General Dynamic Modeling of a Scissor Structure for its Deployment Control in Space
General Dynamic Modeling of a Scissor Structure for its Deployment Control in Space
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DOI：
10.1260/0266-3511.30.3-4.245
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发表时间：
2015-12
影响因子：
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通讯作者：
Masao Takatsuka
中科院分区：
文献类型：
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作者：
Masao Takatsuka
针对空间可展翼形结构这一无边界不稳定结构，通过对其动力学模型的推广，预测其展开运动与驱动器输入力矩之间的关系，给出了一种动力学计算方法。目的是研究未来太阳能卫星等空间结构的建造过程。鉴于我们以前的研究表明了一个特定的推导序列的优势方程的剪刀单位，本文件显示了广义推导序列及其数值计算的例子，更广泛的分析模型。
The objective of the present study is to reveal a dynamic calculation method for a deployable scissor structure in space as an unstable structure without boundaries, by generalizing its dynamic modeling to predict the relationship between its deployment motion and input moment generated by an actuator. The purpose is to study the construction process of space structures such as a solar power satellite in future. Whereas our previous study demonstrated a specific derivation sequence of a dominant equation of a scissors unit, the present paper shows the generalized derivation sequence and its numerical calculation examples of more extended analysis models.