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基于偏差比例导航的可重复使用运载火箭预测校正着陆制导

IF 2.3 3区 工程技术 Q1 ENGINEERING, AEROSPACE
Journal of Guidance Control and Dynamics Pub Date : 2025-05-01 DOI:10.2514/1.g008911
Runqiu Yang
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引用次数: 0

摘要

制导、控制与动力学杂志，出版前。
本文章由计算机程序翻译，如有差异，请以英文原文为准。
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Biased-Proportional-Navigation-Based Predictor–Corrector Landing Guidance for Reusable Launch Vehicles
Journal of Guidance, Control, and Dynamics, Ahead of Print.
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来源期刊
Journal of Guidance Control and Dynamics
Journal of Guidance Control and Dynamics 工程技术-工程：宇航
CiteScore
6.20
自引率
19.20%
发文量
201
审稿时长
3.7 months
期刊介绍： This Journal is devoted to the advancement of the science and technology of guidance, control, and dynamics through the dissemination of original archival papers disclosing significant technical knowledge, exploratory developments, design criteria, and applications in aeronautics, astronautics, celestial mechanics, and related fields. The Journal publishes qualified papers on dynamics, stability, guidance, control, navigation, optimization, electronics, avionics, and information processing related to aeronautical, astronautical, and marine systems. Papers are sought which demonstrate the application of recent research to practical engineering problems. Papers that describe aspects of the dynamics and control of significant recent developments, such as a new or different aircraft or spacecraft, also are desired.
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