Analytical framework for space debris collision avoidance maneuver design
Juan Luis Gonzalo, Camilla Colombo, Pierluigi Di Lizia (Politecnico di, Milano, Italy)

TL;DR
This paper presents an analytical framework for designing space debris collision avoidance maneuvers, optimizing for maximum deviation and minimum collision probability using eigenproblem solutions and covariance propagation.
Contribution
It introduces an analytical formulation that simplifies the optimization of collision avoidance maneuvers and compares different strategies across various conjunction geometries.
Findings
Maximum deviation and collision probability are constrained by uncertainties over time.
Eigenproblem approach effectively finds optimal maneuvers.
Lead time impacts collision probability reduction due to growing uncertainties.
Abstract
An analytical formulation for collision avoidance maneuvers involving a spacecraft and a space debris is presented, including solutions for the maximum deviation and minimum collision probability cases. Gauss' planetary equations and relative motion equations are used to map maneuvers at a given time to displacements at the predicted close approach. The model is then extended to map changes in state between two times, allowing one to propagate covariance matrices. The analytical formulation reduces the optimization problem to an eigenproblem, both for maximum deviation and minimum collision probability. Two maximum deviation cases, total deviation and impact parameter, are compared for a large set of spacecraft-debris conjunction geometries derived from European Space Agency's Meteoroid and Space Debris Terrestrial Environment Reference (MASTER-2009) model. Moreover, the maximum impact…
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