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利用过载开关和程序控制器的航天器减速着陆系统开伞控制方法

雷江利 邓黎 吕智慧 赵铮

航天器工程2017,Vol.26Issue(5):28-33,6.
航天器工程2017,Vol.26Issue(5):28-33,6.DOI:10.3969/j.issn.1673-8748.2017.05.005

利用过载开关和程序控制器的航天器减速着陆系统开伞控制方法

Parachute Deployment Control Method for Spacecraft Descent and Landing System Based on Overload Switch and Program Controller

雷江利 1邓黎 1吕智慧 1赵铮1

作者信息

  • 1. 北京空间机电研究所,北京 100094
  • 折叠

摘要

Abstract

The control method of parachute deployment for spacecraft is a key part of the de-scent and landing system design, it directly affects the success of the descent and landing system.Aiming at the problem of low reliability and singleness mode of parachute deploy-ment control based on overload switch and time controller, a control method of parachute deployment based on the overload switch and program controller is presented which can ef-fectively identify the overload switch failure mode and provide control signals for parachute deployment reliably.The parameters setting method of overload switch,axial acceleration cal-culation of the re-entry capsule are raised,and the analysis of the error for axial accelera-tion,parachute deployment altitude and additional overload are given.Flight test shows that working mode of overload switch is well-judged, control precision of parachute deployment altitude meets requirement,and the design has a certain practical value and it also is safety and reliable.

关键词

航天器减速着陆系统/开伞控制/过载开关/程序控制器/时间延迟

Key words

spacecraft descent and landing system/parachute deployment control/overload switch/program controller/time-delay

分类

航空航天

引用本文复制引用

雷江利,邓黎,吕智慧,赵铮..利用过载开关和程序控制器的航天器减速着陆系统开伞控制方法[J].航天器工程,2017,26(5):28-33,6.

基金项目

国家重大科技专项工程 ()

航天器工程

OA北大核心CSCDCSTPCD

1673-8748

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