Aerodynamic/Power Integrated Optimization of the Sounding Rocket Based on the Sequential Approximate Optimization
HUANG Hao
PENG Ke
WU Ze-ping
JIANG Zhen-yu
ZHANG Wei-hua
Abstract：Aimed at a certain type of a single stage solid sounding rocket,traj ectory,power and aerodynam-ic models are established in this paper.Taking the maximum height of rocket theory traj ectory peak as op-timization goal,the aerodynamic/power integrated optimization are realized by using the method of se-quential approximate optimization to obtain a set of better parameters in conception design.In the whole process of optimization,the number of times for shifting model is less and the convergence is quick in ve-locity.
Keywords：sounding rocketssequential approximate optimizationoptimization of overall parameters
Publication Date：2014-01-01
Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)
Pages：5( 17-21 )