Optimal design of hybrid rocket motor for sub-orbital vehicle based on improved particle swarm optimization
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Optimal design of hybrid rocket motor for sub-orbital vehicle based on improved particle swarm optimization
Vol. 26, Issue 9, (2011)
作者机构:
北京航空航天大学 宇航学院,北京,100191
作者简介:
基金信息:
DOI:
CLC:
Published:2011
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CHI Yuan-cheng, ZHU Hao, FANG Jie, et al. Optimal design of hybrid rocket motor for sub-orbital vehicle based on improved particle swarm optimization[J]. 2011, 26(9).
DOI:
CHI Yuan-cheng, ZHU Hao, FANG Jie, et al. Optimal design of hybrid rocket motor for sub-orbital vehicle based on improved particle swarm optimization[J]. 2011, 26(9).DOI:
Optimal design of hybrid rocket motor for sub-orbital vehicle based on improved particle swarm optimization
called as dynamic target particle swarm optimization (DTPSO)
was proposed to use dynamic target strategy for solving complex multi-dimensional optimization problems by analyzing the position between individual particles
personal best and global best.As a specific example
the DTPSO was applied to the optimal design for hybrid rocket for a certain hybrid rocket motor of sub-orbital vehicle.The optimization results show that algorithm has strong search capability
and can also reach convergence rapidly and solve such problem effectively.All those can provide a theoretical reference for the research of sub-orbital vehicle engine's optimal design.