飞机控制中的可达性和可控性分析

G. Călugăru, I. Reșceanu, Elena-Andreea Dănişor
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引用次数: 0

摘要

本文对多步骤飞机约束最优控制问题的可达可控集理论进行了推广。首先简要介绍了可达集和可控集理论,以及飞机多步约束最优控制问题。总共分析了4架飞机的案例(一架通用航空飞机、一架战斗机、一架公务机和一架大型商用飞机)。考虑模型的具体参数,在给定的预测范围下,确定每个时间实例的可控和可达集合,并给出了所考虑的每种机型的可控和可达集合布局的图形表示。这种对与飞机控制相关的多步约束优化问题的可达性和可控性方面的扩展,可以用于使用模型预测控制技术的飞机系统的设计和开发用例。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Reachability and controllability analysis in aircraft control
This article proposes an extension of the reachable and controllable sets theory for multi-step aircraft constrained optimal control problems. Initially, a brief overview of the reachable and controllable sets theory is provided, together with the aircraft multi-step constrained optimal control problem. In total, 4 aircraft cases are analyzed (a general aviation aircraft, a fighter jet, a business jet and a large commercial craft). Considering the specific parameters of the models and with a given prediction horizon, the controllable and reachable sets are determined for each time instance and graphical representations of their layout is provided for each type of aircraft considered. This extension of the reachability and controllability aspects for multi-step constrained optimal problems related to aircraft control can serve in use cases for the design and development of aircraft systems which also employ model predictive control techniques.
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