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Bifurcation analysis using rigorous branch and bound methods

机译:使用严格分支定界方法进行分叉分析

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For the study of nonlinear dynamic systems, it is important to locate the equilibria and bifurcations occurring within a specified computational domain. This paper proposes a new approach for solving these problems and compares it to the numerical continuation method. The new approach is based upon branch and bound and utilizes rigorous enclosure techniques to yield outer bounding sets of both the equilibrium and local bifurcation manifolds. These sets, which comprise the union of hyper-rectangles, can be made to be as tight as desired. Sufficient conditions for the existence of equilibrium and bifurcation points taking the form of algebraic inequality constraints in the state-parameter space are used to calculate their enclosures directly. The enclosures for the bifurcation sets can be computed independently of the equilibrium manifold, and are guaranteed to contain all solutions within the computational domain. A further advantage of this method is the ability to compute a near-maximally sized hyper-rectangle of high dimension centered at a fixed parameter-state point whose elements are guaranteed to exclude all bifurcation points. This hyper-rectangle, which requires a global description of the bifurcation manifold within the computational domain, cannot be obtained otherwise. A test case, based on the dynamics of a UAV subject to uncertain center of gravity location, is used to illustrate the efficacy of the method by comparing it with numerical continuation and to evaluate its computational complexity.
机译:对于非线性动力系统的研究,重要的是找到在指定计算域内发生的平衡和分支。本文提出了一种解决这些问题的新方法,并将其与数值连续法进行了比较。新方法基于分支定界,并利用严格的包围技术产生平衡和局部分支歧管的外部边界集。可以将包含超矩形并集的这些组设置为所需的紧密度。以状态-参数空间中的代数不等式约束形式存在的平衡点和分歧点的充分条件,用于直接计算它们的包围度。分支集的包围可独立于平衡歧管进行计算,并保证包含计算域内的所有解。该方法的另一个优点是能够计算以固定参数状态点为中心的高尺寸近最大尺寸的超矩形,该矩形的元素被保证可以排除所有分叉点。否则就无法获得需要在计算域内对分叉流形进行全局描述的超矩形。一个测试案例基于无人机在重心位置不确定的情况下的动力学,通过将其与数值连续性进行比较来说明该方法的有效性,并评估其计算复杂性。

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