力学与实践 ›› 2020, Vol. 42 ›› Issue (2): 151-155.DOI: 10.6052/1000-0879-19-321

• 应用研究 • 上一篇    下一篇

基于拉网主动控制的运载火箭回收策略

叶立军*,,**,1)(), 刘付成,**, 宝音贺西*   

  1. * 清华大学航天航空学院,北京 100084
    上海航天控制技术研究所,上海201109
    ** 上海市空间智能控制技术重点实验室,上海 201109
  • 收稿日期:2019-09-02 修回日期:2019-11-14 出版日期:2020-04-20 发布日期:2020-05-11
  • 通讯作者: 叶立军
  • 作者简介:1) 叶立军,高级工程师,主要研究方向为航天控制系统设计。E-mail: xthylj@163.com

RECOVERY STRATEGY OF LAUNCH VEHICLE BASED ON CONTROLLABLE NETWORK

YE Lijun*,,**,1)(), LIU Fucheng,**, BAOYIN Hexi*   

  1. * School of Aerospace, Tsinghua University, Beijing 100084, China
    Shanghai Aerospace Control Technology Institute, Shanghai 201109, China
    ** Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai 201109, China
  • Received:2019-09-02 Revised:2019-11-14 Online:2020-04-20 Published:2020-05-11
  • Contact: YE Lijun

摘要:

运载火箭回收技术已经成为热门研究课题,本文提出了一种基于拉网主动控制的运载火箭回收策略,介绍了基本工作原理及组成,给出了初步设计。

关键词: 拉网控制, 运载火箭, 回收着陆

Abstract:

The launch vehicle recycling technology has become a hot research topic. The Recovery Strategy of Launch Vehicle based on controllable network is proposed, the basic working principle and composition is introduced, and the preliminary design is given.

Key words: controllable network, launch vehicle, recovery and landing

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