宇航学报

宇航学报 ›› 2020, Vol. 41 ›› Issue (7): 850-859.doi: 10.3873/j.issn.1000-1328.2020.07.003

• 综述 • 上一篇    下一篇

空天飞行器制导控制技术研究进展与展望

姚德清，魏毅寅，杨志红，崔乃刚   

  1. 1. 哈尔滨工业大学航天学院，哈尔滨 150001；2.北京空天技术研究所，北京 100074； 3.中国航天科工集团有限公司，北京 100048； 4.中国航天科工飞航技术研究院，北京 100074
  • 收稿日期:2019-11-27 修回日期:2020-03-11 出版日期:2020-07-15 发布日期:2020-07-25
  • 基金资助:
    微小航天器技术国防重点实验室开放基金（HIT.KLOF.MST.201704）；哈尔滨市科技创新人才专项基金（2015RQQXJ089）

Progress and Prospect of Research on Guidance and Control Technology of Aerospace Vehicle#br#

YAO De qing, WEI Yi yin, YANG Zhi hong,CUI Nai gang   

  1. 1. School of Astronautics, Harbin Institute of Technology, Harbin 150001, China; 2. Beijing Aerospace Technology Institute, Beijing 100074, China; 3. China Aerospace Science and Industry Corporation, Beijing 100048, China; 4. HIWING Technology Academy of CASIC, Beijing 100074, China
  • Received:2019-11-27 Revised:2020-03-11 Online:2020-07-15 Published:2020-07-25

PDF

935

摘要： 本文在简要介绍空天飞行器制导控制技术发展情况基础上，针对其典型的任务形态给制导控制技术带来的挑战，分别从动力学建模、轨迹优化与制导、飞行控制与导航等四个方面阐述了制导控制技术中面临的关键技术，并探讨了空天飞行器制导控制技术后续发展方向与思路。

关键词: 空天飞行器, 动力学建模, 轨迹优化与制导, 导航与控制

Abstract: Based on the brief introduction to the development of the guidance and control technology of aerospace vehicle, aiming at the challenges brought by its typical mission, this paper expounds the key technologies from four aspects, i.e. dynamics modeling, trajectory optimization and guidance, flight control and navigation, and discusses the development of the guidance and control technology of aerospace vehicle.

Key words: Aerospace vehicle, Dynamics modeling, Trajectory optimization and guidance, Navigation and Control

中图分类号: