Sep 2026· Italian National Conference on Sensors· Vol 26, pp. 5607· 0 citations· 34 references
Medicine
TL;DR
A hybrid framework where a Double Deep Q-learning Network agent learns a policy to adaptively control the key parameters of a Particle Swarm Optimization (PSO) algorithm is proposed, validating the potential of deep reinforcement learning methods for complex aerospace optimization problems.
Abstract
Designing Low Earth Orbit (LEO) constellations for applications like Positioning, Navigation, and Timing (PNT) is a challenging multi-objective optimization challenge. Conventional metaheuristics often suffer from premature convergence due to their reliance on static adaptive rules, limiting their effectiveness in complex search space. To address this limitation, we proposed a hybrid framework where a Double Deep Q-learning Network (DDQN) agent learns a policy to adaptively control the key parameters of a Particle Swarm Optimization (PSO) algorithm. The proposed framework formulates Walker constellation optimization as an sequential parameter control problem. Based on constellation performance feedback, the DDQN controller jointly selects the inertia weight and acceleration coefficients of PSO, guiding the PSO to more effectively balance exploitation and exploration. In a regional design case for China, our algorithm demonstrated superior performance. Compared to a 120 satellites benchmark constellation, the optimized constellation achieved a 27% reduction in Geometric Dilution of Precision (GDOP), a 27.6% enhancement in navigation accuracy, and a 5% increase in coverage multiplicity. This work establishes a robust methodology for the automated and intelligent design of LEO systems, validating the potential of deep reinforcement learning methods for complex aerospace optimization problems.
Low Earth Orbit (LEO) mega-constellations are becoming central to global broadband delivery, yet their scale and constantly shifting topology make centralized, ground-based control impractical. This paper proposes a multi-agent reinforcement learning (MARL) framework in which each satellite acts as an autonomous agent...
Shubh Tiwari, K. Reddy· 2026 International Conferenc...· 0 citations
The explosive expansion of Low Earth Orbit (LEO) satellite mega-constellations presents critical challenges in operational risk management, real-time task allocation, and dynamic resource management due to their inherent time-varying topology and systemic uncertainties. To overcome the limitations of traditional optimi...
With the development of constellations and satellite chains, trajectory planning for constellation satellites has gradually attracted research attention. To address the infeasibility issues of trapezoidal sequential convex programming (T-SCP) in this strong non-convexity problem, this paper proposes high-precision adap...
Zi-Hui Ma, Rong Chen, Yuzhu Bai· Aerospace· 0 citations
To address the requirement for the fast design of fuel-optimal maneuver trajectories in on-orbit servicing of satellite constellations, traditional numerical methods for solving the Lambert problem suffer from high computational complexity and numerous iterations, making them inefficient for scenarios involving multipl...
Jun-Jie Lu, Zhong-Jie Meng, Bo Liu et al.· IEEE Transactions on Aerospa...· 0 citations
By prioritizing absolute search stability and robustness in high-dimensional tasks, the proposed algorithm attains an optimal balance between convergence quality and practical engineering efficiency, proving exceptionally effective in complex path-planning scenarios.
The Personal History Memory Mechanism is introduced, which replaces random perturbation with weighted historical experience to enhance the directional search capability of the algorithm, and a greedy selection strategy is embedded to ensure the monotonically non-deteriorating quality of population solutions.