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Active Control of Flow Over a Backward-Facing Step

机译:主动控制后向步骤的流量

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摘要

We describe a control-oriented model reduction process from partial differential equation (PDE) descriptions of aerodynamic flow systems, and the design of low-order feedback controllers using these procedures. An effective approach for flow model reduction for active control using balanced truncation approaches was developed. The techniques were applied to a flow control problem representative of aerospace problems: active control of flow over a modified 2D backward-facing step, which can be handled by most commercial finite element packages. Although the geometry is rather simple, the richness of the flow field is well documented. Feedback controllers were developed for disturbance rejection and tracking of the reattachment point for both high and low Reynolds numbers.
机译:我们从气动流动系统的偏微分方程(PDE)描述以及使用这些程序的低阶反馈控制器设计中描述了一种面向控制的模型简化过程。开发了一种有效的减少流量模型的主动控制方法,该方法采用了平衡截断法。该技术已应用于代表航空航天问题的流量控制问题:经过修改的2D朝后步骤的主动流量控制,可以通过大多数商业有限元程序包来处理。尽管几何形状相当简单,但是流场的丰富性已得到充分证明。开发了反馈控制器,用于抑制干扰和跟踪高雷诺数和低雷诺数的重新连接点。

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