PARAMETRIC OPTIMIZATION AND STRUCTURAL DESIGN OF NLS

来源 :Transactions of Nanjing University of Aeronautics & Astronau | 被引量 : 0次 | 上传用户:hebeihuazi
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A physical and mathematical model is developed for describing nitrogen launching system(NLS)based on the dynamics of pneumatics and mechanisms.The multi objective optimization function for the pitching angle and velocity of a missile was proposed for the first time.Singularity detection of wavelet analysis was conducted to find the optimum iteration points in a new direct algorithm of non linear programming.Comparison between wavelet optimization and complex method show that the former is better for optimization design. A physical and mathematical model is developed for Nail launching system (NLS) based on the dynamics of pneumatics and mechanisms. The multi objective optimization function for the pitching angle and velocity of a missile was proposed for the first time. Singularity detection of wavelet analysis was conducted to find the optimum iteration points in a new direct algorithm of non linear programming. Comparison between wavelet optimization and complex method show that the former is better for optimization design.
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