基于偏置比例导引与凸优化的火箭垂直着陆制导

Translated title of the contribution: Landing-phase guidance of rocket using bias proportional guidance and convex optimization

Ze An, Fenfen Xiong*, Zhuonan Liang

*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

13 Citations (Scopus)

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Engineering