Research on Hybrid Constellation Design Method for Key Target Collaborative Observation Based on Adaptive-Reference-Point-Adjusted NSGA-III

The rapid deployment of low-orbit mega-constellations has intensified the need for space situational awareness systems to transition from wide-area surveillance to persistent collaborative tracking of maneuvering targets. However, existing constellation design methods face three fundamental challenges: insufficient coverage overlap for multi-satellite collaborative observation, poor temporal continuity for long-arc tracking, and weak resilience against satellite failures. To address these bottlenecks, this paper proposes a hybrid constellation multi-objective optimization design method based on adaptive-reference-point-adjusted NSGA-III. The configuration adopts a Walker–Flower hybrid architecture, where the Walker constellation provides wide-area target search and the Flower constellation enables regional persistent tracking, forming a “search-track” cascaded collaborative mechanism. The optimization model integrates four competing objectives—observation duration, constellation cost, positioning accuracy, and performance decay slope—into a unified framework. To overcome the limitations of classical NSGA-III, three improvement strategies are introduced: adaptive reference point adjustment, constraint-dominated sorting, and mixed-integer encoding. Simulation results over a 24 h LEO target observation scenario with 168 background satellites demonstrate that the proposed algorithm achieves an average observation duration of 33.7 h across four maneuvering targets, outperforming classical NSGA-III by 54.8%, while improving positioning accuracy by 97.7% and resilience by 45.5%. All recommended solutions strictly satisfy engineering constraints, whereas comparison algorithms retain infeasible solutions due to the penalty function approach. The proposed method provides a practical and robust engineering solution for LEO key target collaborative observation constellation design, with demonstrated advantages in tracking continuity, positioning accuracy, and system resilience.

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Publication Details

Journal
Aerospace
Published
2026-09-30
DOI
https://doi.org/10.3390/aerospace13100896
Primary Topic
Spacecraft Dynamics and Control
Type
article
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Research on Hybrid Constellation Design Method for Key Target Collaborative Observation Based on Adaptive-Reference-Point-Adjusted NSGA-III

Ping Jian, Changshou Quan
Aerospace
Spacecraft Dynamics and Control
article

Research on Hybrid Constellation Design Method for Key Target Collaborative Observation Based on Adaptive-Reference-Point-Adjusted NSGA-III

Ping Jian, Changshou Quan
article en

Abstract

The rapid deployment of low-orbit mega-constellations has intensified the need for space situational awareness systems to transition from wide-area surveillance to persistent collaborative tracking of maneuvering targets. However, existing constellation design methods face three fundamental challenges: insufficient coverage overlap for multi-satellite collaborative observation, poor temporal continuity for long-arc tracking, and weak resilience against satellite failures. To address these bottlenecks, this paper proposes a hybrid constellation multi-objective optimization design method based on adaptive-reference-point-adjusted NSGA-III. The configuration adopts a Walker–Flower hybrid architecture, where the Walker constellation provides wide-area target search and the Flower constellation enables regional persistent tracking, forming a “search-track” cascaded collaborative mechanism. The optimization model integrates four competing objectives—observation duration, constellation cost, positioning accuracy, and performance decay slope—into a unified framework. To overcome the limitations of classical NSGA-III, three improvement strategies are introduced: adaptive reference point adjustment, constraint-dominated sorting, and mixed-integer encoding. Simulation results over a 24 h LEO target observation scenario with 168 background satellites demonstrate that the proposed algorithm achieves an average observation duration of 33.7 h across four maneuvering targets, outperforming classical NSGA-III by 54.8%, while improving positioning accuracy by 97.7% and resilience by 45.5%. All recommended solutions strictly satisfy engineering constraints, whereas comparison algorithms retain infeasible solutions due to the penalty function approach. The proposed method provides a practical and robust engineering solution for LEO key target collaborative observation constellation design, with demonstrated advantages in tracking continuity, positioning accuracy, and system resilience.

AerospaceVol. 13(10)
Space Engineering University (CN)
Openalex Percentile: Top 8%
Spacecraft Dynamics and Control
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Research on Hybrid Constellation Design Method for Key Target Collaborative Observation Based on Adaptive-Reference-Point-Adjusted NSGA-III — Ping Jian, Changshou Quan · Aerospace (2026) | TGRS Research Map | TGRS