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航天任务设计工业软件ATK通用轨道机动规划设计方法

杨震 金柯 郭祥 王华 罗亚中

国防科技大学学报2025,Vol.47Issue(4):10-22,13.
国防科技大学学报2025,Vol.47Issue(4):10-22,13.DOI:10.11887/j.issn.1001-2486.24120053

航天任务设计工业软件ATK通用轨道机动规划设计方法

General orbital maneuver planning design for space mission design industrial software ATK

杨震 1金柯 1郭祥 1王华 1罗亚中1

作者信息

  • 1. 国防科技大学空天科学学院,湖南长沙 410073||太空系统运行与控制全国重点实验室,湖南长沙 410073
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摘要

Abstract

Orbital maneuver planning is an important part of the design of complex space missions such as rendezvous and docking,lunar exploration,etc.However,the varying configuration requirements of different missions for orbit transfer positions,maneuver magnitudes,and targeting parameters pose significant challenges to the generalized modeling and solution of maneuver planning.Regarding this problem,a generalized orbital maneuver planning modeling method based on orbital segments was proposed,which abstracts the maneuver requirements of different scenarios into orbital segments,stopping conditions,and constraints,forming a building-block spacecraft mission description model.The orbital maneuver requirements were converted into a unified nonlinear programming problem,which was subsequently solved by employing three distinct methods:differential correction,sequential quadratic programming,and intelligent optimization algorithms.A software module ATK.Astromaster was developed as a core module for ATK(aerospace tool kit)software.Simulation results show that the proposed method can achieve general orbit maneuver modeling and solving in different scenarios.

关键词

轨道机动/航天动力学/航天任务设计/工业软件/ATK

Key words

orbital maneuver/astrodynamics/space mission design/industrial software/ATK

分类

航空航天

引用本文复制引用

杨震,金柯,郭祥,王华,罗亚中..航天任务设计工业软件ATK通用轨道机动规划设计方法[J].国防科技大学学报,2025,47(4):10-22,13.

基金项目

国家自然科学基金资助项目(12372052) (12372052)

湖南省自然科学基金资助项目(2023JJ20047) (2023JJ20047)

载人航天工程科技创新团队课题资助项目 ()

国防科技大学学报

OA北大核心

1001-2486

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