谢磊
电子信息 -- 【招收硕士研究生】 -- 航天学院
其他联系方式
暂无内容
论文成果DOI码：10.1109/TAES.2025.3622573
所属单位：南京航空航天大学
发表刊物：IEEE Transactions on Aerospace and Electronic Systems
摘要：Real-time trajectory optimization can improve the guidance accuracy and the ability to respond to sudden failures for lunar spacecraft. Sequential convex programming (SCP) has become one of the most promising methods to achieve real-time trajectory optimization due to its high efficiency. The L1 penalty function-based SCP is one of the few with theoretically guaranteed convergence. However, its convergence is highly sensitive to penalty coefficients. The main contribution of this paper are as follows: 1)We find that one main reason for this sensitivity is the penalty coupling between the……
备注：2025-10 在线首发，正式卷期为 2026 年第 62 卷
学科门类：工学
一级学科：航空宇航科学与技术
文献类型：J
卷号：62
页面范围：646-660
ISSN号：0018-9251
是否译文：否
发表时间：2026-01-01
合写作者：Zhenyu Gong, Hongbo Zhang, Guojian Tang, Shuang Li
第一作者：谢磊
