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Published on: December 9, 2012
The optimization of low Earth orbit satellite constellation visibility with genetic algorithm for improved navigation
Chao Qin1,2, Yanbin Gao3, Yihuan Wang4
1College of Intelligent Systems Science and Engineering, Harbin Engineering University, Harbin, 150001, China. max_qinchao@163.com.
This study enhances Low Earth Orbit satellite constellation visibility using an adaptive parallel Genetic Algorithm (GA). The optimized framework improves navigation accuracy and dynamic robustness, outperforming other methods.
Area of Science:
- Satellite Constellation Design
- Optimization Algorithms
- Orbital Mechanics
Background:
- Low Earth Orbit (LEO) satellite constellations face visibility optimization challenges.
- Ensuring navigation accuracy and dynamic robustness is critical for LEO constellations.
- J2 perturbation effects impact long-term constellation performance.
Purpose of the Study:
- To propose an enhanced framework for LEO satellite constellation visibility optimization.
- To improve navigation accuracy and dynamic robustness of satellite constellations.
- To provide a technical foundation for next-generation Global Navigation Satellite System (GNSS) enhancements.
Main Methods:
- Developed an adaptive parallel Genetic Algorithm (GA) framework.
- Designed a hybrid constellation integrating polar, Walker, and Orthogonal Circular Orbits.
- Incorporated a dynamic relaxation factor (γ) to compensate for J2 perturbations.
- Implemented adaptive parameter adjustment using population diversity entropy.
- Utilized a parallel fitness evaluation strategy for multi-core architectures.
- Employed a simplified fitness function design.
Main Results:
- Achieved an average of 14.3 visible satellites in a 100-satellite scenario, outperforming D-NSDE by 3.6%.
- Reduced Position Dilution of Precision (PDOP) to 2.3 with 95.6% global coverage.
- Demonstrated high robustness with only a 3.5% coverage drop after single satellite failure.
- Maintained 94.8% coverage after 10 years of orbital perturbation.
- Achieved PDOP ≤ 2.8 with convergence times under 210s for 500-1000 satellite scenarios.
- Outperformed Particle Swarm Optimization and Dynamic Non-dominated Sorting Differential Evolution in visibility, robustness, and efficiency.
Conclusions:
- The proposed adaptive parallel GA framework effectively optimizes LEO satellite constellation visibility.
- The framework offers superior navigation accuracy, dynamic robustness, and computational efficiency.
- This research provides a significant advancement for future GNSS development.
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