A Determination and Reduction of Collision Probability for Satellites Using a Metalog Distribution
Abstract
The increasing levels of space debris in Earth's orbit require more accurate and efficient methods for estimating satellite collision probabilities to ensure reliable operations. Monte Carlo analysis remains a widely adopted approach due to its robustness, but its high computational cost is a limiting factor. This work introduces a methodology to increase efficiency by obtaining the probability estimation from a flexible metalog distribution that has been fitted to the Monte Carlo data. By fitting the metalog distribution to Monte Carlo sampling results, a continuous representation of collision probability is generated, allowing the probability estimation to be evaluated with a significantly reduced number of iterations. With this estimation, an optimized avoidance maneuver is calculated to reduce the probability of collision by targeting a user-specified miss distance with an in-plane burn. The results of this study demonstrate a reduction in computational demands associated with Monte Carlo methods and the feasibility of decreasing the probability of satellite collisions using a fuel-optimized avoidance burn. This combination of computational efficiency and maneuver planning provides a powerful approach to mitigating collision risks in increasingly congested orbital environments.
Fields of Study & Subjects
Space Satellite Systems and Control
Spacecraft Dynamics and Control
Space exploration and regulation
Publication details
- Journal / source
- AIAA SciTech Forum
- Publication date
- 8 January 2026