Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Bangsheng Fu"'
Publikováno v:
Scientific Reports, Vol 11, Iss 1, Pp 1-14 (2021)
Abstract With the application of advanced composite materials in High-Aspect-Ratio wings (HARW), the randomness of structural parameters, such as elastic modulus and Poisson's ratio, is enhanced. Hence, in order to explore the whole picture of aeroel
Externí odkaz:
https://doaj.org/article/77c6bdfe43c74670a08ace1901108a62
Publikováno v:
IEEE Access, Vol 7, Pp 4453-4465 (2019)
In this paper, based on the advantages of Newtonian mechanics method, mixed coordinate method, and analytical mechanics method, the dynamic model of rigid-aeroelasticity-sloshing coupling is established for longitudinal vibration and liquid fuel slos
Externí odkaz:
https://doaj.org/article/d3c7658a3c024ce686aae7ed6efc1a57
Publikováno v:
Actuators, Vol 11, Iss 9, p 265 (2022)
Friction nonlinearity, which is common in electromechanical actuator (EMA) systems, leads to undesired dynamic responses such as “flat top”, low-speed crawl, which brings challenges to high precision attitude control of flight vehicles. In order
Externí odkaz:
https://doaj.org/article/160acd5c5faf4c6a8fe8d8cc3d8928d0
Publikováno v:
Journal of Physics: Conference Series. 2355:012021
As an electromechanical drive system, nonlinear factors are unavoidable in electromechanical actuator (EMA). In this paper, elasticity of shaft and backlash nonlinearity are considered in the model, the effects of elasticity and backlash on EMA are a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6ec23c62124eeb478c45bd99febe8d2c
https://doi.org/10.1088/1742-6596/2355/1/012021
https://doi.org/10.1088/1742-6596/2355/1/012021
Publikováno v:
Journal of Aerospace Engineering. 34
The control of aeroelastic response of a wing section with influence of the fuel sloshing in external tank is examined through analytical studies. Based on the simplified mass-spring-damper...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c787cdba43efe204b8a717133271efd4
https://doi.org/10.1061/(asce)as.1943-5525.0001274
https://doi.org/10.1061/(asce)as.1943-5525.0001274
Publikováno v:
Scientific Reports
Scientific Reports, Vol 11, Iss 1, Pp 1-14 (2021)
Scientific Reports, Vol 11, Iss 1, Pp 1-14 (2021)
With the application of advanced composite materials in High-Aspect-Ratio wings (HARW), the randomness of structural parameters, such as elastic modulus and Poisson's ratio, is enhanced. Hence, in order to explore the whole picture of aeroelastic pro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b2dfe128fba6e0087e3b75d037b0c9c9
http://europepmc.org/articles/PMC8329216
http://europepmc.org/articles/PMC8329216
Publikováno v:
Aircraft Engineering and Aerospace Technology. 91:1257-1267
Purpose Regarding the important roles of accuracy and robustness of tightly-coupled micro inertial measurement unit (MIMU)/global navigation satellite system (GNSS) for unmanned aerial vehicle (UAV). This study aims to explore the efficient method to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::690dcc3268ac7db8beefd1b8f943b136
https://doi.org/10.1108/aeat-07-2018-0211
https://doi.org/10.1108/aeat-07-2018-0211
Publikováno v:
Optik. 179:1140-1151
For high speed vehicles, the dimensions of the observed information from the sensors are not always appropriate, and the quality of the information differs. To enhance the accuracy of the terminal autonomous navigation for high speed vehicle, A check
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ac65fb0dfeba3f4e467a46f53b47ecc4
https://doi.org/10.1016/j.ijleo.2018.10.141
https://doi.org/10.1016/j.ijleo.2018.10.141
Publikováno v:
IEEE Access, Vol 7, Pp 4453-4465 (2019)
In this paper, based on the advantages of Newtonian mechanics method, mixed coordinate method, and analytical mechanics method, the dynamic model of rigid-aeroelasticity-sloshing coupling is established for longitudinal vibration and liquid fuel slos
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6cf0a1652476fdcb3e8d785fd4404f92
https://doi.org/10.1109/access.2018.2884544
https://doi.org/10.1109/access.2018.2884544
Publikováno v:
2020 3rd International Conference on Unmanned Systems (ICUS).
Since the missile dynamical system in the pitch plane is nonlinear, uncertain and non-matched, its integrated guidance and control is nontrivial. In order to cope with this problem, an adaptive back-stepping based sliding mode control algorithm is pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4124e53ec2961e7beeac073fbc74a2a2
https://doi.org/10.1109/icus50048.2020.9274893
https://doi.org/10.1109/icus50048.2020.9274893