Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Supeng Zhu"'
Publikováno v:
IEEE Access, Vol 7, Pp 104330-104343 (2019)
The small unmanned aerial vehicles are susceptible to wind disturbances due to the turbulent environment at their low operational altitude. Compared to conventional IMU output, the phase-advanced information provided by angular acceleration measureme
Externí odkaz:
https://doaj.org/article/bfeb740935da48609f05f036db54ec6d
Publikováno v:
Sensors, Vol 18, Iss 10, p 3233 (2018)
Inspired by the exceptional flight ability of birds and insects, a bio-inspired neural adaptive flight control structure of a small unmanned aerial vehicle was presented. Eight pressure sensors were elaborately installed in the leading-edge area of t
Externí odkaz:
https://doaj.org/article/a880f02ac59b403fa7c17350cacabda2
Publikováno v:
ISA Transactions. 129:257-270
This paper proposes a prescribed-time cooperative guidance law (PTCGL) against maneuvering target with variable line-of-sight (LOS) angle constraint for leader-following missiles, where the convergence times of the state errors can be arbitrarily set
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0ebb1a3b7ec77b8b960125834fdfa615
https://doi.org/10.1016/j.isatra.2022.02.043
https://doi.org/10.1016/j.isatra.2022.02.043
Publikováno v:
International Journal of Aeronautical and Space Sciences.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::462cb2bf0981744e0584c6ce1ebedacf
https://doi.org/10.1007/s42405-022-00563-3
https://doi.org/10.1007/s42405-022-00563-3
Publikováno v:
European Journal of Control. 58:17-26
This paper addresses the finite time prescribed performance control problem for hypersonic flight vehicle systems with abrupt actuator faults and time-varying uncertainties. The considered actuator faults contains abrupt gain faults and saltatorial b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0c148d0b6687dee1c82d1f381ae9f52d
https://doi.org/10.1016/j.ejcon.2020.12.003
https://doi.org/10.1016/j.ejcon.2020.12.003
Publikováno v:
IEEE Access, Vol 7, Pp 104330-104343 (2019)
The small unmanned aerial vehicles are susceptible to wind disturbances due to the turbulent environment at their low operational altitude. Compared to conventional IMU output, the phase-advanced information provided by angular acceleration measureme
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::67845e4270fce01a1698ec41fc06a6a1
https://doi.org/10.1109/access.2019.2931646
https://doi.org/10.1109/access.2019.2931646
Publikováno v:
Mathematical Problems in Engineering, Vol 2020 (2020)
The problem of integrated fault detection and fault tolerant control for switched systems with asynchronous switching is focused on in this paper. Based on the switched model, the inherent asynchronous switching is taken into consideration. The async
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::07270032efaf0535b112c59b3aeaf4ab
Publikováno v:
Aerospace Science and Technology. 111:106469
This paper proposes a novel output constrained non-affine control structure by combining backstepping adaptive control with coordinate transformation technique for Generic Hypersonic Vehicles (GHVs) attitude tracking problem suffering from stochastic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c858115b46207641ea227867215eaea4
https://doi.org/10.1016/j.ast.2020.106469
https://doi.org/10.1016/j.ast.2020.106469
Publikováno v:
2015 2nd International Conference on Opto-Electronics and Applied Optics (IEM OPTRONIX).
The light field imaging produces the information on the direction of light ray, therefore the refocusing of the raw image shot with the light field camera can acquire high-resolution images of objects at different distances. This paper presents the l
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::916aa1ff5e0c4a93c2a91c62c0d92849
https://doi.org/10.1109/optronix.2015.7345517
https://doi.org/10.1109/optronix.2015.7345517
Autor:
Wenxing Fu, Supeng Zhu
Publikováno v:
2012 Second International Conference on Intelligent System Design and Engineering Application.
The stratosail has the tensile force of the tether but no engine thrust and the size and direction of the tensile force is constantly changing. Also the changes in the size and direction of wind speed have direct influence on the aerodynamic force an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e4d882a768c75a548b9b171c4c5d8073
https://doi.org/10.1109/isdea.2012.454
https://doi.org/10.1109/isdea.2012.454