pitch control system meaning in Chinese
俯仰控制系统
Examples
- Pitch control system of controllable pitch propeller based on single - chip microcomputer
基于单片机技术的调距桨螺距控制系统 - This paper , in advantage of modern control theories , designed the pitch control system and the altitude holding system of the x armed helicopter , and present digital simulation , coupling analysis , sensitivity analysis , system performance analysis under different input and initial condition
本文应用现代控制理论设计了某型武装直升机的俯仰角控制系统和高度保持系统，并进行了数字仿真、耦合分析、飞行状态变化对控制系统性能的影响分析，及在不同输入初始条件下的系统性能分析。 - Along with development of tiltrotor vehicle ’ s research some theoretical productions have been appeared in some project ( aerodynamic behavior of rotor , kinetic behavior of rotor , rotor / wing aerodynamic interactions , etc . ) . in order to carry on further research and experimentation of these project , national - defence science and technology helicopter rotor kinetic lab of our school begin to building tiltrotor model bench . base on need of this bench , this paper study / design pitch control system on it
随着对倾转旋翼飞行器的深入研究,倾转旋翼的气动特性、动力学特性、旋翼/机身间的气动干扰等课题方面已有一定的理论成果出现。为了对这些课题进行深入研究和试验验证,我校直升机旋翼动力学国防科技重点实验室着手建造了倾转旋翼模型实验台。 - Pitch control system consist of three channels which is formed by three drive units . base on need of bench , drive system scheme is designed . single channel three - loop position servo system which is formed by linear motor is simulated . then kinetic behavior of rotor and system ’ s force coupling relation is analyzed . a compensation method for dynamic load which is caused by rotor rotation is presented base on structure - invarient theory
根据实验台的技术要求,设计了整个驱动系统方案。对由直线电机构成的单通道三环位置伺服系统进行了设计和仿真。分析了旋翼运动的动力学特性、系统力耦合关系,并根据结构不变性原理对由旋翼运动产生的动态载荷提出了补偿方法。