The received mixing signals are first mapped to high-dimensionalkernel feature space, and a feature vector basis given by the fitness function of the kernel feature space is constructed.
A kernel function method and the results of computing unsteady load on three-dimensional wings in transonic flow are presented in this paper.
本文给出了在跨音速流动中,计算三维机翼非定常载荷分布的核函数法和计算结果。
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The main idea is to approximate the classical local linear embedding (LLE) by introducing a linear transformation matrix and then find the solution in a very high dimensional space by kernel trick.