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Combined structures-controls optimization of lattice trusses

机译:组合结构-晶格桁架的控制优化

摘要

The role that distributed parameter model can play in CSI is demonstrated, in particular in combined structures controls optimization problems of importance in preliminary design. Closed form solutions can be obtained for performance criteria such as rms attitude error, making possible analytical solutions of the optimization problem. This is in contrast to the need for numerical computer solution involving the inversion of large matrices in traditional finite element model (FEM) use. Another advantage of the analytic solution is that it can provide much needed insight into phenomena that can otherwise be obscured or difficult to discern from numerical computer results. As a compromise in level of complexity between a toy lab model and a real space structure, the lattice truss used in the EPS (Earth Pointing Satellite) was chosen. The optimization problem chosen is a generic one: of minimizing the structure mass subject to a specified stability margin and to a specified upper bond on the rms attitude error, using a co-located controller and sensors. Standard FEM treating each bar as a truss element is used, while the continuum model is anisotropic Timoshenko beam model. Performance criteria are derived for each model, except that for the distributed parameter model, explicit closed form solutions was obtained. Numerical results obtained by the two model show complete agreement.
机译:展示了分布式参数模型可以在CSI中发挥的作用,特别是在组合结构控制中,优化设计在初步设计中很重要。可以针对诸如rms姿态误差之类的性能标准获得封闭式解决方案,从而可以对优化问题进行解析。这与在传统的有限元模型(FEM)使用中涉及对大矩阵求逆的数值计算机解决方案的需求形成了对比。解析解决方案的另一个优点是,它可以提供对现象的急需的洞察力,否则这些现象可能会从数字计算机结果中被掩盖或难以辨别。作为在玩具实验室模型和真实空间结构之间的复杂程度的折衷,选择了EPS(地球指向卫星)中使用的格子桁架。所选择的优化问题是一个通用的问题:使用位于同一位置的控制器和传感器,使结构质量最小化,该结构化质量受规定的稳定性裕度和均方根姿态误差的规定的上限约束。使用将每个钢筋视为桁架元素的标准FEM,而连续体模型是各向异性的Timoshenko梁模型。为每个模型导出性能标准,除了为分布式参数模型获得显式封闭形式的解决方案。通过两个模型获得的数值结果表明完全吻合。

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  • 作者

    Balakrishnan A. V.;

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  • 年度 1991
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