摘要
针对现代航天器往往具有大型挠性附件以及步进电机常作为其主要驱动系统的特点 ,对分力合成主动振动抑制方法进行了讨论 ,建立了相应的数学模型 ,对步进电机驱动挠性结构时产生的振动以及挠性振动对刚体运动的影响进行了分析 ,提出了应用分力合成方法的驱动方式。数值仿真和实验均验证了该方法的正确性。
Considering the large flexibility in modern spacecraft and stepping motors are often used to drive the flexible appendages, in this paper, we discuss the active vibration suppression method with component synthesis. The corresponding mathematics model was built and the analysis of flexible vibration caused by different driving strategies of stepping motor and its influence on rigid attitude were done. A novel driving strategy using component synthesis method was proposed. Both numerical simulation and experiment validate this new method.
出处
《上海航天》
2001年第3期8-14,共7页
Aerospace Shanghai
