悬停状态 meaning in Chinese
hover position
Examples
- System identification of the yaw model for a hovering micro helicopter
悬停状态下微型直升机航向模型的系统辨识 - The rotor / wing aerodynamic interactions of the tilt rotor vehicle in hover is described in this dissertation
本文主要研究的是倾转旋翼飞行器悬停状态时，旋翼机翼之间的气动干扰问题。 - The button has a bitmap for the unpushed state , the hover state when the mouse moves over the button , and the pushed state
按钮具有未按下状态、悬停状态（当鼠标移动到按钮上时）和按下状态的位图。 - Finally , an iterative method coupled between rotor free wake model and lifting wing panel model is given . by the method , the aerodynamic interaction of the rotor on its wing for tilt - rotor aircraft in hover are computed and discussed
最后，建立了一个耦合的旋翼机翼气动干扰分析方法，计算分析了悬停状态旋翼流场对机翼的气动干扰影响。 - The modern unmanned helicopter flight control system is generally composed of the flight control computer , the servo driving mechanism , the sensor , and the ground monitor control system etc . in this thesis the research to the helicopter flight characteristics was conducted at first , and its flight dynamic model was preliminary discussed , especially the mathematic model under hung - stop condition was formulated and the algorithm of the controller was designed in detail
现代无人直升机飞行控制系统一般由飞行控制计算机、伺服驱动机构、传感器、地面监测控制等分系统组成。本文首先对直升机的飞行特性进行了研究,并且对飞行动力数学模型做了初步探讨,尤其对在悬停状态下的数学模型做了较为详尽的公式推导和控制器的算法设计。