Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Hyo-Choong Bang"'
Publikováno v:
Journal of Astronomy and Space Sciences, Vol 24, Iss 3, Pp 235-248 (2007)
We developed a software for simulations and analyses of the Image Navigation and Registration (INR) system, and compares the characteristics of Image Motion Compensation (IMC) algorithms for the INR system. According to the orbit errors and attitude
Externí odkaz:
https://doaj.org/article/d373b717de154a7caee61e0f7dc9dc1a
Publikováno v:
Journal of Astronomy and Space Sciences, Vol 21, Iss 3, Pp 209-220 (2004)
Some methods have been presented to get optimal formation trajectories in the step of configuration or reconfiguration, which subject to constraints of collision avoidance and final configuration. In this study, a method for optimal formation traject
Externí odkaz:
https://doaj.org/article/2f7bc92504cb45928fd894de25b92570
Publikováno v:
Journal of Astronomy and Space Sciences, Vol 20, Iss 4, Pp 365-374 (2003)
Satellite formation flying is currently an active area of research in the aerospace engineering. So it has been researched by various authors. In this study, a tracking controller using sliding mode techniques was designed to control a satellite for
Externí odkaz:
https://doaj.org/article/423fb87961fd411085ddc7464da7f153
Publikováno v:
Journal of Spacecraft and Rockets. 48:691-694
T HREE-AXIS magnetometer (henceforth TAM) is widely used as a component of spacecraft attitude sensors. During the launch and on-orbit period, TAM is affected by mechanical distortion, thermal gradients, and internal magnetic moment disturbance of ma
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::63c7affa9fd8d1574096720fce9635c3
https://doi.org/10.2514/1.52634
https://doi.org/10.2514/1.52634
Publikováno v:
Journal of Spacecraft and Rockets. 40:889-893
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::30e61a8d7927f12ce1344f7416a5daf6
https://doi.org/10.2514/1.2370
https://doi.org/10.2514/1.2370
Publikováno v:
Journal of Guidance, Control, and Dynamics. 22:816-822
A new output-feedback control approach for the single-axis rotational maneuver of a e exible structure by use of on‐off thrusters is discussed. The target structural model represents a large-space-structure type with relatively lownaturalfrequencie
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e3bd62d18d738ba7ba27545450af50c9
https://doi.org/10.2514/2.4483
https://doi.org/10.2514/2.4483
Publikováno v:
AIAA 5th ATIO and16th Lighter-Than-Air Sys Tech. and Balloon Systems Conferences.
This paper presents the process and results of the nonlinear system analysis and controller design for the station keeping flight of the large-scaled unmanned airship. Based on the nonlinear control techniques, the feedback linearization controller o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e75bcff740a1eac852d1b878eaae202
https://doi.org/10.2514/6.2005-7343
https://doi.org/10.2514/6.2005-7343
Publikováno v:
AIAA Guidance, Navigation, and Control Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4df3f99a784f929a77dc44b14c79a5b1
https://doi.org/10.2514/6.2005-5946
https://doi.org/10.2514/6.2005-5946
Autor:
Jung-ho Kim, Dae-woo Lee, Park, C.G., Hyo-choong Bang, Jong-hun Kim, Sun-young Cho, Young-il Kim, Kwang-yul Baek
Publikováno v:
2008 International Conference on Control, Automation & Systems; 2008, p2485-2488, 4p
Autor:
Eunghyun Kim, Hyo-Choong Bang
Publikováno v:
2007 International Conference on Control, Automation & Systems; 2007, p195-198, 4p