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Optimization and Sizing for Propulsion System of Liquid Rocket Using Genetic Algorithm
作者姓名:Saqlain  Akhtar  He  Lin-shu
作者单位:School of
摘    要:Flight vehicle conceptual design appears to be a promising area for application of the Genetic Algorithm (GA) as an approach to help to automate part of the design process. This computational research effort strives to develop a propulsion system design strategy for liquid rocket to optimize take-off mass, satisfying the mission range under the constraint of axial overload. The method by which this process is accomplished by using GA as optimizer is outlined in this paper. Convergence of GA is improved by introducing initial population based on Design of Experiments Technique.

关 键 词:遗传分析  推进系统  液压系统  航空技术
收稿时间:16 January 2006
修稿时间:2006-01-162006-06-20

Optimization and Sizing for Propulsion System of Liquid Rocket Using Genetic Algorithm
Saqlain Akhtar He Lin-shu.Optimization and Sizing for Propulsion System of Liquid Rocket Using Genetic Algorithm[J].Chinese Journal of Aeronautics,2007,20(1):40-46.
Authors:Saqlain Akhtar  He Lin-shu
Institution:School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:Flight vehicle conceptual design appears to be a promising area for application of the Genetic Algorithm (GA) as an approach to help to automate part of the design process. This computational research effort strives to develop a propulsion system design strategy for liquid rocket to optimize take-off mass, satisfying the mission range under the constraint of axial overload. The method by which this process is accomplished by using GA as optimizer is outlined in this paper. Convergence of GA is improved by introducing initial population based on Design of Experiments Technique.
Keywords:liquid rocket  propulsion system  genetic algorithm  design of experiments  Genetic Algorithm  Rocket  Liquid  Propulsion System  Convergence  improved  initial  population  based  Design of Experiments  Technique  method  process  optimizer  paper  range  constraint  axial  overload  computational
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