and verified for autonomous satellite mission operations. As satellite control and operational techniques continue to develop, satellite missions become more complicated and the overall
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::432523c39a60c41343ffbdca69f64891
https://doi.org/10.1016/j.actaastro.2010.08.011
https://doi.org/10.1016/j.actaastro.2010.08.011
Autor:
Peter M. Bainum, Pedro A. Capó-Lugo
Publikováno v:
Journal of Aerospace Engineering, Sciences and Applications. 3:1-18
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d646fe3c505c16fb4644da12083680cf
https://doi.org/10.7446/jaesa.0301.01
https://doi.org/10.7446/jaesa.0301.01
Autor:
Pedro A. Capó-Lugo, Peter M. Bainum
Publikováno v:
Acta Astronautica. 65:1058-1067
In previous papers, the authors developed an active control scheme based on the linear quadratic regulator (LQR) to maintain the separation distance constraints of the NASA benchmark tetrahedron constellation. Two different active control schemes wer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ffc0539302555a0a2af4ee3052007093
https://doi.org/10.1016/j.actaastro.2009.03.040
https://doi.org/10.1016/j.actaastro.2009.03.040
Autor:
Pedro A. Capo-Lugo, Peter M. Bainum
Publikováno v:
Journal of Mechanics of Materials and Structures. 4:837-854
The NASA Benchmark Tetrahedron Constellation is a four-satellite formation that requires a nominal separation distance at every apogee point. The deployment procedure of a tetrahedron constellation is complex and depends on the separation distance be
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e1d4408e807cda67cea611d178ff2364
https://doi.org/10.2140/jomms.2009.4.837
https://doi.org/10.2140/jomms.2009.4.837
Autor:
Pedro A. Capo-Lugo, Peter M. Bainum
Publikováno v:
Journal of Guidance, Control, and Dynamics. 32:675-679
I NHIGHLY elliptical orbits (HEO), the solar pressure can perturb themotion of a constellation because of the longer exposure of the satellites to the sun [1]. To study its effects on the controller, the Tschauner–Hempel (TH) equations are augmente
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2f5113ecc4c9224dfc20377366eb349a
https://doi.org/10.2514/1.37484
https://doi.org/10.2514/1.37484
Autor:
Peter M. Bainum, Pedro A. Capó-Lugo
Publikováno v:
Journal of Mechanics of Materials and Structures. 2:1541-1559
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dbc88eca59d526c272a617095751907f
https://doi.org/10.2140/jomms.2007.2.1541
https://doi.org/10.2140/jomms.2007.2.1541
Autor:
Pedro A. Capó-Lugo, Peter M. Bainum
Publikováno v:
Journal of Guidance, Control, and Dynamics. 30:1152-1156
T HE proposed NASA benchmark tetrahedron constellation is a complex formation to be maintained at every apogee point. In previous papers, the authors developed a strategy and determined the initial conditions to maintain the tetrahedron formation [1,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e48e95c5bc3689d369923b121da1d6d0
https://doi.org/10.2514/1.24371
https://doi.org/10.2514/1.24371
Publikováno v:
Acta Astronautica. 60:865-872
This work provides some important information about control structure interaction (CSI) for a large space structure (LSS) attitude control subsystem (ACS) comprised of thrusters and reaction wheels. The LSS physical model is assumed as a rigid long t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0679066be1aed515f81bca722ef90c98
https://doi.org/10.1016/j.actaastro.2006.11.008
https://doi.org/10.1016/j.actaastro.2006.11.008
Publikováno v:
Acta Astronautica. 57:685-697
Two techniques to deploy four spacecraft in an along-track formation with 500 km separation distance in an elliptical orbit are developed and evaluated: (1) The deployment from the original (parking) circular orbit into the final elliptical orbit is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0baecb9b0c0709bb7d78ef48eecf2aa7
https://doi.org/10.1016/j.actaastro.2005.03.065
https://doi.org/10.1016/j.actaastro.2005.03.065