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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.

Active Publication Date: 2022-08-02
CALCULATION AERODYNAMICS INST CHINA AERODYNAMICS RES & DEV CENT
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Problems solved by technology

However, in this literature, the Cholesky decomposition method is used to solve the linear equations in LS-SVM. When the sample size is large, there is also the problem that the coefficient matrix A has a singular value and the training algorithm cannot be performed.

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  • ls-svm modeling method for nonlinear unsteady aerodynamic characteristics of missiles

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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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Abstract

The invention relates to a LS-SVM modeling method for nonlinear unsteady aerodynamic characteristics of a missile. The method decomposes the missile aerodynamic force into the sum of static aerodynamic force and aerodynamic force increments generated by dynamic motion, and adopts the LS-SVM modeling method to establish dynamic aerodynamic force. Dynamic incremental model, in which the motion history is approximately described with finite sampling points to reflect the influence of the motion history on aerodynamic characteristics; the linear equations of LS-SVM are solved by singular value decomposition method, and the model is trained; the training-verification method is used to determine Penalty factor and kernel width to improve the generalization performance of the LS‑SVM model. The purpose is to provide an aerodynamic modeling method for missile maneuvering at high angle of attack based on machine learning.

Description

technical field [0001] The invention belongs to the technical field of aerodynamics, and in particular relates to a LS-SVM modeling method for missile nonlinear unsteady aerodynamic characteristics. Background technique [0002] High angle of attack maneuverability is an important design indicator of modern tactical missiles. Especially for air-launched missiles, the use of large angle of attack maneuvers to achieve over-the-shoulder launch can greatly shorten the combat response time, improve the survival probability of the carrier aircraft and the missile combat effectiveness. Regardless of whether it is a traditional over-the-shoulder launch or a new type of self-flipping over-shoulder launch, the missile will experience a large angle of attack and a stall state, and the aerodynamic force exhibits highly unsteady and strong nonlinear characteristics. At this time, the aerodynamic derivative model based on the quasi-steady assumption is no longer applicable, and a nonline...

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Application Information

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IPC IPC(8): G06F30/27G06F17/12G06N20/10G06F119/14
CPCG06F30/27G06F17/12G06N20/10G06F2119/14
Inventor 孔轶男汪清陈功余婧王波兰伍彬钱炜祺段光强
Owner CALCULATION AERODYNAMICS INST CHINA AERODYNAMICS RES & DEV CENT
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