带状态不平等约束的奇异控制问题的间接 Bang-Singular 算法 (IBSA)

IF 2.5 3区 计算机科学 Q2 AUTOMATION & CONTROL SYSTEMS European Journal of Control Pub Date : 2024-06-29 DOI:10.1016/j.ejcon.2024.101071
Amin Jafarimoghaddam, Manuel Soler
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引用次数: 0

摘要

在本研究中,我们提出了间接 Bang-Singular 算法 (IBSA),这是一个简单明了的计算框架,用于解决各种带有状态不平等约束的奇异优化控制问题 (SOCP)。该算法是一种弧形分类技术,它将 SOCP 重新表述为一个关于切换时间的非线性编程问题,可能还包括一些其他参数,如进入奇异区间时的共态初始值。我们利用庞特里亚金最大原则推导出奇异控制反馈,并分析了多个控制同时奇异的区间的可能性。此外,我们还利用直接连接法加入了状态不平等约束。由于共态动力学的线性特性,共态变量以及奇异控制都是通过 MATLAB 的符号平台自动计算的。非线性编程的构建方式规避了在涉及以不完整状态反馈函数表示的奇异控制的更复杂情况下状态不完整约束所带来的挑战。我们还提出了几个定理,这些定理对于设计一种直接的计算方法来求解 SOCP 是不可或缺的。为了评估所提算法的有效性,我们解决了以下新问题:(1) 垂直面上时间燃料最优的商用飞机巡航飞行(即具有状态不完全约束、标量奇异控制和风切变效应),以及 (2) 垂直面上时间燃料最优的商用飞机自由航线飞行(即具有状态不完全约束、双进入奇异控制和风切变效应)。值得注意的是,我们通过一阶和二阶最优条件仔细检查了图表结果的最优性。
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The Indirect Bang-Singular Algorithm (IBSA) for singular control problems with state-inequality constraints

In this study, we present the Indirect Bang-Singular Algorithm (IBSA), a straightforward computational framework developed to solve a wide range of Singular Optimal Control Problems (SOCP) with state-inequality constraints. The algorithm is a type of arc-classification technique which reformulates the SOCP as a nonlinear programming problem over the switching times, and possibly some other parameters such as the co-states’ initial values at the entry time to a singular interval. We derive the singular control feedback using the Pontryagin’s maximum principle and analyze the possibility of an interval where multiple controls are simultaneously singular. Furthermore, we incorporate the state-inequality constraints using the direct-adjoining method. Owing to the linear property of the co-state dynamics, the co-state variables and consequently, the singular controls are computed automatically using MATLAB’s symbolic platform. The nonlinear programming is constructed in a manner to circumvent the challenges posed by state-inequality constraints in more intricate scenarios involving singular controls expressed in terms of incomplete state-feedback functions. We also present several theorems that are integral to devising a straightforward computational approach for solving SOCPs. To assess the effectiveness of the proposed algorithm, we solve the following novel problems: (1) time–fuel-optimal commercial aircraft cruise flight in a vertical plane (i.e., with state-inequality constraint, a scalar singular control, and wind shear effects), and (2) the free-routing time–fuel-optimal commercial aircraft flight in a vertical plane (i.e., with state-inequality constraint, a dual-entry singular control, and wind shear effects). Notably, the optimality of the graphed results has been carefully inspected through first and second-order optimality conditions.

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来源期刊
European Journal of Control
European Journal of Control 工程技术-自动化与控制系统
CiteScore
5.80
自引率
5.90%
发文量
131
审稿时长
1 months
期刊介绍: The European Control Association (EUCA) has among its objectives to promote the development of the discipline. Apart from the European Control Conferences, the European Journal of Control is the Association''s main channel for the dissemination of important contributions in the field. The aim of the Journal is to publish high quality papers on the theory and practice of control and systems engineering. The scope of the Journal will be wide and cover all aspects of the discipline including methodologies, techniques and applications. Research in control and systems engineering is necessary to develop new concepts and tools which enhance our understanding and improve our ability to design and implement high performance control systems. Submitted papers should stress the practical motivations and relevance of their results. The design and implementation of a successful control system requires the use of a range of techniques: Modelling Robustness Analysis Identification Optimization Control Law Design Numerical analysis Fault Detection, and so on.
期刊最新文献
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