Open AccessStudy on the optimization of missile take off mass and its influence on aerodynamic parameters
Author(s) -
Jun Li,
Qi Wei,
H.R. Gong,
Yang Zhang
Publication year - 2020
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1600/1/012054
Subject(s) - missile , takeoff , aerodynamics , computer science , quality (philosophy) , process (computing) , engineering design process , engineering , aerospace engineering , control theory (sociology) , mathematical optimization , mathematics , control (management) , mechanical engineering , artificial intelligence , philosophy , epistemology , operating system
Aiming at the problem of optimal design of take-off quality in the process of missile overall design, on the basis of establishing the optimization model of missile take-off quality, three different optimization algorithms are used to optimize the calculation of missile take-off quality, by comparing the effects of the three algorithms on the takeoff mass optimization and aerodynamic parameters, the models and algorithms for different types of missiles are obtained.