Finding multiple local solutions to optimal control problems via saddle points and its application to the ascent trajectory of a winged rocket

T. Fujikawa, K. Yonemoto
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引用次数: 0

Abstract

Complex nonlinear optimal control problems can have more than a single local solution due to the lack of convexity, and widely-used gradient-based approaches for optimal control have a risk of producing an inferior local solution. Although global optimization methods for optimal control may overcome this difficulty, such existing methods suffer from high computational complexities. This paper presents a novel numerical algorithm for multi-modal optimal control problems based on a saddle-point search method. Starting from an already-found local solution, a saddle-point search algorithm finds a surrounding saddle point of the constrained optimization problem, from which a new local solution is obtained by applying a gradient-based optimizer. By repeating this procedure, multiple locally optimal solutions are explored exhaustively and systematically. Although the developed method is not rigorously guaranteed to produce the global solution, it is applicable to large-scale general optimal control problems with equality and inequality constraints, which makes it a practically beneficial technique. After numerical experiments with an example problem, the ascent trajectory optimization problem of a winged rocket for maximizing apogee altitude is solved by using the proposed method.
鞍点最优控制问题的多局部解及其在有翼火箭上升弹道中的应用
由于缺乏凸性,复杂的非线性最优控制问题可能有多个局部解,而广泛使用的基于梯度的最优控制方法有产生劣局部解的风险。虽然最优控制的全局优化方法可以克服这一困难,但现有的方法具有较高的计算复杂度。提出了一种基于鞍点搜索的多模态最优控制算法。鞍点搜索算法从已有的局部解出发,寻找约束优化问题的周围鞍点,并在此鞍点上应用基于梯度的优化器得到新的局部解。通过重复这一过程,详尽而系统地探索了多个局部最优解。虽然所提出的方法不能严格保证产生全局解,但它适用于具有等式和不等式约束的大规模一般最优控制问题,是一种实用的技术。通过一个算例问题的数值实验,用该方法求解了带翼火箭最大远地点高度的上升弹道优化问题。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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CiteScore
1.20
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