kriging辅助有效筛选优化(KVSO)研究多支柱飞机的最优转向策略

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
XiaZheng Shi , Hong Nie , Ming Zhang , XiWen Gui , YuTing Zheng , YuHan Xu , TianYang Hu
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引用次数: 0

摘要

在多支柱飞机(MSA)地面机动过程中,某些主起落架(mlg)需要具有与前起落架(nlg)协调的转向能力,以减小转向半径并保持稳定性。在极端情况下,不适当的MLG转向角度可能导致轮胎侧滑和潜在的飞机侧翻。本文提出了一种kriging辅助有效筛选优化(KVSO)方法,用于预测复杂约束条件下MSA的最优转向策略,确定mlg的最优协调角。该方法首先引入基于惩罚的预筛选滤波器(PBPF)机制,通过综合评估多个约束违规来选择样本,从而提高了算法的优化效率。在此基础上,提出了一种有效的基于正态分布原理的约束筛选(VCS)机制,以降低计算成本。在此基础上,提出了一种基于约束边界抽样(CBS)准则的感兴趣区域抽样代理模型更新机制。该机制对优化目标区域和约束边界都构建了高精度的代理模型,从而加速了全局优化收敛。通过两个工程实例验证了该方法的有效性。结果表明,该方法具有较高的计算效率和优化精度。该方法为mlg转向角设计提供了理论依据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Kriging-assisted valid-screening optimization (KVSO) to study optimal steering strategies for multi-struts aircraft
During ground maneuvering of multi-strut aircraft (MSA), certain main landing gears (MLGs) require steering capabilities to coordinate with the nose landing gears (NLGs) for minimizing steering radius and maintaining stability. Inappropriate MLG steering angles may lead to tire sideslip and potential aircraft rollover in extreme cases. This article presents a Kriging-assisted valid-screening optimization (KVSO) method for predicting optimal steering strategies of MSA under complex constraints, determining optimal coordination angles for the MLGs. The proposed method first introduces a penalty-based pre-screening filter (PBPF) mechanism that selects samples by comprehensively evaluating multiple constraint violations, thereby enhancing the algorithm's optimization efficiency. Subsequently, a valid constraint screening (VCS) mechanism, based on normal distribution principles, is proposed to reduce computational costs. Furthermore, a region of interest sampling surrogate model update mechanism is developed based on the constraint boundary sampling (CBS) criterion. This mechanism constructs high-precision surrogate models for both optimization objective regions and constraint boundaries, thus accelerating global optimization convergence. The effectiveness of the proposed method is validated through two engineering case studies. The results demonstrate superior computational efficiency and optimization accuracy in resolving the optimal steering strategy for MSA. This method provides theoretical foundations for MLGs steering angle design.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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