Geometric Approach to Lateral Guidance for Reentry Vehicle

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-08-26 DOI:10.1109/TAES.2024.3449247
Xinghao Cheng;Xun Song;Sai Chen;Chaoyong Li
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Abstract

In this article, we study the lateral guidance problem for a hypersonic reentry vehicle. More specifically, we propose a geometric solution to the lateral corridor that will help to achieve a tradeoff between bank reversal frequency and corridor safety. As is well known, lateral corridor determines the boundary of bank angle and its configuration reflects the timing of reversals, and the most salient challenge is how to formulate the corridor accurately, instead of otherwise commonly used linear approximations. In particular, the proposed solution elaborated on the prediction of the crossrange-range information, and formulated the corridor as a geometric curve, which offers much improved accuracy in envelop prediction. Simulation results verified the performance of the proposed scheme.
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再入飞行器侧向制导的几何方法
本文研究了高超声速再入飞行器的横向制导问题。更具体地说,我们提出了一个横向廊道的几何解决方案,这将有助于实现河岸反转频率和廊道安全之间的权衡。众所周知,横向走廊决定了岸角的边界,其配置反映了反转的时间,而最突出的挑战是如何准确地制定走廊,而不是通常使用的线性近似。特别的是,该方案详细阐述了横贯距离信息的预测,并将廊道表示为几何曲线,大大提高了包络预测的精度。仿真结果验证了该方案的有效性。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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