Zobrazeno 1 - 10
of 183
pro vyhledávání: '"Ziyang Zhen"'
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2021, Vol. 93, Issue 4, pp. 642-650.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-11-2020-0244
Publikováno v:
Drones, Vol 6, Iss 10, p 271 (2022)
The effectiveness of multiple UAVs at attacking the enemy target and defending against the attacking UAVs simultaneously gained researchers’ attention due to their cost efficiency and high mission success rates. This paper explores the UAV swarm vs
Externí odkaz:
https://doaj.org/article/e8684c2820cd4b638f4606de1339dd4b
Publikováno v:
IEEE Access, Vol 7, Pp 181273-181283 (2019)
This paper studies an automatic carrier landing control problem of fixed-wing aircraft with system uncertainties under the airwake and deck motion disturbances. A robust preview control scheme and an autoregressive (AR) model prediction scheme are or
Externí odkaz:
https://doaj.org/article/d1675b7933184e5da9f3afbab7721ae0
Publikováno v:
IEEE Access, Vol 7, Pp 154121-154130 (2019)
In this paper, the robust adaptive control scheme based on backstepping technique is presented that improves the trajectory tracking performance of the quadrotor unmanned aerial vehicles (UAVs), specially tasked for supply, rescue and combat missions
Externí odkaz:
https://doaj.org/article/e5ea8b7d1dee4c95933556ff25a40f3f
Publikováno v:
International Journal of Advanced Robotic Systems, Vol 17 (2020)
The multi-weapon multi-target assignment is always an unavoidable problem in military field. It does make sense to find a proper assignment of weapons to targets which may help maximize the attack effect. In this article, as the information achieved
Externí odkaz:
https://doaj.org/article/c4dbadf495614e259423f88d636e70d8
Publikováno v:
International Journal of Robust and Nonlinear Control. 32:7336-7347
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::31ef7265d60e4fb013fa0479e440fe47
https://doi.org/10.1002/rnc.6232
https://doi.org/10.1002/rnc.6232
Publikováno v:
Aircraft Engineering and Aerospace Technology.
Purpose Accurate glide path tracking is vital to the automatic carrier landing task of unmanned aerial vehicle (UAV). The purpose of this paper is to develop a reliable flight controller that can simultaneously deal with external disturbance, structu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4ac4f09b583f05d136826e76d8bca0f5
https://doi.org/10.1108/aeat-02-2023-0047
https://doi.org/10.1108/aeat-02-2023-0047
Publikováno v:
Advances in Space Research.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5b502c3e9b5a3240809559c12f983c4e
https://doi.org/10.1016/j.asr.2023.03.007
https://doi.org/10.1016/j.asr.2023.03.007
Publikováno v:
Nonlinear Dynamics. 108:3505-3528
The main goal of this study was to create a robust control system that could guide or replace the pilots in tracking of commanded velocity and attitude in multimodal maneuver, while complex dynamics and uncertain aerodynamic cross-coupling among cont
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d6ecc2385e2c5db172060d3b1399e343
https://doi.org/10.1007/s11071-022-07382-x
https://doi.org/10.1007/s11071-022-07382-x
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 236:2235-2253
A composite control scheme based on a disturbance observer is presented in this paper to deal with the attitude control problem of flexible spacecraft. Specifically, a sliding mode disturbance observer (SMDO) is developed to attenuate the unmodeled s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4ae76391782af2a98434f291500701e0
https://doi.org/10.1177/09544100211055318
https://doi.org/10.1177/09544100211055318