运载火箭设计与轨迹优化的仿生计算

S. Sundaram, Hai-Jun Rong, N. Sundararajan
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引用次数: 5

摘要

本文提出了一种基于仿生计算算法和非线性规划的运载火箭设计和轨迹优化工具。目标是确定运载火箭的尺寸,使有效载荷与升力重量比最大化(即发射重量最小)。在此,采用粒子群优化(PSO)方法求解分期问题。利用实数编码遗传算法(RCGA)和直接射击法求解非线性规划(NLP),得到了该飞行器的最优轨迹。利用PSO和RCGA的解对NLP变量进行初始化。通过一个案例研究,证明了该方法的优越性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Bio-inspired computing for launch vehicle design and trajectory optimization
This paper presents an optimization tool for launch vehicle design and trajectory optimization using bio-inspired computing algorithms and nonlinear programming. The objective is to size a launch vehicle such that the payload to lift-of-weight ratio is maximized (i.e the lift off weight is a minimum). Here, the staging problem is solved using Particle Swarm Optimization (PSO) method. With the above vehicle, an optimal trajectory is arrived at using a Real-Coded Genetic Algorithm (RCGA) and solving a nonlinear programming (NLP) by the direct shooting method. The solutions from PSO and RCGA are used for initialization of NLP variables. A case study is carried out that establishes the advantage of the proposed approach.
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