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The Research on Key Technologies of Chinese Heavy-Lift Launch Vehicle Control System

SONG Zhengyu

中国航天(英文版)2017,Vol.18Issue(2):13-22,10.
中国航天(英文版)2017,Vol.18Issue(2):13-22,10.DOI:10.3969/j.issn.1671-0940.2017.02.002

The Research on Key Technologies of Chinese Heavy-Lift Launch Vehicle Control System

The Research on Key Technologies of Chinese Heavy-Lift Launch Vehicle Control System

SONG Zhengyu1

作者信息

  • 1. Beijing Aerospace Automatic Control Institute, Beijing 100854
  • 折叠

摘要

关键词

Dynamic trajectory planning/on-line identification/MPC/integrated avionics system/heavy-lift launch vehicle/technical margin

Key words

Dynamic trajectory planning/on-line identification/MPC/integrated avionics system/heavy-lift launch vehicle/technical margin

引用本文复制引用

SONG Zhengyu..The Research on Key Technologies of Chinese Heavy-Lift Launch Vehicle Control System[J].中国航天(英文版),2017,18(2):13-22,10.

中国航天(英文版)

1671-0940

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