Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft. 反作用轮(RW)是影响航天器姿态控制系统精度的主要扰动源之一。
To study the problems of decoupling and eliminating precession for zero-momentum reaction wheel system, a new method to eliminate precession was put forward. 针对零动量轮卫星控制系统解耦和进动抑制问题,提出了一种新的进动抑制方案。
Effects Analysis of Reaction Wheel(RW) Disturbance on Structure Dynamics Characters of Spacecraft 反作用轮(RW)扰动对航天器结构动态特性的影响分析
Speed Mode Nonlinear Synergetic Control Approach for Magnetically Suspended Reaction Wheel(RW) 磁悬浮反作用飞轮速率模式非线性协同控制方法
Dynamic inversion based satellite attitude fault tolerant control system with reaction wheel fault 基于动态逆的卫星姿控系统飞轮故障容错控制