Convex Maneuver Planning for Spacecraft Collision Avoidance
Fausto Vega, Jon Arrizabalaga, Ryan Watson, Zachary Manchester

TL;DR
This paper introduces a convex optimization-based algorithm for designing low-thrust collision avoidance maneuvers for spacecraft, enabling efficient and globally optimal solutions for short-term conjunctions in dense satellite environments.
Contribution
It formulates the maneuver planning as a nonconvex QCQP and relaxes it to a convex SDP, ensuring globally optimal solutions and handling collision probability constraints effectively.
Findings
The relaxation is empirically tight, allowing recovery of global optima.
The algorithm produces minimum-energy, minimum-risk collision avoidance maneuvers.
Validation shows effective collision risk reduction in high-fidelity simulations.
Abstract
Conjunction analysis and maneuver planning for spacecraft collision avoidance remains a manual and time-consuming process, typically involving repeated forward simulations of hand-designed maneuvers. With the growing density of satellites in low-Earth orbit (LEO), autonomy is becoming essential for efficiently evaluating and mitigating collisions. In this work, we present an algorithm to design low-thrust collision-avoidance maneuvers for short-term conjunction events. We first formulate the problem as a nonconvex quadratically-constrained quadratic program (QCQP), which we then relax into a convex semidefinite program (SDP) using Shor's relaxation. We demonstrate empirically that the relaxation is tight, which enables the recovery of globally optimal solutions to the original nonconvex problem. Our formulation produces a minimum-energy solution while ensuring a desired probability of…
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Taxonomy
TopicsSpacecraft Dynamics and Control · Space Satellite Systems and Control · Spacecraft Design and Technology
