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2008
A document describes the Interplanetary Overlay Networking Protocol Accelerator (IONAC) an electronic apparatus, now under development, for relaying data at high rates in spacecraft and interplanetary radio-communication systems utilizing a delay-tolerant networking protocol. The protocol includes provisions for transmission and reception of data in bundles (essentially, messages), transfer of custody of a bundle to a recipient relay station at each step of a relay, and return receipts. Because of limitations on energy resources available for such relays, data rates attainable in a conventional software implementation of the protocol are lower than those needed, at any given reasonable energy-consumption rate. Therefore, a main goal in developing the IONAC is to reduce the energy consumption by an order of magnitude and the data-throughput capability by two orders of magnitude. The IONAC prototype is a field-programmable gate array that serves as a reconfigurable hybrid (hardware/ f...
2006
NASA's demonstration of the successful transmission of relay data through the orbiting Mars Odyssey, Mars Global Surveyor, and Mars Express by the Mars Exploration Rovers has shown not only the benefit of using a relay satellite for multiple landed assets in a deep space environment but also the benefit of international standards for such an architecture. As NASA begins the quest defined in the Vision for Exploration with robotic and manned missions to the Moon, continues its study of Mars, and is joined in these endeavors by countries worldwide , landed assets transmitting data through relay satellites will be crucial for completing mission objectives. However, this method of data delivery will result in increased complexity in routing and prioritization of data transmission as the number of missions increases. Also, there is currently no standard method among organizations conducting such missions to return these data sets to Earth given a complex environment. One possibility for establishing such a standard is for mission designers to deploy protocols which fall under the umbrella of Delay Tolerant Networking (DTN). These developing standards include the Bundle Protocol (BP) which provides a standard, secure, store and forward mechanism designed for high latency and asymmetric communication links and the Licklider Transmission Protocol (LTP) which is used to provide a reliable deep space link transmission service.
International Journal On Advances in Internet Technology, 2010
Abstract: In the last few years deep space exploration missions are undergoing a significant transformation as are the expectations of their scientific investigators and the public who participate in these experiences. National Aeronautics and Space Administration (NASA) and European Space Agency (ESA), recently, decided pursuing a mission to study Jupiter and its moons, and another to visit the largest moons of Saturn. Those missions need new communication and networking infrastructures able to support space exploration, to ...
International Journal of Astrobiology, 2020
The paper describes the architecture for a data repository and distribution system to be used in the case of a SETI detection event. This system is conceptually modelled after the Deep Space Network, although the hardware and infrastructure involved are different and substantially less expensive to operate. The system is designed to accommodate a large number of users from a variety of fields who wish to contribute to the analysis and comprehension effort that would follow the detection of an information-bearing signal.
2009
Achieving NASA's lunar and Mars exploration objectives will require significant advances in space-qualified communications systems. The communications capabilities required by lunar missions and beyond cannot be supported through simple, point-to-point radio communications. While such radio links will may provide basic elements of the system, the number of communications sources, sensors, radios, etc. will necessitate the formation of networks. These networks will require the ability to form automatically, adapt to changing topologies, recover from faults, compensate for interference or other external factors inhibiting communications, and additional capabilities as mission needs evolve over the life of their deployment. The communications systems supporting these missions will require significant advances in the architecture and design over current systems. This paper presents work in progress to meet the needs of the next generation space-based communications and networking.
2013
NASA proposes to develop a common infrastructure for all its forthcoming space exploration missions. This infrastructure called the Interplanetary Internet (IPN) will take the Internet of the Earth to outside planets and facilitate in the efficient transfer of the huge amount of scientific data collected by the space probes back to Earth. The development of an efficient transport protocol for the Interplanetary Internet is a major challenge to the research community. In this paper, a survey has been done for all the major transport protocols developed for deep space communication. The paper discusses the infrastructure of the IPN along with the major challenges for deep space communication. Emphasis has been made on the issues of transport protocol design for LEO-GEO based satellite networks and deep space communication networks. The genesis of the work on Interplanetary Internet and the evolution of the concept of Delay Tolerant Networks have been explained. An attempt has been mad...
2002
This paper presents work being done at NASA/GSFC by the Operating Missions as Nodes on the Internet (OMNI) project to demonstrate the application of Internet communication technologies to space communication. The goal is to provide global addressability and standard network protocols and applications for future space missions. It describes the communication architecture and operations concepts that will be deployed and tested on a Space Shuttle flight scheduled to fly in August 2002. This is a NASA Hitchhiker mission called Communication and Navigation Demonstration On Shuttle (CANDOS). The mission will be using a small programmable transceiver mounted in the Shuttle bay that can communicate through NASA's ground tracking stations as well as NASA's space relay satellite system. The transceiver includes a processor running the Linux operating system and a standard synchronous serial interface that supports the High-level Data Link Control (HDLC) framing protocol. One of the main goals will be to test the operation of the Mobile IP protocol (RFC 2002) for automatic routing of data as the Shuttle passes from one contact to another. Other protocols to be utilized onboard CANDOS include secure login (SSH), UDP-based reliable file transfer (MDP), and blind commanding using UDP. The paper describes how each of these standard protocols available in the Linux operating system can be used to support communication with a space vehicle. It will discuss how each protocol is suited to support the range of special communication needs of space missions.
SpaceOps 2012 Conference, 2012
The goal of the "Space-Data Routers" (SDR) project is to explore concepts for an enhanced architecture for the exploitation of space data capable of mitigating current availability limitations with respect to volume, timeliness, and continuity. The objective is to establish a mission / application-oriented communication overlay for data dissemination on Earth and to include into this overlay space born sources and network nodes. Technically, that is achieved by deploying the Delay Tolerant Networking (DTN) stack and integrating the interfaces of various Space and Internet communication and networking protocols, including TM/TC, Space Packets, and AOS along with Ethernet, TCP/IP and UDP. In addition, the overlay supports and enforces policies for resource and data sharing as well as for data dissemination. These concepts will be implemented through the development of the Space-Data Router, a DTN-enabled device that will interconnect space data providers, ground stations, research centers, and academic institutions in a much more efficient and decentralized manner than today. I. Overview Space data exploitation by research centers and academic institutes today is constrained by limitation in the access to scientific data with respect to volume, timeliness, and continuity. Typically data are collected and preprocessed by space data collection centers and are then distributed from there according to the orders placed by the user community. In many cases order management and dissemination of data still requires human interaction and this implies considerable bureaucratic overhead. Direct access to real-time data downlinked from Earth Observation (EO) spacecraft is sometimes available but is then typically limited to the pass over the ground station used and of
This paper presents a simplified SpaceWire network architecture to overcome a challenging high-speed and real time packet switching process required in a baseband processing unit of a regenerative satellite payload as a part of the "On-Board Processing EHF (Extremely High Frequency) Satellite Transponder and Testbed Development Project". This is an R&D Project supported by the Scientific and Technological Research Council of Turkey (TUBITAK). With this project, an on-board processing geo-satellite transponder serving two spot beams will provide communications between satcom terminals. The baseband processing subsystem in this project takes part as the central unit by providing on-board processing power by using the state of the art space qualified FPGAs and Leon-3FT based processors. This subsystem, of which the internal network structure is discussed here, is currently being developed by Communications and Information Technologies Group of Aselsan A.Ş., Turkey.
The Topic of this paper is going to be about interplanetary telecommunications and networking. In the past decade, there have been many research studies conducted by National Aeronautics and Space Administration (NASA) scientists and other academic laboratories. Their focus has been on how to better communicate with spacecrafts, orbiters, and rovers on other planets. Initially, sending messages through space was done through radio waves. Each spacecraft, orbiter or rover had a receiver and transmitter that would interpret the information received and act on it.
IEEE Access, 2022
In [A8], Li et al. present a survey on laser communications 42 ranging from terminal, link, and architectures. In [A9], De Rango and Tropea propose a bundle manage-44 ment layer that can be coupled to routing approaches for 45 InterPlanetary Networks or Delay Tolerant Networks. The 46 authors show that the proposed approach brings significant 47 improvements in terms of delivery time when applied to 48 Earliest Arrival Optimal Delivery Ratio (EAODR) routing. The Guest Editors hope that this Special Section will bene-50 fit the scientific community and contribute to the knowledge 51 base for the next-generation internet, where satellite-based 52 networks are becoming an integrated part of the internet 53 infrastructure. The Guest Editors would like to take this 54 opportunity to applaud the contributions of the authors to this 55 Special Section.
2010
This paper reviews some of the possible architectures that can be used for the deployment of Interplanetary Internet. In fact, the task of optimizing space system architectures is very complex, and it is not possible to design and analyze all possible configurations. Therefore, it is useful to have a clear vision of a large set of possible configurations, so that a remarkable subset can be extracted to allow the successive design optimization. We considered spacecrafts orbiting around the planets, spacecrafts orbiting around the sun and spacecrafts orbiting around a Lagrangian point. Furthermore, Flower constellations are considered as a viable tool to optimize the visibility of the network nodes. 1 2
… , 2006. SMC-IT 2006. …, 2006
We present advanced technology developments in space networking achieved under the Interplanetary Network Directorate Information Technology Program. Progress has been made in three primary areas: (1) distributed on-board scheduling as it applies to communications, (2) middleware services, and (3) communications protocols. Demonstrations of these capabilities have been provided using a simulation environment capable of providing a realistic representation of the underlying space communications network environment.
SpaceOps 2002 Conference, 2002
Spacecraft applications that interact with on-board sensors, effectors, and major components have traditionally used private interfaces which are tightly bound to the interface details of the data links connecting these sub-systems. The latest spacecraft, which often include several powerful processors running real time operating systems, highspeed on-board networks, and intelligent peripherals, can support a more layered networked environment. Use of standard interfaces and networked elements is expected to yield reusable software and hardware components. Within CCSDS Panel 1K we have been developing such on-board interface standards. This paper will present a Message Transfer Service that defines a common API for use within a single spacecraft or among spacecraft flying in a constellation.
22nd AIAA International Communications Satellite Systems Conference & Exhibit 2004 (ICSSC), 2004
Space communications architecture concepts play a key role in the development and deployment of NASA's future exploration and science missions. Once a mission is deployed, the communication link to the user needs to provide maximum information delivery and flexibility to handle the expected large and complex data sets and to enable direct interaction with the spacecraft and experiments. In human and robotic missions, communication systems need to offer maximum reliability with robust two-way links for software uploads and virtual interactions. Identifying the capabilities to cost effectively meet the demanding space communication needs of 21 st century missions, proper formulation of the requirements for these missions, and identifying the early technology developments that will be needed can only be resolved with architecture design. This paper will describe the development of evolvable space communication architecture models and the technologies needed to support Earth sensor web and collaborative observation formation missions; robotic scientific missions for detailed investigation of planets, moons, and small bodies in the solar system; human missions for exploration of the Moon, Mars, Ganymede, Callisto, and asteroids; human settlements in space, on the Moon, and on Mars; and great in-space observatories for observing other star systems and the universe. The resulting architectures will enable the reliable, multipoint, high data rate capabilities needed on demand to provide continuous, maximum coverage of areas of concentrated activities, such as in the vicinity of outposts inspace, on the Moon or on Mars.
Lecture Notes of the Institute for Computer Sciences, Social Informatics and Telecommunications Engineering, 2010
In the framework of the so called InterPlaNetary (IPN) Internet, the paper surveys possible advanced communications and networking solutions applied by a specific IPN node architecture. The proposed solutions have been preliminarily evaluated by using the ns2 simulator by considering possible network status changes due to the nodes' movements, typical in the deep space scenario. In particular, the performance study on one hand highlights the role of the Multicast and, on the other hand, it shows the effects of new possible control approaches such as the dynamic Link Selection in the IPN network. The performance study represents the main paper contribution.
24th AIAA International Communications Satellite Systems Conference, 2006
NASA is planning a series of short and long duration human and robotic missions to explore the Moon and then Mars. A key objective of these missions is to grow, through a series of launches, a system of systems infrastructure with the capability for safe and sustainable autonomous operations at minimum cost while maximizing the exploration capabilities and science return. An incremental implementation process will enable a buildup of the communication, navigation, networking, computing, and informatics architectures to support human exploration missions in the vicinities and on the surfaces of the Moon and Mars. These architectures will support all space and surface nodes, including other orbiters, lander vehicles, humans in spacesuits, robots, rovers, human habitats, and pressurized vehicles. This paper describes the integration of an innovative MAC and networking technology with an equally innovative position-dependent, data routing, network technology. The MAC technology provides the relay spacecraft with the capability to autonomously discover neighbor spacecraft and surface nodes, establish variable-rate links and communicate simultaneously with multiple in-space and surface clients at varying and rapidly changing distances while making optimum use of the available power. The networking technology uses attitude sensors, a time synchronization protocol and occasional orbit-corrections to maintain awareness of its instantaneous position and attitude in space as well as the orbital or surface location of its communication clients. A position-dependent data routing capability is used in the communication relay satellites to handle the movement of data among any of multiple clients (including Earth) that may be simultaneously in view; and if not in view, the relay will temporarily store the data from a client source and download it when the destination client comes into view. The integration of the MAC and data routing networking technologies would enable a relay satellite system to provide end-toend communication services for robotic and human missions in the vicinity, or on the surface of the Moon with a minimum of Earth-based operational support.
Acta Astronautica, 2003
IEEE Communications Magazine, 2003
International Space Station: The Next Space Marketplace, 2000
During the past five years, using NASA's Advanced Communications Technology Satellite (ACTS), a group of NASA and industry participants have performed a series of experiments focusing on the interoperability of TCP lIP, ATM, and higher layer protocols and applications. These experiments have yielded very exciting results, including pro-forma configurations in the following areas: TCP lIP data transfer over geostationary satellite delays at speeds exceeding 500 Megabits per second using standard network hardware, computers, and operating systems Video, audio, and telephony over satellite links using ATM to engineer links with a constant Quality of Service for these time-sensitive applications Security overlays featuring encryption and IP firewalls at up to 155 Megabits per second Mobile satellite terminals that operate on ships, trucks, aircraft, and (eventually) spacecraft. This paper describes a proposed communications payload for the International Space Station, which supports the use of commodity industry-standard communications protocols to support direct user access to science instruments and experiment payloads from the ground. The payload concept, which is based entirely on commercial off-the-shelf products, was developed as a result of the five-year ACTS experiments program. 195
2003
Traditional NASA missions, both near Earth and deep space, have been stove-pipe in nature and point-topoint in architecture. Recently, NASA and others have conceptualized missions that required space-based networking. The notion of networks in space is a drastic shift in thinking and requires entirely new architectures, radio systems (antennas, modems, and media access) and possibly new protocols. A full system engineering approach for some key mission architectures will occur which considers issues such as the science being performed, station keeping, antenna size, contact time, data rates, radio-link power requirements, media access techniques, and appropriate networking and transport protocols. This paper highlights preliminary architecture concepts and key technologies that will be investigated.
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