用诱饵角色情景防御拦截器:有限时间合作制导方法

IF 1 4区 工程技术 Q3 ENGINEERING, AEROSPACE
Yang Guo, Shuai Zhang, Shaobo Wang, Shicheng Wang, Zhiguo Liu
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引用次数: 0

摘要

研究重点是多机协同拦截机动目标的问题。为有效节约拦截所需成本,考虑了不同角色的协同制导方案,提出了基于有限时间有界条件下 H2 准则性能指标的协同制导方法。首先,基于相对运动方程和一阶动力学特性建立了协同拦截模型。其次,通过考虑系统状态和输出的有限时间稳定性特征,推导出有限时间约束条件下系统 H2 准则性能合成的充分条件。然后,在有限时间约束条件下,基于 H2 准则性能指标合成方法设计了一种具有引诱作用的协同引导方法。所提出的方法能确保防御者满足输出有限时间收敛特性,且能耗较小。此外,中间状态不超过预定限值,有效节省了引导过程中拦截所需的过载。此外,还通过仿真实验验证了所提方法的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Defending an interceptor with lure role scenario: A finite-time cooperative guidance method
The problem of multi-aircraft cooperative intercepting maneuvering targets is focused in the study. To effectively save the required cost of interception, a cooperative guidance scheme with different roles is considered, and a cooperative guidance method is proposed based on H2 norm performance index under finite-time boundedness conditions. First, a cooperative interception model is established based on the relative motion equation and first-order dynamics characteristics. Second, by considering the system state and finite-time stability characteristics of the output, sufficient conditions for the synthesis of the H2 norm performance of the system under the finite-time bounded conditions are derived. Then, under the finite-time boundedness conditions, a cooperative guidance method with lure roles is designed based on the H2 norm performance index synthesis method. The proposed method can ensure that the defender satisfies the output finite-time convergence characteristic with a small energy consumption. Furthermore, the intermediate state does not exceed the predetermined limit value and effectively saves the overload required for interception during the guidance process. Additionally, simulation experiments are conducted to verify the effectiveness of the proposed method.
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来源期刊
CiteScore
2.40
自引率
18.20%
发文量
212
审稿时长
5.7 months
期刊介绍: The Journal of Aerospace Engineering is dedicated to the publication of high quality research in all branches of applied sciences and technology dealing with aircraft and spacecraft, and their support systems. "Our authorship is truly international and all efforts are made to ensure that each paper is presented in the best possible way and reaches a wide audience. "The Editorial Board is composed of recognized experts representing the technical communities of fifteen countries. The Board Members work in close cooperation with the editors, reviewers, and authors to achieve a consistent standard of well written and presented papers."Professor Rodrigo Martinez-Val, Universidad Politécnica de Madrid, Spain This journal is a member of the Committee on Publication Ethics (COPE).
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