Zobrazeno 1 - 10
of 17
pro vyhledávání: '"Qing-Lei Hu"'
Publikováno v:
Acta Automatica Sinica. 38:462-468
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aa00a777306b80c0c1bc9c0b89b68820
https://doi.org/10.3724/sp.j.1004.2012.00462
https://doi.org/10.3724/sp.j.1004.2012.00462
Publikováno v:
The Journal of China Universities of Posts and Telecommunications. 19:35-44
This paper presents a distributed and adaptive fluctuation control scheme for many-to-one routing (FCM) in wireless sensor networks. Unlike well-known topology control schemes, the primary design objective is to reduce the fluctuation which happens d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e44246e8bb3daf55b75e20c0d1edd822
https://doi.org/10.1016/s1005-8885(11)60316-6
https://doi.org/10.1016/s1005-8885(11)60316-6
Publikováno v:
Chinese Journal of Aeronautics. 25(3):406-415
This paper deals with the problem of cooperative attitude tracking with time-varying communication delays as well as the delays between inter-synchronization control parts and self-tracking control parts in the spacecraft formation flying. First, we
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3f2a3691f5ea21e4a66d0e82c16ce8b4
Autor:
Qing-lei Hu, Guang-fu Ma
Publikováno v:
Asian Journal of Control. 9:20-29
This paper presents a dual-stage control system design method for the rotational maneuver and vibration stabilization of a spacecraft with flexible appendages. In this design approach, attitude control system and vibration suppression were designed s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::449fe7c8315e64a2d869551336afb76c
https://doi.org/10.1111/j.1934-6093.2007.tb00300.x
https://doi.org/10.1111/j.1934-6093.2007.tb00300.x
Publikováno v:
2012 24th Chinese Control and Decision Conference (CCDC).
The reaction wheels (RWs) play an important role in conducting spacecraft attitude control commands, and redundant RWs are dominantly configurated for spacecraft missions to ensure the pointing accuracy and reliability. In this work, firstly, for the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2198a17e8895b34c6d490ebe6e07659c
https://doi.org/10.1109/ccdc.2012.6243002
https://doi.org/10.1109/ccdc.2012.6243002
Publikováno v:
2008 International Conference on Machine Learning and Cybernetics.
A robust control approach is presented for the attitude maneuvering control and vibration damping of a spacecraft with flexible appendages. Firstly, a fuzzy logic system is used to approximate the unknown dynamics of the spacecraft system. A new atti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3af63bf929684506ffd42ba0f37ec8dc
https://doi.org/10.1109/icmlc.2008.4620730
https://doi.org/10.1109/icmlc.2008.4620730
Publikováno v:
2007 2nd IEEE Conference on Industrial Electronics and Applications.
Even the multiple support vector machine (SVM) ensemble has been proved to improve the classification performance greatly than a single SVM, the classification result of the practically implemented SVM is often far from the theoretically expected lev
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f441591f98ea6d8d444c2ba9cc497db1
https://doi.org/10.1109/iciea.2007.4318607
https://doi.org/10.1109/iciea.2007.4318607
Publikováno v:
Proceedings of the 2003 International Conference on Machine Learning and Cybernetics (IEEE Cat. No.03EX693).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d2f0f55a63dfed96a0f359cade7ba26d
https://doi.org/10.1109/icmlc.2003.1259635
https://doi.org/10.1109/icmlc.2003.1259635
Publikováno v:
26th Chinese Control & Decision Conference (2014 CCDC); 2014, p3130-3135, 6p
Publikováno v:
2013 25th Chinese Control & Decision Conference (CCDC); 2013, p1913-1917, 5p