| 注册
首页|期刊导航|上海航天(中英文)|一种基于约束规则的航天器全相位交会对接程序规划方法

一种基于约束规则的航天器全相位交会对接程序规划方法

姜萍 可荣硕 高宇辉 周心婷 王瑞玮

上海航天(中英文)2024,Vol.41Issue(1):33-37,5.
上海航天(中英文)2024,Vol.41Issue(1):33-37,5.DOI:10.19328/j.cnki.2096-8655.2024.01.004

一种基于约束规则的航天器全相位交会对接程序规划方法

A Programming Method for Spacecraft All-Phase Rendezvous and Docking Based on Constraint Rules

姜萍 1可荣硕 1高宇辉 1周心婷 1王瑞玮1

作者信息

  • 1. 北京航天飞行控制中心,北京 100094
  • 折叠

摘要

Abstract

A programming method based on constraint rules is designed for the rendezvous and docking process in the field of manned spaceflight.The flight program is divided into flight control events based on the correlations,and the event constraints are decoupled from time or cycles to form a planning configuration system suitable for all phase rendezvous and docking.Through a set of configurations,the planning generation of each normal and emergency branch program is achieved.Compared with traditional time-series based programming methods,the designed method improves the adaptability of the configuration and the program design efficiency,and provides reference for subsequent rendezvous and docking program planning program design.

关键词

全相位/交会对接/约束规则/规划设计/航天器

Key words

all-phase/rendezvous and docking/constraint rule/programming and design/spacecraft

分类

航空航天

引用本文复制引用

姜萍,可荣硕,高宇辉,周心婷,王瑞玮..一种基于约束规则的航天器全相位交会对接程序规划方法[J].上海航天(中英文),2024,41(1):33-37,5.

基金项目

国家重点研发计划项目(2020YFC2200902) (2020YFC2200902)

国家自然科学基金重点项目(72131009) (72131009)

上海航天(中英文)

OACSTPCD

2096-8655

访问量0
|
下载量0
段落导航相关论文