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Optimization Design of Missile Take-off Mass Based on Differential Evolution Algorithm.
- Source :
- Transactions of Beijing Institute of Technology; 2011, Vol. 31 Issue 11, p1270-1272, 3p
- Publication Year :
- 2011
-
Abstract
- The optimization algorithm was developed to calculate the take-off mass more efficiently and accurately, and the missile take-off mass design method based on differential evolution was proposed. The take-off mass of the missile with single-chamber dual-thrust motor was set as the example for optimization design. The design variables and constraints were set up, and the model to optimize take-off mass was established. The parameters of population size and the maximum evolutionary generation were determined according to the optimization model. Finally, the minimum take-off mass was obtained via continuous iterations. Compared with genetic algorithms, differential evolution algorithm demonstrates its faster convergence and more computational accuracy in take-off mass design of missile. [ABSTRACT FROM AUTHOR]
Details
- Language :
- Chinese
- ISSN :
- 10010645
- Volume :
- 31
- Issue :
- 11
- Database :
- Supplemental Index
- Journal :
- Transactions of Beijing Institute of Technology
- Publication Type :
- Academic Journal
- Accession number :
- 74485291