Survey of Inter-satellite Communication for Small Satellite Systems: Physical Layer to Network Layer View

Small satellite systems enable whole new class of missions for navigation, communications, remote sensing and scientific research for both civilian and military purposes. As individual spacecraft are limited by the size, mass and power constraints, mass-produced small satellites in large constellations or clusters could be useful in many science missions such as gravity mapping, tracking of forest fires, finding water resources, etc. Constellation of satellites provide improved spatial and temporal resolution of the target. Small satellite constellations contribute innovative applications by replacing a single asset with several very capable spacecraft which opens the door to new applications. With increasing levels of autonomy, there will be a need for remote communication networks to enable communication between spacecraft. These space based networks will need to configure and maintain dynamic routes, manage intermediate nodes, and reconfigure themselves to achieve mission objectives. Hence, inter-satellite communication is a key aspect when satellites fly in formation. In this paper, we present the various researches being conducted in the small satellite community for implementing inter-satellite communications based on the Open System Interconnection (OSI) model. This paper also reviews the various design parameters applicable to the first three layers of the OSI model, i.e., physical, data link and network layer. Based on the survey, we also present a comprehensive list of design parameters useful for achieving inter-satellite communications for multiple small satellite missions. Specific topics include proposed solutions for some of the challenges faced by small satellite systems, enabling operations using a network of small satellites, and some examples of small satellite missions involving formation flying aspects.Comment: 51 pages, 21 Figures, 11 Tables, accepted in IEEE Communications Surveys and Tutorial

Towards the deployment of software defined networks over satellites - an in-laboratory demonstration for GEO satellite services

Traditional satellite communications missions are based on artificial satellites that can communicate with ground stations. This type of network provides wide-area coverage as well as resilient communications. Satellite systems are expected to be merged with the introduction of 5G/6G mobile systems to offer seamless connection and ubiquitous coverage for users worldwide. SDN/NFV are two of the most important enabling technologies for deploying new 5G/6G mobile network architectures, and they are widely used in telecommunications to deliver different services. Its method is based on network softwarization, which abstracts the physical infrastructure by separating the functionality of the hardware. Furthermore, using SDN, it is possible to reconfigure the network in flexible topologies that adapt to the performance necessary at any given time, thereby maximizing resources and lowering costs. SDN/NFV, on the other hand, relies on a strong and continuous network layer to construct a control plane and deploy VNF. However, establishing a stable link is difficult in constellations of several LEO/MEO satellites. TALENT is a software platform created with the purpose of supplying satellite and ground connection by coordinating satellite and terrestrial systems from a single location, developed under the SaTG5 project that defined the integration of satellite solutions for 5G. Regardless of these solutions, a robust testbed is required to help in the discovery of novel protocols for delivering and orchestrating network services over satellite networks that take dynamic network architecture on satellite constellations into account. This thesis addresses the lack of a testbed for deploying VNF via a satellite network, as well as the orchestration and deployment of VNF across various satellite constellations. Its main contribution is an update to TALENT to allow it to work with newer Open Source MANO versions, and a testbed for deploying a VNF across a simulated satellite network based on the OpenSand satellite simulation tool.Objectius de Desenvolupament Sostenible::9 - Indústria, Innovació i Infraestructur

Distributed Spacecraft Mission (DSM) Plume Design Reference Mission (DRM) Inter-Satellite Link Modeling, Analysis, and Simulation

NASA Goddard Space Flight Center (GSFC) Radical Innovation Initiative (R12) plans to focus intently on DSM capability advancements in FY22-24. A DSM mission involves multiple spacecraft, arranged in a constellation, to achieve one or more common goals via the use of inter-satellite links (ISL) between the satellites. Recently, the GSFC Internal Research & Development (IRAD) program established Enceladus as a design reference mission (DRM) for the current DSM effort to foster the conceptual development of communication architecture, requirements, and solutions for future DSM ISL, as well as being able to push other research areas of interest. Enceladus is an icy moon of the planet Saturn. The DRM Enceladus mission concept involves a constellation of 24 small satellites, orbiting Enceladus around 100 km altitude in 3 planes, as observing nodes for science measurement. The mission science data will be sent back to Earth through a relay orbiting Saturn, using the constellation\u27s inter-satellite links. A QualNet/STK simulation model of the Relay and constellation ISL optical and RF links is developed for the design and optimization of the link and orbital parameters, as well as the inter-networking protocols. Delay Tolerant Networking (DTN) is utilized in the application layer modeling. This paper describes the plume DRM mission concept of an Enceladus constellation to relay science data to Earth and includes the proposed communication architecture and operation concepts. We present details of the QualNet/STK engineering model for this communication scenario to simulate the end-to-end data traffic through multiple layers (physical, data link, networking, transport and application). A link analysis for the constellation\u27s ISL, constellation to Relay and Direct to Earth (DTE) optical link is provided and discussed. The results of end-to-end traffic simulation for the data throughout/latency evaluation and assessment of the communication architecture are presented. The investigation of the concept of optical multiple access (OMA) for the Plume DRM is discussed. The modeling and simulation methodology developed in this paper is applicable to other DSMs in near Earth and deep space such as Earth-Moon L1/L2 and Lunar regions

OPTIMIZATION OF INTER-CUBESAT COMMUNICATION LINKS

Cubesat constellations may become the next generation of communication backbone architecture to provide future worldwide communication services. In this thesis, we investigate the feasibility of deploying Cubesat constellations with inter-satellite links (ISL) for the delivery of continuous global communication. Cubesat constellation designs for various mission scenarios are proposed and verified using a simulation toolkit commonly used by space engineers. Link optimization to improve the overall theoretical data rate is also discussed. The results obtained affirm that a Cubesat constellation at an orbital height of 450 km can achieve a data rate of 11.46 kbps and requires the least number of satellites in the constellation. We ascertained that using ISL as the communication backbone in a network architecture, complete with space and globally distributed ground nodes, is achievable. In the near future, there is a high potential for the implementation of ISL with optical communication links, whereby there is assurance of a significantly higher data rate and lower power requirements.Civilian, Singapore Technologies ElectronicsApproved for public release; distribution is unlimited

A Wised Routing Protocols for Leo Satellite Networks

This Study proposes a routing strategy of combining a packet scheduling with congestion control policy that applied for LEO satellite network with high speed and multiple traffic. It not only ensures the QoS of different traffic, but also can avoid low priority traffic to be "starve" due to their weak resource competitiveness, thus it guarantees the throughput and performance of the network. In the end, we set up a LEO satellite network simulation platform in OPNET to verify the effectiveness of the proposed algorithm.Comment: The 10th Asian Control Conference (ASCC), Universiti Teknologi Malaysia, Malaysi

Architectural Model for Evaluating Space Communication Networks

[ANGLÈS] The space exploration endeavor started in 1957 with the launch and operation of the first manmade satellite, the URSS Sputnik 1. Since then, multiple space programs have been developed, pushing the limits of technology and science but foremost unveiling the mysteries of the universe. In all these cases, the need for flexible and reliable communication systems has been primordial, allowing the return of collected science data and, when necessary, ensuring the well-being and safety of astronauts. To that end, multiple space communication networks have been globally deployed, be it through geographically distributed ground assets or through space relay satellites. Until now most of these systems have relied upon mature technology standards that have been adapted to the specific needs of particular missions and customers. Nevertheless, current trends in the space programs suggest that a shift of paradigm is needed: an Internet-like space network would increase the capacity and reliability of an interplanetary network while dramatically reducing its overall costs. In this context, the System Architecting Paradigm can be a good starting point. Through its formal decomposition of the system, it can help determine the architecturally distinguishing decisions and identify potential areas of commonality and cost reduction. This thesis presents a general framework to evaluate space communication relay systems for the near Earth domain. It indicates the sources of complexity in the modeling process, and discusses the validity and appropriateness of past approaches to the problem. In particular, it proposes a discussion of current models vis-à-vis the System Architecting Paradigm and how they fit into tradespace exploration studies. Next, the thesis introduces a computational performance model for the analysis and fast simulation of space relay satellite systems. The tool takes advantage of a specifically built-in rule-based expert system for storing the constitutive elements of the architecture and perform logical interactions between them. Analogously, it uses numerical models to assess the network topology over a given timeframe, perform physical layer computations and calculate plausible schedules for the overall system. In particular, it presents a newly developed heuristic scheduler that guarantees prioritization of specific missions and services while ensuring manageable computational times.[CASTELLÀ] El inicio de la carrera espacial se inició en 1957 con el lanzamiento y operación del primer satélite artificial, el Sputnik 1 de la URSS. Desde entonces se han desarrollado múltiples programas espaciales que han llevado al límite tanto la tecnología como la ciencia y han permitido desvelar los misterios del universo. En todos estos casos, la necesidad de sistemas de comunicación flexibles y fiables ha sido primordial con el fin de asegurar el retorno de los datos científicos recopilados y, en ciertos casos, garantizar la seguridad de los astronautas. Como consecuencia, múltiples redes de comunicaciones espaciales han sido desplegadas, ya sea a través de antenas globalmente distribuidas a través de la superficie terrestre o mediante satélites repetidores. Hasta ahora la mayoría de estos sistemas se ha basado en estándares tecnológicos maduros y testeados, los cuales se han adaptado con el fin de satisfacer las necesidades específicas de cada misión y cliente. Sin embargo, las tendencias actuales en el diseño de los nuevos programas espaciales indica que un cambio de paradigma es necesario: una red espacial a imagen de Internet permitiría incrementar la capacidad y fiabilidad de las comunicaciones interplanetarias y, a la vez, reducir dramáticamente sus costes. En este contexto, el paradigma de arquitectura de sistemas puede ser un buen punto de partida. Mediante la descomposición formal del sistema, puede ayudar a determinar las decisiones que tienen un impacto cabal en el diseño de la arquitectura así como identificar las áreas con tecnologías similares y de menor coste. Esta tesis presenta un marco teórico general para evaluar sistemas de comunicaciones espaciales para misiones que orbitan la Tierra. Adicionalmente, la tesis indica los principales orígenes de complejidad durante el modelado del sistema y presenta una discusión sobre la validez de anteriores estrategias para analizar el problema. En concreto, propone una comparación de anteriores modelos respecto el paradigma de arquitectura de sistemas y su grado de adecuación para evaluar y comprar arquitecturas. A continuación, la tesis introduce un modelo computacional para simular y evaluar el rendimiento de sistemas de repetidores por satélite. La herramienta utiliza un rule-based expert system específicamente diseñado con el fin de almacenar los principales elementos constitutivos de la arquitectura y comprender las interacciones lógicas entre ellos. Análogamente, el modelo usa métodos numéricos con el fin de calcular la evolución temporal de la topología de la red en un determinado intervalo de tiempo, así como su capa física y un posible programa de contactos. En concreto, presenta un nuevo scheduler heurístico que garantiza la correcta ordenación de las misiones y servicios a la vez que asegura un tiempo computacional aceptable.[CATALÀ] L'inici de la cursa espacial va iniciar-se l'any 1957 amb el llançament i operació del primer satèl·lit artificial, l'Sputnik 1 de la URSS. Des d'aleshores s'han dut a terme múltiples programes espacials que han portat al límit tant la tecnologia com la ciència i han permès desvelar els misteris de l'univers. En tots aquests casos, la necessitat de sistemes de comunicació flexibles i fiables ha sigut primordial per tal d'assegurar el retorn de les dades científiques recopilades i, en certs casos, garantir el benestar i seguretat dels astronautes. Com a conseqüència, múltiples xarxes de comunicacions espacials han sigut desplegades, ja sigui a través d'antenes globalment distribuïdes a través de la superfície terrestre o mitjançant satèl·lits repetidors. Fins ara la majoria d'aquests sistemes s'han basat en estàndards tecnològics madurs i testats, els quals s'han adaptat per tal de satisfer les necessitats específiques de cada missió i client. Això no obstant, les tendències actuals en el disseny dels nous programes espacials indica que un canvi de paradigma és necessari: una xarxa espacial a imatge d'Internet permetria incrementar la capacitat i fiabilitat de les comunicacions interplanetàries i, alhora, reduir dramàticament els seu costs. En aquest context, el paradigma d'arquitectura de sistemes pot ser un bon punt de partida. Mitjançant la descomposició formal del sistema, pot ajudar a determinar les decisions que tenen un impacte cabdal en el disseny de l'arquitectura així com permetre identificar àrees amb tecnologies similars i de menor cost. Aquesta tesi presenta un marc teòric general per avaluar sistemes de comunicacions espacials per missions orbitant la Terra. Addicionalment, la tesi indica els principals orígens de complexitat durant el modelatge del sistema i presenta una discussió sobre la validesa d'anteriors estratègies per analitzar el problema. En concret, proposa una comparació d'anteriors models respecte el paradigma d'arquitectura de sistemes i el seu grau d'adequació per avaluar i comparar arquitectures. A continuació, la tesi introdueix un model computacional per simular i avaluar el rendiment de sistemes de repetidors per satèl·lit. L'eina empra un rule-based expert system específicament dissenyat per tal d'emmagatzemar els principals elements constitutius de l'arquitectura i comprendre les interaccions lògiques entre ells. Anàlogament, el model utilitza mètodes numèrics per tal de calcular l'evolució temporal de la topologia de la xarxa en un determinat interval de temps, així com calcular la seva capa física i un possible programa de contactes. En concret, presenta un nou scheduler heurístic que garanteix la correcte ordenació de les missions i serveis tot assegurant un temps de computació acceptable

Electromagnetic Interference Estimation via Conditional Neural Processing

The goal of this thesis is to determine the efficacy of employing Machine Learning (ML) to solve Joint Urgent Operational Need (JUON) CC-0575, which aims to develop a Common Operating Picture (COP) of the Global Positioning System (GPS) Electromagnetic Interference (EMI) environment. With the growing popularity of Artificial Neural Networks (ANNs), ML solutions are quickly gaining traction in businesses, academia and government. This in turn allows for problem solutions that were previously inconceivable using the classical programming paradigm. This thesis proposes a method to develop a COP of the battlefield via ANN ingestion of multiple-source signals and sensors. We conduct three separate experiments with varying amounts of EMI interference sources (single, double, and triple jammer datasets). The type of ANN developed to address this problem is a Conditional Neural Process (CNP) with residual connections. The model is developed to provide the estimated EMI environment as well as a measure of confidence in its estimates, as the specific application of this model could lead to loss of life in the event the model estimates are taken as truth. The model resulted in an EMI estimator that was neutral on the single jammer test data set, yet aggressive on the multiple jammer test data sets