Transition control of the blasius boundary layer using linear robust control theory

Q3 Earth and Planetary Sciences Aerospace Systems Pub Date : 2023-12-13 DOI:10.1007/s42401-023-00258-x
Christopher J. Damaren
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Abstract

The paper considers control system design for linearized three-dimensional perturbations about a nominal laminar boundary layer over a flat plate (the Blasius profile). The objective is prevention of the laminar to turbulent transition using appropriate inputs, outputs, and feedback controllers. They are synthesized with a view to reducing transient energy growth, a known precursor to important transition scenarios. The linearized Navier–Stokes equations are reduced to the Orr–Sommerfeld and Squire equations with wall-normal velocity actuation entering through the boundary conditions on the wall. The sensor output is taken to be the wall-normal derivative of the wall-normal vorticity measured on the plate. Several multivariable output controllers are examined, including simple constant gain output feedback, loop transfer recovery, and \(H_{\infty }\) loop shaping. Reduced order compensators are developed using balanced truncation and analyzed for robustness using the gap metric between reduced order models and full order models. It is demonstrated that the level of minimum transient energy growth that can be achieved is similar for these diverse controller methodologies but falls short of that which can be achieved using optimal state feedback.

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利用线性鲁棒控制理论对布拉修斯边界层进行过渡控制
本文考虑了对平板上的标称层流边界层(Blasius 剖面)进行线性化三维扰动的控制系统设计。目的是利用适当的输入、输出和反馈控制器防止层流向湍流过渡。对它们进行合成的目的是减少瞬态能量增长,而瞬态能量增长是重要过渡情况的已知前兆。线性化纳维-斯托克斯方程被简化为 Orr-Sommerfeld 和 Squire 方程,墙壁法向速度驱动通过墙壁的边界条件进入。传感器输出为在板上测量到的壁面法向涡度的壁面法向导数。研究了几种多变量输出控制器,包括简单的恒定增益输出反馈、环路传递恢复和 \(H_{\infty }\) 环路整形。使用平衡截断法开发了降阶补偿器,并使用降阶模型和全阶模型之间的差距度量法分析了其鲁棒性。结果表明,这些不同的控制器方法所能实现的最小瞬态能量增长水平是相似的,但与使用最佳状态反馈所能实现的水平相差甚远。
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来源期刊
Aerospace Systems
Aerospace Systems Social Sciences-Social Sciences (miscellaneous)
CiteScore
1.80
自引率
0.00%
发文量
53
期刊介绍: Aerospace Systems provides an international, peer-reviewed forum which focuses on system-level research and development regarding aeronautics and astronautics. The journal emphasizes the unique role and increasing importance of informatics on aerospace. It fills a gap in current publishing coverage from outer space vehicles to atmospheric vehicles by highlighting interdisciplinary science, technology and engineering. Potential topics include, but are not limited to: Trans-space vehicle systems design and integration Air vehicle systems Space vehicle systems Near-space vehicle systems Aerospace robotics and unmanned system Communication, navigation and surveillance Aerodynamics and aircraft design Dynamics and control Aerospace propulsion Avionics system Opto-electronic system Air traffic management Earth observation Deep space exploration Bionic micro-aircraft/spacecraft Intelligent sensing and Information fusion
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