DOI码：10.1016/j.asr.2024.05.053

所属单位：南京航空航天大学

发表刊物：Advances in Space Research

摘要：Convex optimization has great potential for onboard trajectory generation which can eliminate large state deviations and improve landing precision. In practical applications, the convex optimization problem is often infeasible under disturbances. In this paper, we analyze the reason for the infeasibility of the fuel-optimal trajectory optimization problem. The analysis result shows that the thrust saturation degrade the anti-disturbance performance and then lead to infeasibility. Based on this analysis, we improved the anti-disturbance performance of convex optimization-based guidance from……

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：74

期号：7

页面范围：3256-3272

ISSN号：0273-1177

是否译文：否

发表时间：2024-10-01

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

第一作者：谢磊