reaction wheel control

As a kind of high accuracy executive machine, reaction wheel has been extensively applied to the attitude control system ( ACS) of satellites.

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。

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Aimed at the initial attitude capture, a combined control algorithm for the magnetorquer and reaction wheel has been adopted.

针对小卫星入轨阶段的姿态捕获控制，提出了一种使用磁力矩器和反作用飞轮进行联合控制的算法。

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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.

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。

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In this paper, the design of a feedback compensation control system for reaction wheel of torque mode is introduced.

介绍了反作用飞轮力矩模式反馈补偿控制系统的设计。

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Speed Mode Nonlinear Synergetic Control Approach for Magnetically Suspended Reaction Wheel

磁悬浮反作用飞轮速率模式非线性协同控制方法

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Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft.

反作用轮是影响航天器姿态控制系统精度的主要扰动源之一。

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Based on the project of Reaction wheel control system, the design and realization of circuit and controller for flywheel is described and the flywheel control system is deeply and systemically researched in this thesis.

本文以飞轮控制系统实际研发项目为背景，设计实现了一套反作用飞轮控制器，并对飞轮控制进行了系统而深入的研究。

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The Design of Torque Mode Control for Reaction Wheel System

反作用飞轮力矩模式控制系统设计

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The character of one-degree of freedom of reaction wheel makes the amount of associated duplicated functional components and attendant redundancy increase in multi-wheel configuration for three-axis attitude control system, consequently the mass, volume, power and cost of attitude control system increase greatly.

航天器三轴姿态控制常用的多飞轮控制方案中，反作用飞轮的单自由度动量交换属性使系统的功能重复部件和冗余件数目增多，严重影响了姿控系统的重量、体积、功耗及成本；

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Research and simulation experiments based on nonlinear control method of the satellite attitude large-angle maneuver based on reaction wheel are studied in this paper.

本文对基于反作用飞轮的卫星大角度姿态机动控制系统的非线性方法进行了研究和实验仿真。

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