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Localization of Ad-Hoc Lunar Constellations in Communication Failure Modes for Distributed Spacecraft AutonomyAs Lunar missions increase in complexity, inspired by NASA’s Artemis Program, they will require reliable and sufficient Position, Navigation, and Timing (PNT) capability to support the upcoming Lunar users. The navigation service should also be compatible with the smaller platforms, like CubeSats, being sent by the public and private sectors. A non-dedicated, ad-hoc Lunar navigation constellation can provide PNT services on-demand using the non-dedicated swarm assets. Swarm members cooperatively and autonomously localize themselves with minimal interaction from Earth, freeing up valuable bandwidth and ground segment resources. The autonomous localization of Lunar constellations utilizes neighbor two-way intersatellite link (ISL) measurements in a distributed extended Kalman filter (DEKF) system to minimize operating costs. Because the decentralized Lunar PNT system relies on relay communication amongst the agents, network failures or loss of assets among ad-hoc Lunar constellations may impact localization performance. This study presents an evaluation of localization performance under increasing levels of network degradation. A simulation of an ad-hoc Lunar PNT swarm is augmented to include system faults and the impacts of intermittent and permanent failures on localization performance are evaluated. We investigate three potential causes of network degradation: single spacecraft loss, multiple spacecraft loss, and antenna failure. The numerical assessments from the simulation show that the LPNT system under study, based on an autonomous decentralized concept of operation, is highly robust and resilient to communication failures. Minor faults, such as single spacecraft loss, solar interference, technical malfunctions, message delays, and antenna outages, have minimal impact on state estimation, with only a 4.47% and 3.75% degradation in median position error for assets and a representative ground user, respectively, compared to an ideal communication scenario. However, major faults, such as hardware failures or meteor strikes leading to the loss of multiple spacecrafts, are more concerning. The permanent loss of three spacecraft results in a more severe performance degradation, with median position error increasing by 23.3% for assets and 11.7% for a representative ground user, despite the Lunar PNT system remaining functional.
Document ID
20240015245
Acquisition Source
Ames Research Center
Document Type
Conference Proceedings
Authors
Yeji Kim
(Yonsei University Seoul, South Korea)
Brian Kempa
(Ames Research Center Mountain View, United States)
Caleb Adams
(Ames Research Center Mountain View, United States)
Richard Levinson
(Wyle (United States) El Segundo, California, United States)
Jeremy Frank
(Ames Research Center Mountain View, United States)
Date Acquired
November 27, 2024
Publication Date
February 12, 2025
Publication Information
Publication: Proceedings of the 2025 International Technical Meeting of The Institute of Navigation
Publisher: Institute of Navigation
Issue Publication Date: February 5, 2025
URL: https://www.proceedings.com/institute-of-navigation-ion/
Subject Category
Spacecraft Instrumentation and Astrionics
Lunar and Planetary Science and Exploration
Communications and Radar
Meeting Information
Meeting: Institute of Navigation International Technical Meeting
Location: Long Beach, CA
Country: US
Start Date: January 27, 2025
End Date: January 30, 2025
Sponsors: Institute of Navigation
Funding Number(s)
CONTRACT_GRANT: 80ARC020D0010
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
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