- 相關推薦
Optimization and Sizing for Propulsion System of Liquid Rocket Using Genetic Algorithm
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.
作 者： Saqlain Akhtar He Lin-shu 作者單位： School of Astronautics, Beijing University of 4eronautics and Astronautics, Beijing 100083, China 刊 名： 中國航空學報（英文版） ISTIC 英文刊名： CHINESE JOURNAL OF AERONAUTICS 年，卷(期)： 2007 20(1) 分類號： V2 關鍵詞： liquid rocket propulsion system genetic algorithm design of experiments【Optimization and Sizing for Propulsi】相關文章：
Apical-dominant particle swarm optimization04-26
Optimization of solid fermentation of cellulase from Trichoderma koningii04-25
Optimization of enrichment processes of pentachlorophenol (PCP) from water samples04-26
Optimization of measurement distance of 109Cd K XRF system for obese subjects04-27