姿态控制器的英文
attitude controller
例句与用法
- Firstly , the basic control structure is presented
给出了卫星姿态控制器的基本形式。 - To solve this problem , we propose an output feedback control law without angular velocities by making use of the inherent passivity of the attitude control system
针对这种情况，本文利用刚体姿态控制系统中固有的无源性，设计了无需角速率测量值的刚体姿态控制器。 - The attitude control system design and its control effect are affected greatly by mass - property parameters of satellite , which can change on - orbit as fuel is expended , the configuration changes , or payloads are added or removed
卫星质量特性对姿态控制器设计及控制效果有着很大的影响。在轨运行过程中,由于质量消耗等原因会导致卫星转动惯量及质心位置的变化,实现卫星质量特性的在线辨识能够有效提高姿态控制精度。 - In order to provide a basic and effective practical engineering tool for handling quality planning , analysing and evaluating , which is needed hi helicopter prototype development , this research work is launched on the fundation of comprehending the new aeronautical standard of united states army - ads - 33 , and has obtained the achievements as following : ( 1 ) performance definition of pcs according to the criteria requirements for an explicit helicopter , beginning at analysis of its missions . ( 2 ) establishment of a helicopter attitude controller , which can meet the criteria requirements , by using the technology of adaptive neural network model - inverse control ; implementation of two response types ( rts ) and two control modes ; evaluation of quantitative parameters according to the ads - 33 . ( 3 ) establishment of a helicopter trajectory contoller based on the attitude controller ; simulations of mission task elements ( mtes ) and evaluation of handling quality
为了给型号研制中飞行品质的规划、分析和评价提供基本的、有效的工程实用工具，本课题在充分消化理解美军新航标ads - 33的基础上，作了以下工作： ( 1 )针对具体直升机，从任务分析入手，根据规范要求确定对飞控系统的要求； ( 2 )应用自适应神经网络模型逆控制技术，构造了能够满足飞行品质要求的直升机姿态控制器，实现了两种响应型式、两种控制模式，并根据ads - 33进行了定量指标评估； ( 3 )在姿态控制器的基础上，构造了轨迹跟踪器，进行了任务科目基元仿真和飞行品质评估。 - To overcome this problem , the author researching from the core of active disturbance rejection control theory " fal function " , having the advantage of : small errors , large gains ; big error , the small gains character , designs a nonlinear pid gesture controller . simulation results showed that the design of nonlinear pid controller shortening the small satellite gesture catch time and improving the attitude control precision
为了克服这个问题,本文从自抗扰控制理论中的核心“ fal函数”出发,基于fal ( e , , )函数具有:小误差,大增益;大误差,小增益的特性,设计了一种非线性pid姿态控制器,比较好的缩短了小卫星姿态捕获时间,一定程度上提高了姿态控制的精度。
