1) reaction wheel control mode
反作用飞轮控制方式
1.
In order to increase the precision of reaction wheels mode in azimuth control,acquired in the present paper is a project of reaction wheel control about azimuth control of nacelle,with the consideration of speed friction torque,via analyses and application of the emulator torque mode and speed mode in the reaction wheel control mode about the azimuth control of nacelle system.
为了提高反作用飞轮控制方式的吊篮方位控制的灵敏度和控制精度,考虑飞轮摩擦力矩的情况下,对反作用飞轮控制方式的力矩模式和速率模式进行理论分析与实际应用比较,选取了高空气球吊篮方位控制的反作用飞轮控制的速率模式。
2) reaction wheel control
反作用轮控制
3) Reaction wheel
反作用飞轮
1.
Then,the spacecraft large-angle maneuver controller,which is based on the reaction wheels,is designed by using the control algorithm of variable structure control.
讨论了空间飞行器大角度机动控制实验平台的实现方法,并给出了硬件系统原理框图和软件的设计流程图;采用变结构控制算法,设计了基于反作用飞轮的大角度姿态机动控制器,并进行了不同角度下的闭环姿态机动控制实验,实验结果验证了该实验平台设计的可行性,对空间飞行器大角度姿态机动的研究提供了一个较好的实验平台。
2.
Reaction wheel is an important executive component of satellite attitude control system,and the improvement of flywheel system is spurred by high performance satellite attitude control system.
反作用飞轮是卫星姿态控制系统的重要执行元件,提高飞轮系统的性能对卫星姿态控制系统具有重要意义。
3.
A reaction wheel model of the satellite is employed.
最后引入卫星反作用飞轮模型,对单飞轮发生故障的情况进行了仿真,结果表明提出的方法有效、可行。
4) reaction flywheel
反作用飞轮
1.
DC torque motor under the reaction flywheel control mode was used in nacelle azimuth control in this paper.
实现了用直流力矩电机在反作用飞轮控制方式下对气球吊篮的方位控制。
2.
The controller using reaction flywheel on the SABGT is designed and then computer simulation is obtained.
用反作用飞轮作为控制执行机构，设计了控制器，进行了相关的计算机仿真。
3.
According to the feature that large-angle attitude maneuver control is nonlinear, strong coupled and includes uncertain parameters, simulation and experiments are taken for the nonlinear design method of large-angle attitude maneuver control system based on reaction flywheel by using the Lyapunov theory, the variable structure control theory for nonlinear systems and.
针对大角度机动控制具有非线性、强耦合及不确定性等特点,应用李亚普诺夫理论、非线性系统变结构控制理论及逆动态解耦理论,对基于反作用飞轮的大角度姿态机动控制系统的非线性设计方法进行仿真和实验研究。
5) reaction-wheel
反作用飞轮
1.
of the flywheel operation device,the outline parameters of a reaction-wheel structure was designed dynamically optimum to satisfy the requirements that are as follows:(1) to ensure the reaction-wheel to arrive at an angle momentum level at designed angle velocity;(2)to ensure the reaction-wheel structure to satisfy the requirements of strength, stiffness, shape, size, etc.
在综合考虑飞轮执行机构的动量容量、输出力矩、质量、体积、功耗、成本及复杂性等因素的基础上,基于优化设计软件ISIGHT及结构有限元分析软件ANSYS,对基于磁悬浮轴承技术的反作用飞轮的结构外形尺寸进行动态优化设计,在确保反作用飞轮结构在给定设计转速下能达到一定的角动量,同时满足结构强度、刚度、形态等方面的要求的前提下,使反作用飞轮的质量最小,优化结果令人满意。
6) reaction wheel failure
反作用飞轮故障
补充资料：作用与反作用定律
即“牛顿第三定律”(879页)。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条