| 注册
首页|期刊导航|中国空间科学技术(中英文)|基于综合效能的低轨异构星座优化设计方法

基于综合效能的低轨异构星座优化设计方法

刘思阳 潘瑞雪 李任飞 蒙涛

中国空间科学技术(中英文)2026,Vol.46Issue(1):59-72,14.
中国空间科学技术(中英文)2026,Vol.46Issue(1):59-72,14.DOI:10.16708/j.cnki.1000-758X.2026.0009

基于综合效能的低轨异构星座优化设计方法

Comprehensive performance optimized design methodology for LEO heterogeneous constellations

刘思阳 1潘瑞雪 2李任飞 3蒙涛4

作者信息

  • 1. 浙江大学海南研究院海洋先进技术研究中心,三亚 572025
  • 2. 上海卫星工程研究所,上海 201100
  • 3. 浙江大学航空航天学院,杭州 310027
  • 4. 浙江大学海南研究院海洋先进技术研究中心,三亚 572025||浙江大学航空航天学院,杭州 310027
  • 折叠

摘要

Abstract

A comprehensive study is conducted on the design methodology for low Earth orbit(LEO)mega-constellations composed of heterogeneous satellites with diverse functions,orbits and payloads.Three critical challenges are addressed,including nonlinear coverage superposition,differentially coupled drift trajectories,and large-parameter optimization.An efficient semi-major axis decay model is developed under the influence of J2 perturbation and atmospheric drag with combined linear and quadratic fitting.Relative drift compensation equations for both the right ascension of the ascending node and the argument of latitude are derived to maintain orbital stability.A complex optimization model is constructed with the objective of minimizing the integrated manufacturing-launch cost,incorporating multi-dimensional coverage constraints such as revisit time,imaging resolution and coverage stability as well as multi-source engineering constraints including limited fuel,selectable satellites,and multiple mission phases.Key variables are reduced through theoretical analysis to improve computational efficiency.A genetic algorithm is employed to determine the cost-optimal nominal configuration parameters.Furthermore,a closed-loop design framework is developed to coordinate nominal configuration,partial correction,fuel planning,and control implementation throughout the constellation lifecycle.For missions targeting coverage between 30°(N)and the equator,with constraints of≤10 min revisit time and≤1 m imaging resolution,the optimized heterogeneous constellation configuration demonstrates a 26%-30%reduction in total cost compared with uniform configurations.Additionally,temporal consistency of revisit time across different latitudes shows improvement.The performance advantage increases with wider latitude coverage.The optimized methodology enables synergistic optimization of coverage performance and cost,supports scalable design of constellations exceeding 1000 satellites for emergency remote sensing and global IoT applications,and contributes to reduced lifecycle cost and design complexity.

关键词

异构星座/构型优化/遗传算法/覆盖效能/综合成本/全流程设计

Key words

heterogeneous constellation/configuration optimization/genetic algorithm/coverage performance/integrated cost/full-process design

分类

航空航天

引用本文复制引用

刘思阳,潘瑞雪,李任飞,蒙涛..基于综合效能的低轨异构星座优化设计方法[J].中国空间科学技术(中英文),2026,46(1):59-72,14.

基金项目

上海航天科技创新基金(SAST2023-092) (SAST2023-092)

浙江大学海南研究院项目(0210-6602-A12301) (0210-6602-A12301)

中国空间科学技术(中英文)

1000-758X

访问量0
|
下载量0
段落导航相关论文