DOI码：10.2514/1.G007494

所属单位：南京航空航天大学

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

摘要：Sequential second-order cone programming (SSOCP) is commonly used in aerospace applications for solving nonlinear trajectory optimization problems. The SSOCP possesses good real-time performance. However, one long-standing challenge is its unguaranteed convergence. In this paper, we theoretically analyze the descent property of the [Formula: see text] penalty function in the SSOCP. Using Karush–Kuhn–Tucker conditions, we obtain two important theoretical results: 1) the [Formula: see text] penalty function of the original nonlinear problem always descends along the iteration direction; 2) a……

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：46

期号：12

页面范围：2346-2361

ISSN号：0731-5090

是否译文：否

发表时间：2023-12-01

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

第一作者：谢磊