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

机译:中国重型运载火箭控制系统关键技术研究

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摘要

This paper reviewed the development of control technology in domestic and foreign launch vehicle (LV),and based on which,the key technologies of control system for Chinese heavy-lift launch vehicles were proposed.A dynamic on-line trajectory planning technique was discussed to meet the demand of guidance control under complex constraints,and model based identification and adaptive control technology was suggested to deal with the control problems caused by model uncertainty and disturbance,and an integrated avionics system based on high speed communication was put forward for module integration and distributed control,and FBG based real time flight control was also discussed.Moreover,other key technologies,such as wireless interconnection,wireless power transfer,and temporal and spatial partitioning operating system,are both briefly introduced for the application in control systems.These studies will lead to breakthroughs in autonomous flight control in LV,and provide technical support for more long-term deep space explorations.
机译:本文回顾了国内外运载火箭控制技术的发展,在此基础上,提出了中国重型运载火箭控制系统的关键技术。讨论了一种动态在线轨迹规划技术。为满足复杂约束条件下制导控制的需求,提出了基于模型的辨识和自适应控制技术,以解决模型不确定性和扰动引起的控制问题,提出了基于高速通信的航空电子集成系统,实现了模块的集成。还讨论了分布式控制和基于FBG的实时飞行控制。此外,还简要介绍了无线互连,无线功率传输以及时空划分操作系统等其他关键技术在控制系统中的应用。将导致LV自主飞行控制方面的突破,并提供技术支持进行更长期的深空探索。

著录项

  • 来源
    《中国航天(英文版)》 |2017年第2期|13-22|共10页
  • 作者

    SONG Zhengyu;

  • 作者单位

    Beijing Aerospace Automatic Control Institute, Beijing 100854;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-18 22:23:09
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