Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Mingle Deng"'
Publikováno v:
Acta Mechanica Sinica. 37:1696-1713
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c316aa68701260072023382b2d44087a
https://doi.org/10.1007/s10409-021-01138-3
https://doi.org/10.1007/s10409-021-01138-3
Publikováno v:
Applied Mathematics and Mechanics. 41:753-768
The Chebyshev spectral variational integrator (CSVI) is presented in this paper. Spectral methods have aroused great interest in approximating numerically a smooth problem for their attractive geometric convergence rates. The geometric numerical meth
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::15de3c74ae4a7cf40f3a06d044d02227
https://doi.org/10.1007/s10483-020-2602-8
https://doi.org/10.1007/s10483-020-2602-8
Autor:
Baozeng Yue, Mingle Deng
Publikováno v:
Acta Mechanica Sinica. 33:1095-1102
This paper is focused on attitude tracking control of a spacecraft that is equipped with flexible appendage and partially filled liquid propellant tank. The large amplitude liquid slosh is included by using a moving pulsating ball model that is furth
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::913dcbff1b0fefd2cd9d58c84a635243
https://doi.org/10.1007/s10409-017-0700-9
https://doi.org/10.1007/s10409-017-0700-9
Autor:
Baozeng Yue, Mingle Deng
Publikováno v:
Acta Astronautica. 133:111-120
This paper is focused on the nonlinearly modelling and attitude dynamics of spacecraft coupled with large amplitude liquid sloshing dynamics and flexible appendage vibration. The large amplitude fuel slosh dynamics is included by using an improved mo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a3e4f1acd9b91a82379ad29587812ff4
https://doi.org/10.1016/j.actaastro.2017.01.003
https://doi.org/10.1016/j.actaastro.2017.01.003
Publikováno v:
Journal of Aerospace Engineering. 32
This paper discusses the coupling dynamics behavior of spacecraft equipped with flexible appendages and liquid propellant tanks. The moving pulsating ball model (MPBM) is used to imitate la...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0fd9825fd8702d3f223fc94a80c5aac5
https://doi.org/10.1061/(asce)as.1943-5525.0001070
https://doi.org/10.1061/(asce)as.1943-5525.0001070
Publikováno v:
Journal of Aerospace Engineering. 30
This paper is focused on the position and attitude control of spacecraft with multiple liquid propellant tanks, while considering large amplitude propellant slosh and depletion. The large a...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cb6054fd1d552dc893e2caa6c3e1a67f
https://doi.org/10.1061/(asce)as.1943-5525.0000785
https://doi.org/10.1061/(asce)as.1943-5525.0000785
Publikováno v:
Journal of Sound and Vibration. 460:114907
The problems of large-amplitude lateral sloshing, rotary sloshing and liquid rotation-starting in liquid-filled spacecraft remain of great concern to aerospace engineers. A composite 3DOF-rigid-pendulum model is proposed in this paper for nonlinear l
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9fd6a142fa8efea930418bde6f229d47
https://doi.org/10.1016/j.jsv.2019.114907
https://doi.org/10.1016/j.jsv.2019.114907
Autor:
Baozeng Yue, Mingle Deng
Publikováno v:
Journal of Aerospace Engineering. 29
This paper focuses on the dynamics and control of spacecraft with multiple liquid propellant tanks. The liquid slosh dynamics are included by using an improved moving pulsating ball model. The moving pulsating ball model is an equivalent mechanical m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f17aeda3ed7e17221a317a9e9b0d0bcc
https://doi.org/10.1061/(asce)as.1943-5525.0000636
https://doi.org/10.1061/(asce)as.1943-5525.0000636
Autor:
Mingle Deng, Baozeng Yue
Publikováno v:
Journal of Aerospace Engineering; Nov2016, Vol. 29 Issue 6, p4016042-1-4016042-11, 11p