Radiometric Interferometry for Deep Space Navigation using Geostationary Satellites

TL;DR

This paper introduces a novel space-based interferometry method using geostationary satellites to improve deep space navigation by extending baselines and eliminating atmospheric errors, showing promising theoretical accuracy.

Contribution

The paper proposes a new GEO satellite-based interferometry approach for deep space navigation, enhancing baseline length and visibility compared to terrestrial systems.

Findings

Achieves approximately 3.73 nanoradians angular error.

Nearly doubles geometrical availability for tracking.

Eliminates atmospheric phase errors.

Abstract

Deep space navigation presents significant challenges due to the unavailability of Global Navigation Satellite System (GNSS) signals and severe signal attenuation over interplanetary distances. Traditional terrestrial systems, such as NASA Deep Space Network (DSN) and ESA ESTRACK, rely on Very Long Baseline Interferometry (VLBI) for angular positioning. However, these systems are limited by relatively short baselines, atmospheric distortions requiring extensive calibration, and reduced visibility availability due to Earth rotation. This research proposes a complementary deep space navigation approach using space based interferometry, in which radio signals from the spacecraft are received and cross correlated onboard Geostationary Earth Orbit (GEO) satellites. By replacing terrestrial VLBI stations with dual GEO platforms, the method significantly extends the effective baseline, removes atmospheric phase errors, and provides almost continuous visibility to deep space targets. Unlike Earth based systems, GEO based interferometry maintains persistent station mutual visibility, enabling higher measurement availability and more flexible mission support. A complete system model is presented, including the principles of dual frequency phase based angular tracking and a structured error budget analysis. Theoretical results show that the GEO based system achieves a total angular error of approximately 3.73 nanoradians, within the same order of magnitude as terrestrial VLBI. Space based architecture nearly doubles the geometrical availability for interferometric tracking, while eliminating atmospheric distortions. These findings support the feasibility of the GEO based VLBI concept and motivate continued research and field validation for future deep space navigation applications.