Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Gan, Qingzhong"'
Atmospheric powered descent guidance can be solved by successive convexification; however, its onboard application is impeded by the sharp increase in computation caused by nonlinear aerodynamic forces. The problem has to be converted into a sequence
Externí odkaz:
http://arxiv.org/abs/2209.04157
This paper studies the worst case iteration complexity of an infeasible interior point method (IPM) for seconder order cone programming (SOCP), which is more convenient for warmstarting compared with feasible IPMs. The method studied bases on the hom
Externí odkaz:
http://arxiv.org/abs/2205.03570
Akademický článek
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Autor:
Wang, Shenglin, Xu, Sheng, He, Haihuan, Chen, Haiyong, Gan, Qingzhong, Yang, Jiahao, Zhang, Junjie
Publikováno v:
Journal of Physics: Conference Series; Nov2023, Vol. 2662 Issue 1, p1-9, 9p
Publikováno v:
2021 36th Youth Academic Annual Conference of Chinese Association of Automation (YAC).
This paper presents an adaptive velocity pursuit guidance law considering the dynamic characteristics of the missile autopilot. The design model of the velocity pursuit guidance system in the pitch plane is firstly established, where the autopilot dy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8268431cc72977493823fcea358eeaa0
https://doi.org/10.1109/yac53711.2021.9486481
https://doi.org/10.1109/yac53711.2021.9486481
Publikováno v:
2021 36th Youth Academic Annual Conference of Chinese Association of Automation (YAC).
This paper presents an integrated guidance and control (IGC) design scheme for the semi-strapdown missiles with the terminal attack angle and the seeker field-of-view (FOV) constraints. Firstly, an IGC model in the pitch plane is established. Then, b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a9f601dbef7e39facac155fd85e79168
https://doi.org/10.1109/yac53711.2021.9486624
https://doi.org/10.1109/yac53711.2021.9486624