Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Xingju LU"'
Publikováno v:
水下无人系统学报, Vol 32, Iss 3, Pp 396-410 (2024)
Unmanned aerial-undersea vehicles(UAUVs), with broad application prospects in both military and civilian fields, have gradually become a research hotspot in the field of robotics in recent years. UAUVs were taken as the research object in this study,
Externí odkaz:
https://doaj.org/article/410a5143b7504bf8b6eafbdc656c9ed3
Publikováno v:
Aerospace, Vol 8, Iss 5, p 144 (2021)
Fast and accurate threat evaluation (TE) of incoming air targets has a great influence on air defense. In this paper, two new generalized intuitionistic fuzzy soft set (GIFSS) methods are proposed for threat evaluation of air targets. Firstly, the th
Externí odkaz:
https://doaj.org/article/5cdec2c5523043e789bd30a2c138b6d7
Publikováno v:
International Journal of Aerospace Engineering, Vol 2013 (2013)
Externí odkaz:
https://doaj.org/article/f6fac892c91a4948860efbf492691d0d
Publikováno v:
Nonlinear Dynamics. 96:2307-2326
This paper proposes a new nonlinear system identification method in time domain for a small-scale flybarless unmanned helicopter based on an adaptive differential evolution algorithm. By analyzing and processing the real input and output data, a nonl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c3dcfe4f354474c6c7bae7dcafaba5b9
https://doi.org/10.1007/s11071-019-04923-9
https://doi.org/10.1007/s11071-019-04923-9
Publikováno v:
2021 40th Chinese Control Conference (CCC).
In this paper, a backstepping-based adaptive neural network control scheme is proposed for a small coaxial rotor unmanned aerial vehicle (CRUAV). Firstly, the mathematical dynamic model of the CRUAV is established and the state space expression of th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::59ff86a7147df43bf37be3a177222109
https://doi.org/10.23919/ccc52363.2021.9549615
https://doi.org/10.23919/ccc52363.2021.9549615
Publikováno v:
2020 4th CAA International Conference on Vehicular Control and Intelligence (CVCI).
In this paper, we focus on a self-adaptive network reconstruction problem in a distributed multi-agent system. In this system, the relationship among agents forms a complex network, in which each agent plays two roles, task execution and communicatio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fc1f2d3b93f390951ea207d52e75db7b
https://doi.org/10.1109/cvci51460.2020.9338641
https://doi.org/10.1109/cvci51460.2020.9338641
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science. 229:1839-1860
A comprehensive mathematical model of a coaxial helicopter’s swashplate mechanism is established, analyzed and verified in this paper. The mechanism widely used in helicopters to manipulate blade pitch angles is complex because of its configuration
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::39d774da457b3563c62b297b7e5e5530
https://doi.org/10.1177/0954406214547402
https://doi.org/10.1177/0954406214547402
Publikováno v:
International Journal of Aerospace Engineering, Vol 2013 (2013)
This paper presents the development of a small-scale unmanned aerial vehicle (UAV) helicopter system based on a Raptor 90 hobby helicopter. Firstly, onboard avionics system and ground station are designed carefully. The onboard avionics system mainly
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1407082dbc69d5ef2e1f811f5d05f1f9
https://doi.org/10.1155/2013/524856
https://doi.org/10.1155/2013/524856
Publikováno v:
ECC
This paper investigates the reliable tracking problem against helicopter actuator impairment under different trimming points with parameters uncertainty. First, the model of actuator faults is presented. Then a reliable robust tracking controller des
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d060e1b710e660889d0aa67e8caa6e5b
https://doi.org/10.23919/ecc.2009.7075003
https://doi.org/10.23919/ecc.2009.7075003
Publikováno v:
ECC
An adaptive retrofit fault-tolerant control algorithm against actuator faults suitable for flight control applications is developed in this paper which is based on the linear matrix inequalities (LMI) approach and adaptive approach. The algorithm is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4d70c2cafb03b2b70c2b6f74a3700577
https://doi.org/10.23919/ecc.2009.7074646
https://doi.org/10.23919/ecc.2009.7074646