Z
Zixuan Liang
Researcher at Beijing Institute of Technology
Publications - 80
Citations - 477
Zixuan Liang is an academic researcher from Beijing Institute of Technology. The author has contributed to research in topics: Trajectory & Computer science. The author has an hindex of 10, co-authored 69 publications receiving 336 citations. Previous affiliations of Zixuan Liang include Beihang University & Chinese Ministry of Education.
Papers
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Optimum tooling design for resin transfer molding with virtual manufacturing and artificial intelligence
TL;DR: In this paper, a neural network is trained to create a rapid RTM process model and genetic algorithms are applied to this model to search for the optimum solution to the problem of tooling design.
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Distributed cooperative guidance for multiple missiles with fixed and switching communication topologies
TL;DR: In this article, a two-step guidance strategy is proposed to realize the simultaneous attack for multiple missiles with fixed and switching directed communication topologies, where a distributed cooperative guidance law is designed using local neighboring information for multiple targets to achieve consensus on range-to-go and leading angle.
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Distributed group cooperative guidance for multiple missiles with fixed and switching directed communication topologies
TL;DR: In this article, a distributed group cooperative guidance (DGCG) problem for multiple missiles with fixed and switching directed communication topologies is dealt with, and a two-step guidance strategy is developed.
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Waypoint constrained guidance for entry vehicles
TL;DR: A guidance algorithm for the waypoint constrained atmospheric entry is presented and results show that the conventional path constraint, the terminal constraint and the additional waypoint constraint are well satisfied, which indicates the effectiveness of the proposed guidance algorithm.
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Lateral entry guidance with no-fly zone constraint
TL;DR: Two lateral guidance methods are presented for the entry flight constrained by multiple no-fly zones using a dynamic heading corridor to control the vehicle's velocity heading angle and results indicate that these methods are effective for no- fly zone avoidance missions in both the nominal and dispersed cases.