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Orbit-based authentication using TDOA signatures in satellite networks

Eric Jedermann, Martin Strohmeier, Mathias Schäfer, Jens Schmitt, Vincent Lenders

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Abstract

Given the nature of satellites orbiting the Earth on a fixed trajectory, in principle, it is interesting to investigate how this invariant can be exploited for security purposes. In particular, satellite orbit information can be retrieved from public databases. Using time difference of arrival (TDOA) measurements from multiple receivers, we can check this orbit information against a corresponding TDOA-based signature of the satellite. In that sense, we propose an orbit-based authentication scheme for down-link satellite communications in this paper. To investigate the properties and fundamentals of our novel TDOA signature scheme we study two satellite systems at different altitudes: Iridium and Starlink.

Topics & Concepts

MultilaterationComputer scienceSatelliteOrbit (dynamics)Communications satelliteAuthentication (law)FDOAScheme (mathematics)TrajectoryInvariant (physics)Real-time computingAerospace engineeringComputer securityAstronomyMathematicsPhysicsEngineeringMathematical physicsMathematical analysisAzimuthIndoor and Outdoor Localization TechnologiesSatellite Communication SystemsGNSS positioning and interference