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.

互联网

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.

互联网

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.

互联网

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.

互联网