An adaptive neural networks controller is designed for tilt rotor aircraft platform.
采用自适应神经网络控制方法,设计出倾转旋翼机模拟平台姿态角控制器.
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Responses of tilt rotor to initial conditions in airplane mode were computed at typical flying speed.
计算了典型前飞速度时的系统对初始条件的响应.
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The multi - body analysis of the aeroelastic stability of the tilt rotor aircraft is presented.
通过多体动力学方法建立了倾转旋翼机动力学分析模型.
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A complete tilt rotor aircraft flight control model was developed to enable design of rotor aircraft.
建立倾转旋翼机数学模型是设计其合理的飞行控制律的基础.
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