AEROSPACE CHINA

中国航天科技集团有限公司主管

中国航天系统科学与工程研究院主办

ISSN 1671-0940

CN 11-4673/V

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AEROSPACE CHINA ›› 2016, Vol. 17 ›› Issue (1): 12-18.

• 学术研究 • 上一篇    下一篇

Nonlinear Rolling Control Technology of Liquid Launch Vehicle Based on Single Engine

  

  • 出版日期:2016-03-25 发布日期:2019-11-26

Nonlinear Rolling Control Technology of Liquid Launch Vehicle Based on Single Engine

  1. 1.Shanghai Academy of Spaceflight Technology, Shanghai 201109
    2.Shanghai Institute of Aerospace Systems Engineering, Shanghai 201109
  • Online:2016-03-25 Published:2019-11-26
  • About author:Z H A N G We i d o n g (1958- ), graduated from the National University of Defense Technology. He is a researcher of the Shanghai Academy of Spaceflight Technology and is engaged in launch vehicle’s general design, dynamics and control. He serves as the Chief Designer of LM-6 launch vehicle.

Abstract:  New program was proposed in LM-6 rolling control technology that using high-pressure staged combustion gas. Launch vehicle rolling control by just one engine was realized. Under the limit of the rolling control moment of the launch vehicle, a new attitude dynamic model is established. Interference source and how to reduce the effect was analyzed, and method of designing a pre-compensated robust controller was proposed. Simulation and flight results showed that the attitude dynamic model established and the pre-compensation robust controller proposed in this 
paper could solve the key problems with a strong coupling attitude controller, and realize high quality and high reliability control in wind areas, and improve the capability of the launch vehicle.

Key words: LM-6, Rolling control, Attitude model, Attitude control.