首页> 外文会议>4th IFAC(International Federation of Automatic Control) Symposium; Jun 25-27, 2003; Milan, Italy >A NONSMOOTH, NONCONVEX OPTIMIZATION APPROACH TO ROBUST STABILIZATION BY STATIC OUTPUT FEEDBACK AND LOW-ORDER CONTROLLERS
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A NONSMOOTH, NONCONVEX OPTIMIZATION APPROACH TO ROBUST STABILIZATION BY STATIC OUTPUT FEEDBACK AND LOW-ORDER CONTROLLERS

机译:通过静态输出反馈和低阶控制器进行鲁棒镇定的非光滑非凸优化方法

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Stabilization by static output feedback (SOF) is a long-standing open problem in control: given an n by n matrix A and rectangular matrices B and C, find a p by q matrix K such that A + BKC is stable. Low-order controller design is a practically important problem that can be cast in the same framework, with (p+k)(q+k) design parameters instead of pq, where k is the order of the controller, and k n. Robust stabilization further demands stability in the presence of perturbation and satisfactory transient as well as asymptotic system response. We formulate two related nonsmooth, nonconvex optimization problems over K, respectively with the following objectives: minimization of the ε-pseudospectral abscissa of A + BKC, for a fixed ε ≥ 0, and maximization of the complex stability radius of A + BKC. Finding global optimizers of these functions is hard, so we use a recently developed gradient sampling method that approximates local optimizers. For modest-sized systems, local optimization can be carried out from a large number of starting points with no difficulty. The best local optimizers may then be investigated as candidate solutions to the static output feedback or low-order controller design problem. We show results for two problems published in the control literature. The first is a turbo-generator example that allows us to show how different choices of the optimization objective lead to stabilization with qualitatively different properties, conveniently visualized by pseudospectral plots. The second is a well known model of a Boeing 767 aircraft at a flutter condition. For this problem, we are not aware of any SOF stabilizing K published in the literature. Our method was not only able to find an SOF stabilizing K, but also to locally optimize the complex stability radius of A + BKC. We also found locally optimizing order-1 and order-2 controllers for this problem. All optimizers are visualized using pseudospectral plots.
机译:静态输出反馈(SOF)的稳定是控制中一个长期存在的开放问题:给定n×n矩阵A和矩形矩阵B和C,找到p×q矩阵K,使得A + BKC稳定。低阶控制器设计是一个实际重要的问题,可以在同一框架中使用(p + k)(q + k)设计参数代替pq进行浇铸,其中k是控制器的阶数,而k << n 。鲁棒的稳定还要求在存在扰动和令人满意的瞬态以及渐近系统响应的情况下具有稳定性。我们分别针对K制定了两个相关的非光滑,非凸优化问题,其目标如下:对于固定ε≥0,最小化A + BKC的ε-伪谱横坐标,以及最大化A + BKC的复稳定半径。寻找这些功能的全局优化器很困难,因此我们使用了最近开发的近似本地优化器的梯度采样方法。对于中等规模的系统,可以毫无困难地从大量起点进行局部优化。然后可以研究最佳的本地优化器,作为静态输出反馈或低阶控制器设计问题的候选解决方案。我们显示了控制文献中发布的两个问题的结果。第一个是涡轮发电机示例,通过该示例,我们可以显示优化目标的不同选择如何导致具有本质上不同的属性的稳定化,可以通过伪光谱图方便地对其进行可视化。第二个是在颤动条件下的波音767飞机的众所周知的模型。对于此问题,我们不知道文献中有任何SOF稳定K的信息。我们的方法不仅能够找到稳定SOF的K,而且能够局部优化A + BKC的复数稳定半径。我们还发现针对此问题在本地优化了order-1和order-2控制器。所有优化器均使用伪光谱图可视化。

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