Bifurcation Mechanism of Quasi-Halo Orbit from Lissajous Orbit

IF 2.3 3区工程技术 Q1 ENGINEERING, AEROSPACE

Journal of Guidance Control and Dynamics Pub Date : 2024-09-19 DOI:10.2514/1.g008233

Mingpei Lin, Hayato Chiba

引用次数: 0

Abstract

Journal of Guidance, Control, and Dynamics, Ahead of Print.

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准光环轨道与利萨焦轨道的分叉机制

制导、控制和动力学杂志》，印刷版前。

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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来源期刊

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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