A model for the nonlinear dynamics of a subminiature rotorcraft is established.
建立了超小型旋翼機(jī)系統(tǒng)的非線性參數(shù)化模型.
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The output tracking control design of the rotorcraft based on nonlinear inverse dynamics was described.
采用非線性逆動力學(xué)設(shè)計(jì)了輸出跟蹤控制器.
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