Zobrazeno 1 - 10
of 49
pro vyhledávání: '"Dai, Xunhua"'
This paper presents an open-source dataset RflyMAD, a Multicopter Abnomal Dataset developed by Reliable Flight Control (Rfly) Group aiming to promote the development of research fields like fault detection and isolation (FDI) or health assessment (HA
Externí odkaz:
http://arxiv.org/abs/2311.11340
This paper presents a lifting-wing multirotor UAV that allows long-range flight. The UAV features a lifting wing in a special mounting angle that works together with rotors to supply lift when it flies forward, achieving a reduction in energy consump
Externí odkaz:
http://arxiv.org/abs/2006.15579
The traditional multicopter design method usually requires a long iterative process to find the optimal design based on given performance requirements. The method is uneconomical and inefficient. In this paper, a practical method is proposed to autom
Externí odkaz:
http://arxiv.org/abs/1908.06301
Control systems on unmanned vehicles are safety-critical systems whose requirements on reliability and safety are ever-increasing. Currently, testing a complex autonomous control system is an expensive and time-consuming process, which requires massi
Externí odkaz:
http://arxiv.org/abs/1908.02704
Electronic control systems are becoming more and more complicated, which makes it difficult to test them sufficiently only through experiments. Simulation is an efficient way in the development and testing of complex electronic systems, but the simul
Externí odkaz:
http://arxiv.org/abs/1907.03981
Akademický článek
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Publikováno v:
IEEE/ASME Transactions on Mechatronics, 2019, 24: 228-239
Multicopters are becoming increasingly important in both civil and military fields. Currently, most multicopter propulsion systems are designed by experience and trial-and-error experiments, which are costly and ineffective. This paper proposes a sim
Externí odkaz:
http://arxiv.org/abs/1809.02472
Publikováno v:
Journal of Guidance, Control, and Dynamics, Vol. 41, No. 7 (2018), pp. 1577-1584
This paper studies the model of the probe-drogue aerial refueling system under aerodynamic disturbances, and proposes a docking control method based on terminal iterative learning control to compensate for the docking errors caused by aerodynamic dis
Externí odkaz:
http://arxiv.org/abs/1803.00247
Publikováno v:
In Aerospace Science and Technology July 2021 114
Akademický článek
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