An adaptive neural networks controller is designed for tilt rotor aircraft platform.
采用自適應神經網絡控制方法,設計出傾轉旋翼機模擬平臺姿態角控制器.
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Responses of tilt rotor to initial conditions in airplane mode were computed at typical flying speed.
計算了典型前飛速度時的系統對初始條件的響應.
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The multi - body analysis of the aeroelastic stability of the tilt rotor aircraft is presented.
通過多體動力學方法建立了傾轉旋翼機動力學分析模型.
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A complete tilt rotor aircraft flight control model was developed to enable design of rotor aircraft.
建立傾轉旋翼機數學模型是設計其合理的飛行控制律的基礎.
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