中国航天（英文版）2022，Vol.23Issue(2)：55-61,7.DOI:10.3969/j.issn.1671-0940.2022.02.007
Application and Research of High-Power Electric Servo System on Launch Vehicle
Application and Research of High-Power Electric Servo System on Launch Vehicle
FENG Wei 1CUI Yebing 2WANG Yaoyao 1YU Ge 2SONG Shuwei 1CHEN Shuheng 2GU Dawei1
作者信息
- 1. Shanghai Institute of Spaceflight Control Technology,Shanghai 201109
- 2. Shanghai Engineering Research Center of Servo System,Shanghai 20110
- 折叠
摘要
关键词
electric servo system/servo control driver/electric servo mechanism/power drive module/advanced correction link/notch filterKey words
electric servo system/servo control driver/electric servo mechanism/power drive module/advanced correction link/notch filter引用本文复制引用
FENG Wei,CUI Yebing,WANG Yaoyao,YU Ge,SONG Shuwei,CHEN Shuheng,GU Dawei..Application and Research of High-Power Electric Servo System on Launch Vehicle[J].中国航天（英文版）,2022,23(2):55-61,7.
