谢磊
电子信息 -- 【招收硕士研究生】 -- 航天学院
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论文成果DOI码：10.1109/ACCESS.2020.2997235
所属单位：南京航空航天大学
发表刊物：IEEE Access
摘要：Real time trajectory planning is vital in rocket precision powered landing guidance. Due to the nonconvex angle of attack (AOA) constraint and other constraints, including nonlinear dynamics and thrust constraint, the powered landing trajectory planning problem is highly nonconvex, which makes it difficult to be solved in real time via existing nonconvex optimization algorithms. As the main contribution of this paper, the AOA constraint is taken into account in the problem. A convex feasible set method is presented to handle it, in which a quadratic concave function is introduced to find 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：8
页面范围：100485-100496
ISSN号：2169-3536
是否译文：否
发表时间：2020-01-01
合写作者：Hongbo Zhang, Xiang Zhou, Guojian Tang
第一作者：谢磊
