基 于 最 优 误 差 动 力 学 的 变 速 导 弹 飞 行 路 程控 制 制 导 律

Translated title of the contribution: Flying range control guidance for varying⁃speed missiles based on optimal error dynamics

Yuanhe Liu, Kebo Li*, Shaoming He, Yangang Liang

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

5 Citations (Scopus)

Fingerprint

Dive into the research topics of 'Flying range control guidance for varying⁃speed missiles based on optimal error dynamics'. Together they form a unique fingerprint.

Engineering