介绍了反作用飞轮力矩模式反馈补偿控制系统的设计。
In this paper, the design of a feedback compensation control system for reaction wheel of torque mode is introduced.
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。
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。
Reaction wheel is one of the main disturbance sources that affect the precision of attitude control system of spacecraft.
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。
The results of simulation show that the gondola control system achieves the desired results.
作为一种高精度的执行机构，反作用飞轮已广泛应用于卫星姿态控制系统中。
As a kind of high accuracy executive machine, reaction wheel has been extensively applied to the attitude control system (ACS) of satellites.
进一步的设计了反作用飞轮电机力矩的快速控制规律。给出了机动时间和系统状态的简单计算公式。
The time-optimal control law for motor torques of reaction wheels is designed, and, the calculated formulations of maneuver time and system state are given.
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。
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.
本文对反作用飞轮及其控制器进行了探讨，提出并设计了一种新型的反作用飞轮，能很好地满足多种要求。
This thesis would study and design a rw and its controller, and put forward a new pattern rw which can meet various requirements.
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。
Reaction wheel is one of the main disturbance sources that affect the precision of attitude control system of spacecraft.
提出了用直流力矩电动机在反作用飞轮控制方式下对气球吊篮的方位控制，从理论上研究了气球吊篮方位控制系统。
The nacelle azimuth control of DC torque motor under the reaction flywheel control mode is presented, and the nacelle azimuth control system is investigated in theory.
为对磁悬浮反作用飞轮的剩磁矩(RMM)进行分析及最小化设计，提出一种基于等效磁偶极子模型的剩磁矩计算方法。
To analyze and minimally design the remnant magnetic moment (RMM) for a magnetically suspended reaction flywheel, a method based on the equivalent magnetic dipole model is proposed.
设计了由PW M脉宽调制技术构建的工作在速率控制模式下的反作用飞轮控制系统，并对其硬件电路进行了具体实现。
The reaction flywheel control system was designed by using PWM technology under the velocity control mode, and the hardware circuit was also set up.
最后，该文设计了一个基于PC机的三轴稳定卫星姿态控制硬件在回路仿真系统，将反作用飞轮、陀螺等实物接入仿真系统。
At last, the hardware in the loop simulation system for three-axis stabilized satellite attitude control based on PC, with reaction wheel and gyro in the loop is designed.
该系统实现了气球吊篮方位的动态控制，提升了反作用飞轮控制方式的控制特性和系统的控制品质，提高了系统的精度和可靠性。
A dynamic nacelle azimuth control is realized. Its control performance and quality are enhanced under the reaction flywheel control. High precision and reliability was obtained.
变惯量反作用飞轮是一种新型的动量交换装置，不仅可以通过改变飞轮转速输出力矩，还可以通过改变其转动惯量实现大范围的力矩输出。
VIRW is a new momentum exchange device, which can provide attitude control torque not only by adjusting the spin rate, but also by changing the inertia of the wheel.
针对大惯量反作用飞轮系统中的关键技术进行了研究，提出了一套基于数字IP内核集成的硬件实现方案，可以解决飞轮控制中普遍存在的一些问题。
This paper presents a hardware design scheme of torque control for the large inertia retroaction flywheel based on a fully digitized system level integration of IP cores.
针对大惯量反作用飞轮系统中的关键技术进行了研究，提出了一套基于数字IP内核集成的硬件实现方案，可以解决飞轮控制中普遍存在的一些问题。
This paper presents a hardware design scheme of torque control for the large inertia retroaction flywheel based on a fully digitized system level integration of IP cores.
应用推荐