Research on Optimal Mission Planning for Satellite Swarm Configuration Change
This study addresses the challenges of mission allocation and real-time path planning for satellite swarms under strict fuel constraints and computational complexity limitations. By leveraging the Clohessy-Wiltshire (CW) guidance equations, a fuel consumption model is established to quantify propell...
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| Published in: | Chinese Control Conference pp. 2214 - 2219 |
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| Main Authors: | , , |
| Format: | Conference Proceeding |
| Language: | English |
| Published: |
Technical Committee on Control Theory, Chinese Association of Automation
28.07.2025
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| Subjects: | |
| ISSN: | 1934-1768 |
| Online Access: | Get full text |
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| Summary: | This study addresses the challenges of mission allocation and real-time path planning for satellite swarms under strict fuel constraints and computational complexity limitations. By leveraging the Clohessy-Wiltshire (CW) guidance equations, a fuel consumption model is established to quantify propellant expenditure, with optimization objectives targeting both total fuel minimization and fuel equity across the swarm. A particle swarm optimization (PSO) algorithm transforms task allocation into a constrained programming problem, enabling efficient resource distribution for long-term orbital services. To overcome the scalability limitations of centralized methods, a distributed sequential convex programming (SCP) framework is proposed, allowing individual spacecraft to autonomously compute fuel-optimal trajectories while rigorously satisfying orbital dynamics, collision avoidance, and fuel consumption constraints. This dual-layered approach reduces system-wide computational complexity by localizing optimization tasks, achieving the scalability for real-time operations in large-scale swarms, thereby advancing sustainable mission planning capabilities for next-generation space systems. |
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| ISSN: | 1934-1768 |
| DOI: | 10.23919/CCC64809.2025.11179178 |