DOI码：10.1109/CAC48633.2019.8996784

所属单位：南京航空航天大学

发表刊物：2019 Chinese Automation Congress (CAC)

摘要：Rocket powered landing trajectory planning is a typical non-convex and non-smooth optimization problem. To solve this problem, a convex optimization method based on hp-adaptive pseudospectral method is proposed. Combining the advantages of these two methods, the proposed method can quickly and accurately obtain the optimal trajectory. Firstly, the original non-convex optimal control problem is transformed into a convex optimal problem by lossless convexification and change of variables convexifying the non-convex thrust constraint and nonlinear dynamics respectively. Then, t Then, the hp……

学科门类：工学

一级学科：航空宇航科学与技术

文献类型：J

页面范围：895-900

是否译文：否

发表时间：2019-11-01

合写作者：Hongbo Zhang, Xiang Zhou, Guojian Tang

第一作者：谢磊