Description and Estimation of Unsteady Aerodynamic Forces for Application to Elastic Aircraft

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作者
Cui Pingyuan Wu Yaohua Huang Wenhu (School of Astronautics)
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Estimation; unsteady aerodynamic forces; elastic aircraft;
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<正> In this paper, Duhamel's integral of the indicial function is used to describe unsteady aerodynamic forces. An identification method to estimate the aerodynamic forces is proposed for elastic aircraft by the maximum likelihood algorithm with estimated sensi tivities. A numerical example is given and the calculated results show the effectiveness of this method.
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页码:77 / 83
页数:7
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