摘要
把遗传算法与最大似然法相结合 ,形成了一种基于遗传算法的动力学系统辨识方法 ,并以某轴对称战术导弹的非线性气动力参数仿真辨识为例 ,利用仿真技术 ,检验了该方法的实用性和有效性。结果表明 。
A Method of dynamic system identification based on genetic algorithms is put forward through combining genetic algorithm with maximum likelihood method, and nonlinear aerodynamic parameter identification of missile using simulation data is carried out to verify the validity and feasibility of the formed method. The identification results are satisfactory, which shows the maximum likelihood method based genetic algorithm is effective for dynamic system identification.
出处
《飞行力学》
CSCD
2003年第2期56-58,共3页
Flight Dynamics
