As a part of a study of the estimation of aircraft aerodynamic characteristics using dynamic wind tunnel tests, cable mount dynamic wind tunnel tests were executed from 1989. Maximum likelihood estimation algorithm is applied to the test data, and low speed aerodynamic parameters are estimated. The basic performance of the algorithm is evaluated by comparing it to other estimation algorithm.
最尤推定法によるNALスペースプレーン空力パラメータの動的風洞試験での推定
naltr01307.pdf
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