DOI码：10.2514/1.G009022

所属单位：南京航空航天大学

发表刊物：Journal of Guidance, Control, and Dynamics

摘要：This study focuses on the key challenge of achieving high-precision guidance for spacecraft: real-time trajectory optimization. The highly efficient sequential convex programming (SCP) is a potential method to address this issue, but its convergence is difficult to guarantee. To enhance the convergence performance of SCP, this paper proposes a high-dimensional merit-function-based SCP method. The main contribution of this paper is threefold. Firstly, the traditional one-dimensional penalty function used to ensure the convergence of SCP is extended to a high-dimensional merit function, which……

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：48

期号：7

页面范围：1525-1544

ISSN号：0731-5090

是否译文：否

发表时间：2025-07-01

合写作者：Xiang Zhou, Hong-Bo Zhang, Guo-Jian Tang, Shuang Li

第一作者：谢磊