Linear Time/Parameter-Varying Models with Relative Orbit Elements Considering Continuous Controllability

IF 2.3 3区 工程技术 Q1 ENGINEERING, AEROSPACE Journal of Guidance Control and Dynamics Pub Date : 2024-11-22 DOI:10.2514/1.g008297
Takahiro Sasaki
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Abstract

Journal of Guidance, Control, and Dynamics, Ahead of Print.
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考虑到连续可控性的具有相对轨道要素的线性时变/参数可变模型
制导、控制和动力学杂志》,印刷版前。
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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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