Zobrazeno 1 - 10
of 35
pro vyhledávání: '"Cui Hu-tao"'
Publikováno v:
Journal of Materials Science & Technology. 32:1372-1377
As a new solid state welding, pinless friction stir welding (PFSW) can be used to join thin-wall structures. In this study, four new pinless tools with different groove distributions were designed and manufactured in order to enrich technological sto
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44bda857e4a47703d79829327c56f54a
https://doi.org/10.1016/j.jmst.2016.07.003
https://doi.org/10.1016/j.jmst.2016.07.003
Autor:
Wang, Yi-Ze1 wangyize@126.com, Cui, Hu-Tao1, Li, Feng-Ming2 fmli@bjut.edu.cn, Kishimoto, Kikuo3
Publikováno v:
Acta Mechanica. Jun2013, Vol. 224 Issue 6, p1299-1307. 9p. 6 Diagrams.
Publikováno v:
Journal of the Franklin Institute. 349:493-509
The variable structure control (VSC) with sliding mode is presented to design a tracking control law to ensure the fast and accurate response and robustness of guidance law in this paper. First, the small body dynamic equation is deduced in the landi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cd5a7ab713408621bde83c05419f6ed8
https://doi.org/10.1016/j.jfranklin.2011.07.007
https://doi.org/10.1016/j.jfranklin.2011.07.007
Publikováno v:
Aircraft Engineering and Aerospace Technology. 83:296-305
PurposeThe purpose of this paper is to propose an attitude control algorithm for spacecraft with geometric constraints.Design/methodology/approachThe geometric constraint is reformulated as a quadratic form when quaternion is used as attitude paramet
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0acb5d28f1e5484a8537d55defa20c6f
https://doi.org/10.1108/00022661111159906
https://doi.org/10.1108/00022661111159906
Publikováno v:
Journal of Systems Engineering and Electronics. 19:529-536
The autonomous “celestial navigation scheme” for deep space probe departing from the earth and the autonomous “optical navigation scheme” for encountering object celestial body are presented. Then, aiming at the conditions that large initial
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1aa0b4e05d76050a1f0762c78ac9f23e
https://doi.org/10.1016/s1004-4132(08)60117-6
https://doi.org/10.1016/s1004-4132(08)60117-6
Publikováno v:
2015 34th Chinese Control Conference (CCC).
This work is concerned with the minimum-fuel power descent to a prescribed landing site on a irregular-shaped asteroid. With the small and complicated gravitational field taken into account, we present the equations of spacecraft motion in the astero
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::85c175388cf2f3c7630cb338b22c087c
https://doi.org/10.1109/chicc.2015.7260437
https://doi.org/10.1109/chicc.2015.7260437
Publikováno v:
Aircraft Engineering and Aerospace Technology. 77:317-323
PurposeIn order to succeed in landing asteroids, good accuracy autonomous navigation is absolutely necessary. Aims to describe a new autonomous navigation algorithm.Design/methodology/approachFirst, gray images of asteroid surface are acquired by opt
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::40e46fcfc904f95b4e1a7fdd106ac065
https://doi.org/10.1108/00022660510606402
https://doi.org/10.1108/00022660510606402
Publikováno v:
Acta Astronautica. 54:763-771
The autonomous optical navigation and guidance algorithm for soft landing on asteroids is presented. First, the probe position relative to targeted asteroid is acquired from the image coordinates of three selected feature points (FPs) on the asteroid
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::738c6c9fdc58e203ddc239d3bea39bfa
https://doi.org/10.1016/j.actaastro.2003.09.001
https://doi.org/10.1016/j.actaastro.2003.09.001
Publikováno v:
Aircraft Engineering and Aerospace Technology. 75:365-371
Because of indeterminateness of the environment and delay of the communication, deep space spacecraft is required to be autonomous. Planning technology is studied in order to realize the spacecraft autonomy. First, a multi‐agent planning system (MA
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::65e77e24a34bcfef3b69d7a22040c397
https://doi.org/10.1108/00022660310484284
https://doi.org/10.1108/00022660310484284
Publikováno v:
2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics.
Autonomous hazard avoidance is a key technology for planetary pinpoint landing. In this paper, passive image based hazard detection and landing point selecting methods are presented. Craters on planetary surface are detected by edge detection, edge m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::11e232fc786eca713a6eba96d38f3028
https://doi.org/10.1109/isscaa.2010.5633604
https://doi.org/10.1109/isscaa.2010.5633604