ls-svm modeling method for nonlinear unsteady aerodynamic characteristics of missiles
A technology of LS-SVM and aerodynamic characteristics, applied in the field of aerodynamics, it can solve the problems such as the inability of the training algorithm and the numerical singularity of the coefficient matrix A, so as to achieve the effect of improving the generalization performance, improving the robustness and avoiding adverse effects.
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[0070] In order to make the objectives, technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below with reference to the embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention.
[0071] The invention develops a nonlinear unsteady aerodynamic modeling method based on least squares support vector machine (LS-SVM) for the problem of maneuvering aerodynamic modeling of missiles with large attack angles.
[0072] (1) Unsteady aerodynamic LS-SVM model
[0073] In the angle of attack plane, missile aerodynamic forces and moments are nonlinear functions of Mach number, angle of attack, pitch rate, and pitch angle. Using the superposition principle, the aerodynamic force is decomposed into the sum of the aerodynamic force generated by the static aerodynamic force and the dynamic motion, namely:
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