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

作　　者：姜萍 可荣硕 高宇辉[1] 周心婷 王瑞玮 JIANG Ping;KE Rongshuo;GAO Yuhui;ZHOU Xinting;WANG Ruiwei(Beijing Aerospace Control Center,Beijing 100094,China)

机构地区：[1]北京航天飞行控制中心,北京100094

出　　处：《上海航天（中英文）》2024年第1期33-37,共5页Aerospace Shanghai（Chinese&English）

基　　金：国家重点研发计划项目(2020YFC2200902);国家自然科学基金重点项目(72131009)。

摘　　要：针对载人航天领域交会对接过程,设计了一种基于约束规则的程序规划方法,将飞行程序按照相关性划分为飞控事件,将事件约束与时间或圈次解耦,形成适用全相位交会对接的规划配置体系,通过一套配置实现各正常、应急分支程序的规划生成,相比传统基于时序的程序设计方法,提高配置的适应性,提高程序设计效率,为后续交会对接程序规划设计提供参考。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 

分 类 号：V526[航空宇航科学与技术—人机与环境工程]