Design and Development of Fault Tolerant Lunar Satellite Network and Navigation Architecture

dc.contributor.authorAryan, Suryanshen
dc.contributor.committeechairKenyon, Samantha Parryen
dc.contributor.committeechairFitzgerald, Riley McCreaen
dc.contributor.committeememberGramling, Cherylen
dc.contributor.committeememberRoss, Shane Daviden
dc.contributor.departmentAerospace and Ocean Engineeringen
dc.date.accessioned2026-06-11T08:01:02Zen
dc.date.available2026-06-11T08:01:02Zen
dc.date.issued2026-06-10en
dc.description.abstractSpace communication and navigation infrastructure has been a vital part in contributing to human civilization commercially and in achieving scientific endeavors in space exploration. The recent surge of attention towards the cislunar and lunar domains, along with scheduled missions until the next couple of decades, demands an understanding of space systems interactions for a sustainable, fault-tolerant lunar architecture. The LunaNet concept is a collaborative work between NASA, ESA and JAXA space agencies, representing the initial framework of interoperable standards and protocols for delivering communications and position, navigation, timing (CandPNT) services to users around the Moon. With LunaNet currently in the initial stages of the development phase, this thesis work aims to determine optimal CandPNT design architectures based on the communication and navigation performance of a stable Elliptical Lunar Frozen Orbit (ELFO) service constellation along with the Earth-Moon relay constellation models. The tradeoff space for the service constellations were explored with the sequential quadratic programming formulation and a multi-objective particle swarm heuristic search formulation to select diverse set of CandPNT designs. A simulation framework, termed SelenoNet, is designed to digitally model interactions within the CandPNT designs in a high-fidelity lunar environment to facilitate space network topology instantiation for emulating IP packets and BPv7 bundle transfers between lunar users and with Earth. Due to independent node instantiation of service satellites and users, SelenoNet can emulate satellite navigation broadcasts with Signal-In-Space errors (SISE) and clock errors to accurately determine precise point positioning for surface and orbiting lunar users. SelenoNet's high-fidelity cislunar propagator is validated using the Ansys Systems Tool Kit (STK) High Precision Orbit Propagation (HPOP) solutions. The resultant optimal constellations' CandPNT performance is evaluated and compared in SelenoNet to inform additional strategic performance for lunar surface ground stations, CandPNT design sensitivity and combinations of orbiting relay designs to maintain the quality of service (QoS).en
dc.description.abstractgeneralSpace communication from its genesis has played a key role in providing secure, high-speed global services that are accessible to most terrestrial users anywhere on Earth. However, with a plethora of upcoming space missions planned for the next couple of decades, the cislunar regime will be the next frontier. A dedicated satellite constellation around the moon and a dedicated relay system in cislunar space can greatly enhance the efficiency of accessing Earth, additionally also acting as a sustainable means of deep-space communication. This thesis work aims to analyze an initial design architecture motivated from NASA, ESA and JAXA's LunaNet concept with a stable lunar constellation model (specifically the Elliptical Lunar Frozen Orbits) with relay satellites acting as gateways between Earth and Lunar network nodes. Moreover, various forms of delay and disruptive scenarios are designed to stress-test the communication and navigation performances for various types of lunar users. The validation of high-fidelity cislunar dynamics is implemented in Ansys STK simulation and the performance analysis is derived using the developed simulation framework called, SelenoNet and its core deep-space communication and navigation process architecture.en
dc.description.degreeMaster of Scienceen
dc.format.mediumETDen
dc.identifier.othervt_gsexam:47155en
dc.identifier.urihttps://hdl.handle.net/10919/143343en
dc.language.isoenen
dc.publisherVirginia Techen
dc.rightsCreative Commons Attribution 4.0 Internationalen
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/en
dc.subjectData driven simulationen
dc.subjectElliptical constellationsen
dc.subjectDelay Tolerant Networksen
dc.titleDesign and Development of Fault Tolerant Lunar Satellite Network and Navigation Architectureen
dc.typeThesisen
thesis.degree.disciplineAerospace Engineeringen
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen
thesis.degree.levelmastersen
thesis.degree.nameMaster of Scienceen

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