现代防御技术2026，Vol.54Issue(2)：82-91,10.DOI:10.3969/j.issn.1009-086x.2026.02.007
基于伴随法的顺逆轨交汇方式研究
Study on Prograde and Retrograde Orbit Interception Based on the Adjoint Method
陈亚东 1吕博 1任天助 1刘俊辉2
作者信息
- 1. 北京宇航系统工程研究所,北京 100076
- 2. 北京理工大学,北京 100081
- 折叠
摘要
Abstract
In view of the effect of different prograde and retrograde rendezvous modes on miss distance,the vehicle terminal guidance rendezvous process is modeled and analyzed based on the theory of adjoint method.The original model of the terminal guidance problem is established,and the adjoint model of the problem is established based on the adjoint method.Normalized analytical expressions for the influence of factors such as target maneuver and initial heading error on miss distance were obtained.Based on the above theoretical analysis,the characteristics of reverse orbit head-on rendezvous,pursuit following orbit rendezvous and forward following orbit rendezvous are summarized.关键词
末制导/脱靶量/伴随法/顺轨交汇/逆轨交汇/目标机动Key words
terminal guidance/miss distance/adjoint method/prograde interception/retrograde interception/target maneuvering分类
军事科技引用本文复制引用
陈亚东,吕博,任天助,刘俊辉..基于伴随法的顺逆轨交汇方式研究[J].现代防御技术,2026,54(2):82-91,10.
