Zobrazeno 1 - 10
of 59
pro vyhledávání: '"Shuxing Yang"'
Publikováno v:
PLoS ONE, Vol 15, Iss 1, p e0226021 (2020)
Alzheimer's Disease (AD) is a devastating neurodegenerative disorder currently affecting 45 million people worldwide, ranking as the 6th highest cause of death. Throughout the development and progression of AD, over 90% of patients display behavioral
Externí odkaz:
https://doaj.org/article/065bebfd558b418a95565c0fd536e821
Publikováno v:
International Journal of Computational Intelligence Systems, Vol 4, Iss 6 (2011)
State-dependent Riccati equation (SDRE) techniques are rapidly emerging as general design methods for nonlinear controllers. A nonlinear optimal guidance law with impact angle constraint is derived for planar engagements to attack stationary targets.
Externí odkaz:
https://doaj.org/article/99211e2ec597485c9a242a40326bb3fd
Autor:
Kai Li, Wei Mao, Junzhuo Zhou, Boyu Li, Zhengke Yang, Shuxing Yang, Laimin Du, Sixiao Huang, Hao Yu
Publikováno v:
IEEE Transactions on Circuits and Systems II: Express Briefs. 69:4123-4127
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::13c731388815a09989ac7cac269923b6
https://doi.org/10.1109/tcsii.2022.3183007
https://doi.org/10.1109/tcsii.2022.3183007
Publikováno v:
Chinese Journal of Aeronautics, Vol 33, Iss 10, Pp 2707-2715 (2020)
Roll-isolation is an effective way for spinning vehicle to greatly reduce the roll gyro range of strapdown Inertial Navigation System (SINS) and increase the accuracy of inertial navigation. However, during a recent flight test, the roll-isolated con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::48f8d186e65ac5d6e9b91f3f3efce87a
https://doi.org/10.1016/j.cja.2019.08.026
https://doi.org/10.1016/j.cja.2019.08.026
Publikováno v:
In Chinese Journal of Aeronautics June 2010 23(3):312-319
Publikováno v:
Aerospace Science and Technology. 92:314-325
The polynomial chaos (PC) theory and direct collocation method have been integrated to solve a lot of robust trajectory optimization problems. However, the computational cost and memory consumption increase significantly with the increase of the dime
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2edca9e85940df9b5702e6a9fa3fc963
https://doi.org/10.1016/j.ast.2019.06.011
https://doi.org/10.1016/j.ast.2019.06.011
Publikováno v:
Nonlinear Dynamics. 97:2739-2756
To predict the coning motion forms of a rolling projectile with configurational asymmetries, the nonlinear characteristics for the system are investigated in this paper. The nonlinear dynamic model of rolling projectiles in coning motion is built by
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::00791c47b53af3a78508d68d468e675a
https://doi.org/10.1007/s11071-019-05159-3
https://doi.org/10.1007/s11071-019-05159-3
Publikováno v:
Chinese Journal of Aeronautics, Vol 32, Iss 8, Pp 1933-1945 (2019)
To perform an accurate fire-and-forget attack of seeker-less missile with the consideration of the localization error, a new cooperative guidance strategy of multi-missiles is proposed in this work. Firstly, an estimated position of the seeker-less m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d01be110ba3dbabf7a1e9a0059d07ae6
https://doi.org/10.1016/j.cja.2019.03.005
https://doi.org/10.1016/j.cja.2019.03.005
Publikováno v:
Aerospace Science and Technology. 88:308-315
Based on the centralized leader-follower framework, a novel cooperative guidance strategy is proposed to implement the fire-and-forget attacks of seeker-less missiles in which the motion information of a maneuvering target and the strict requirement
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6f594ba0233a2d0973e59aee4c84556e
https://doi.org/10.1016/j.ast.2019.03.036
https://doi.org/10.1016/j.ast.2019.03.036
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 233:4800-4809
A sequential convex programming algorithm is proposed to solve the complex ascent trajectory optimization problems for guided rockets in this paper. Due to the nonlinear dynamics and constraints, especially, the nonlinear thrust terms and aerodynamic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a0f542d8fc052985dcaf465e02e6e2fa
https://doi.org/10.1177/0954410019830268
https://doi.org/10.1177/0954410019830268