The Deep Space Network Scheduling Problem
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NASA's STEREO Mission
NASA’s STEREO Mission J.B. Gurman STEREO Project Scientist W.T. Thompson STEREO Chief Observer Solar Physics Laboratory, Helophysics Division NASA Goddard Space Flight Center 1 The STEREO Mission • Science and technology definition team report, 1997 December: • Understand the origin and consequences of coronal mass ejections (CMEs) • Two spacecraft in earth-leading and -lagging orbits near 1 AU (Solar Terrestrial Probe line) • “Beacon” mode for near-realtime warning of potentially geoeffective events 2 Level 1 Requirements • Understand the causes and mechanisms of CME initiation • Characterize the propagation of CMEs through the heliosphere • Discover the mechanisms and sites of energetic particle acceleration in the low corona and the interplanetary medium • Develop a 3D, time-dependent model of the magnetic topology, temperature, density, and velocity structure of the ambient solar wind 3 Implementation • Two nearly identical spacecraft launched by a single ELV • Bottom spacecraft in stack has adapter ring, some strengthening • Spacecraft built at Johns Hopkins University APL • Four science investigations 4 Scientific Instruments • S/WAVES - broad frequency response RF detection of Type II, III bursts • PLASTIC - solar wind plasma and suprathermal ion composition measurements • IMPACT - energetic electrons and ions, magnetic field • SECCHI - EUV, coronagraphs and heliospheric imagers (surface to 1.5 AU) 5 Instrument Hardware • PLASTIC IMPACT boom IMPACT boom SECCHI SCIP SECCHI HI S/WAVES 6 Orbit Design • Science team selected a separation -
Nustar Observatory Guide
NuSTAR Guest Observer Program NuSTAR Observatory Guide Version 3.2 (June 2016) NuSTAR Science Operations Center, California Institute of Technology, Pasadena, CA NASA Goddard Spaceflight Center, Greenbelt, MD nustar.caltech.edu heasarc.gsfc.nasa.gov/docs/nustar/index.html i Revision History Revision Date Editor Comments D1,2,3 2014-08-01 NuSTAR SOC Initial draft 1.0 2014-08-15 NuSTAR GOF Release for AO-1 Addition of more information about CZT 2.0 2014-10-30 NuSTAR SOC detectors in section 3. 3.0 2015-09-24 NuSTAR SOC Update to section 4 for release of AO-2 Update for NuSTARDAS v1.6.0 release 3.1 2016-05-10 NuSTAR SOC (nusplitsc, Section 5) 3.2 2016-06-15 NuSTAR SOC Adjustment to section 9 ii Table of Contents Revision History ......................................................................................................................................................... ii 1. INTRODUCTION ................................................................................................................................................... 1 1.1 NuSTAR Program Organization ..................................................................................................................................................................................... 1 2. The NuSTAR observatory .................................................................................................................................... 2 2.1 NuSTAR Performance ........................................................................................................................................................................................................ -
Collision Avoidance Operations in a Multi-Mission Environment
AIAA 2014-1745 SpaceOps Conferences 5-9 May 2014, Pasadena, CA Proceedings of the 2014 SpaceOps Conference, SpaceOps 2014 Conference Pasadena, CA, USA, May 5-9, 2014, Paper DRAFT ONLY AIAA 2014-1745. Collision Avoidance Operations in a Multi-Mission Environment Manfred Bester,1 Bryce Roberts,2 Mark Lewis,3 Jeremy Thorsness,4 Gregory Picard,5 Sabine Frey,6 Daniel Cosgrove,7 Jeffrey Marchese,8 Aaron Burgart,9 and William Craig10 Space Sciences Laboratory, University of California, Berkeley, CA 94720-7450 With the increasing number of manmade object orbiting Earth, the probability for close encounters or on-orbit collisions is of great concern to spacecraft operators. The presence of debris clouds from various disintegration events amplifies these concerns, especially in low- Earth orbits. The University of California, Berkeley currently operates seven NASA spacecraft in various orbit regimes around the Earth and the Moon, and actively participates in collision avoidance operations. NASA Goddard Space Flight Center and the Jet Propulsion Laboratory provide conjunction analyses. In two cases, collision avoidance operations were executed to reduce the risks of on-orbit collisions. With one of the Earth orbiting THEMIS spacecraft, a small thrust maneuver was executed to increase the miss distance for a predicted close conjunction. For the NuSTAR observatory, an attitude maneuver was executed to minimize the cross section with respect to a particular conjunction geometry. Operations for these two events are presented as case studies. A number of experiences and lessons learned are included. Nomenclature dLong = geographic longitude increment ΔV = change in velocity dZgeo = geostationary orbit crossing distance increment i = inclination Pc = probability of collision R = geostationary radius RE = Earth radius σ = standard deviation Zgeo = geostationary orbit crossing distance I. -
Contention-Free Periodic Message Scheduler Medium Access Control in Wireless Sensor / Actuator Networks
Contention-Free Periodic Message Scheduler Medium Access Control in Wireless Sensor / Actuator Networks Thomas W. Carley Moussa A. Ba Rajeev Barua David B. Stewart ECE Department Embedded Research ECE Department Embedded Research University of Maryland Solutions University of Maryland Solutions [email protected] mba@embedded- [email protected] dstewart@embedded- zone.com zone.com Abstract actuator network applications have timeliness constrains, both on activities on individual nodes, and across multiple This paper presents a time division multiple access nodes. This results in timeliness constraints on both tasks medium access control protocol for wireless sensor / running on nodes and messages exchanged by nodes. actuator networks implemented with a contention-free Medium access control (MAC) is one of the most message scheduler. A message scheduler is used to important, and most studied, protocol layers in wireless determine which message has access to the medium at sensor / actuator networks. Wireless sensor / actuator any time. A set of messages is contention-free if only one networks are often characterized by extreme constraints message is ready at a time. Otherwise, some other on size, cost, power, and timeliness. This imposes criterion such as priority must be used to resolve constraints on every aspect of the design of these contention. In this case the message scheduler at each networks, especially the protocol stack. Wireless node in the network must schedule all messages in order networks are inherently broadcast media; all nodes in the to resolve contention. If the schedule is contention-free network share one common communication medium. however, then each node only schedules the messages that Therefore, a method for resolving contention when interest it. -
Open Dissertation Draft Revised Final.Pdf
The Pennsylvania State University The Graduate School ICT AND STEM EDUCATION AT THE COLONIAL BORDER: A POSTCOLONIAL COMPUTING PERSPECTIVE OF INDIGENOUS CULTURAL INTEGRATION INTO ICT AND STEM OUTREACH IN BRITISH COLUMBIA A Dissertation in Information Sciences and Technology by Richard Canevez © 2020 Richard Canevez Submitted in Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy December 2020 ii The dissertation of Richard Canevez was reviewed and approved by the following: Carleen Maitland Associate Professor of Information Sciences and Technology Dissertation Advisor Chair of Committee Daniel Susser Assistant Professor of Information Sciences and Technology and Philosophy Lynette (Kvasny) Yarger Associate Professor of Information Sciences and Technology Craig Campbell Assistant Teaching Professor of Education (Lifelong Learning and Adult Education) Mary Beth Rosson Professor of Information Sciences and Technology Director of Graduate Programs iii ABSTRACT Information and communication technologies (ICTs) have achieved a global reach, particularly in social groups within the ‘Global North,’ such as those within the province of British Columbia (BC), Canada. It has produced the need for a computing workforce, and increasingly, diversity is becoming an integral aspect of that workforce. Today, educational outreach programs with ICT components that are extending education to Indigenous communities in BC are charting a new direction in crossing the cultural barrier in education by tailoring their curricula to distinct Indigenous cultures, commonly within broader science, technology, engineering, and mathematics (STEM) initiatives. These efforts require examination, as they integrate Indigenous cultural material and guidance into what has been a largely Euro-Western-centric domain of education. Postcolonial computing theory provides a lens through which this integration can be investigated, connecting technological development and education disciplines within the parallel goals of cross-cultural, cross-colonial humanitarian development. -
Slate XNS TSN Network Scheduler with Browser-Based Topology Modeling
Slate XNS TSN Network Scheduler with Browser-based Topology Modeling Key Benefits Intuitive graphical topology modeling Incremental scheduling of new components and data streams Open, standard configuration for any TSN device One-click scheduling for complex networks Optimized bandwidth use for non-scheduled traffic Slate XNS is a browser-based, user-friendly software that makes it easy to model topologies, create schedules and deploy configurations for TSN networks. Offline network configuration is made possible by the intuitive GUI which provides a topology view or table-based editor for managing components and data streams. Schedules are calculated with just one click via TTTech’s built-in scheduling engine, and network components are configured using open, standard YANG models. Topology Modeling Network Scheduler Graphical One-Click Scheduling The graphical view is ideal for modeling small and TTTech’s high performance scheduling engine is medium sized network topologies. New components built-in to the Slate XNS software. After building the can be added by dragging and dropping into the topology and defining the data streams, the schedule topology. Data streams can also be represented as can be created with just one click. Schedules can logical connections between components. even be updated incrementally when new components or data streams are added. Table-Based Slate XNS schedules IEEE 802.1Qbv and 802.1Qbu The table editor is designed for modeling large traffic as well as supporting cut-through data network topologies and mass editing. Components, streams. Scheduling can be adjusted to optimize data streams and other parameters can be inputted bandwidth for non-scheduled traffic. -
The Deep Space Network - a Technology Case Study and What Improvements to the Deep Space Network Are Needed to Support Crewed Missions to Mars?
The Deep Space Network - A Technology Case Study and What Improvements to the Deep Space Network are Needed to Support Crewed Missions to Mars? A Master’s Thesis Presented to Department of Telecommunications State University of New York Polytechnic Institute Utica, New York In Partial Fulfillment of the Requirements for the Master of Science Degree By Prasad Falke May 2017 Abstract The purpose of this thesis research is to find out what experts and interested people think about Deep Space Network (DSN) technology for the crewed Mars mission in the future. The research document also addresses possible limitations which need to be fix before any critical missions. The paper discusses issues such as: data rate, hardware upgrade and new install requirement and a budget required for that, propagation delay, need of dedicated antenna support for the mission and security constraints. The Technology Case Study (TCS) and focused discussion help to know the possible solutions and what everyone things about the DSN technology. The public platforms like Quora, Reddit, StackExchange, and Facebook Mars Society group assisted in gathering technical answers from the experts and individuals interested in this research. iv Acknowledgements As the thesis research was challenging and based on the output of the experts and interested people in this field, I would like to express my gratitude and appreciation to all the participants. A special thanks go to Dr. Larry Hash for his guidance, encouragement, and support during the whole time. Additionally, I also want to thank my mother, Mrs. Mangala Falke for inspiring me always. Last but not the least, I appreciate the support from Maricopa County Emergency Communications Group (MCECG) and Arizona Near Space Research (ANSR) Organization for helping me to find the experts in space and communications field. -
Complete List of Contents
Complete List of Contents Volume 1 Cape Canaveral and the Kennedy Space Center ......213 Publisher’s Note ......................................................... vii Chandra X-Ray Observatory ....................................223 Introduction ................................................................. ix Clementine Mission to the Moon .............................229 Preface to the Third Edition ..................................... xiii Commercial Crewed vehicles ..................................235 Contributors ............................................................. xvii Compton Gamma Ray Observatory .........................240 List of Abbreviations ................................................. xxi Cooperation in Space: U.S. and Russian .................247 Complete List of Contents .................................... xxxiii Dawn Mission ..........................................................254 Deep Impact .............................................................259 Air Traffic Control Satellites ........................................1 Deep Space Network ................................................264 Amateur Radio Satellites .............................................6 Delta Launch Vehicles .............................................271 Ames Research Center ...............................................12 Dynamics Explorers .................................................279 Ansari X Prize ............................................................19 Early-Warning Satellites ..........................................284 -
Hybrid Event-Time-Triggered Networked Control Systems: Scheduling-Event
Information Sciences 305 (2015) 269–284 Contents lists available at ScienceDirect Information Sciences journal homepage: www.elsevier.com/locate/ins Hybrid event-time-triggered networked control systems: Scheduling-event-control co-design ⇑ Shixi Wen a, Ge Guo a, , Wing Shing Wong b a School of Information Science and Technology, Dalian Maritime University, Dalian 116026, China b Department of Information Engineering, The Chinese University of Hong Kong, Hong Kong, China article info abstract Article history: This paper is concerned with the simultaneous stabilization of a collection of plants Received 19 August 2014 remotely controlled via a wireless network. The so-called most regular binary sequences Received in revised form 21 December 2014 (MRBSs) are used to allocate the limited network channels. To further reduce unnecessary Accepted 27 January 2015 transmissions, an event-triggered transmitter is introduced at each plant. Under the hybrid Available online 7 February 2015 event-time-triggered transmission strategy, a sufficient stability condition is derived for each plant. Then, a unified co-design framework is presented with which the scheduling Keywords: functions (i.e., the MRBSs), the event-triggering condition and the controller gains can be Networked control systems determined simultaneously. The main results are established using piecewise Lyapunov Capacity limitation Event-triggered transmission functional method and average dwell time technique. The effectiveness of the co-design Protocol sequence method is demonstrated by a numerical example. Scheduling-event-control co-design Ó 2015 Elsevier Inc. All rights reserved. 1. Introduction In wireless networked systems (such as wireless sensor networks) consisting of a large number of nodes, network capa- city limitation is often a serious issue. -
Graphpulse: an Event-Driven Hardware Accelerator for Asynchronous Graph Processing
2020 53rd Annual IEEE/ACM International Symposium on Microarchitecture (MICRO) GraphPulse: An Event-Driven Hardware Accelerator for Asynchronous Graph Processing Shafiur Rahman Nael Abu-Ghazaleh Rajiv Gupta Computer Science and Engineering Computer Science and Engineering Computer Science and Engineering University of California, Riverside University of California, Riverside University of California, Riverside Riverside, USA Riverside, USA Riverside, USA [email protected] [email protected] [email protected] Abstract—Graph processing workloads are memory intensive GraphLab [31], GraphX [16], PowerGraph [17], Galois [37], with irregular access patterns and large memory footprint result- Giraph [4], GraphChi [28], and Ligra [49]. ing in low data locality. Their popular software implementations Large scale graph processing introduces a number of chal- typically employ either Push or Pull style propagation of changes through the graph over multiple iterations that follow the Bulk lenges that limit performance on traditional computing systems. Synchronous Model. The performance of these algorithms on First, memory-intensive processing stresses the memory system. traditional computing systems is limited by random reads/writes Not only is the frequency of memory operations relative of vertex values, synchronization overheads, and additional over- to compute operations high, the memory footprints of the heads for tracking active sets of vertices or edges across iterations. graph computations are large. Standard techniques in modern In this paper, we present GraphPulse, a hardware framework for asynchronous graph processing with event-driven schedul- processors for tolerating high memory latency, such as caching ing that overcomes the performance limitations of software and prefetching, have limited impact because irregular graph frameworks. Event-driven computation model enables a parallel computations lack data locality. -
The Deep Space Network: a Functional Description
Chapter 2 The Deep Space Network: A Functional Description Jim Taylor All deep-space missions—defined as those operating at or beyond the orbit of the Earth’s Moon—require some form of telecommunications network with a ground system to transmit to and receive data from the spacecraft. The Deep Space Network or DSN is one of the largest and most sophisticated of such networks. NASA missions in low Earth orbit communicate through either the Near Earth Network (NEN) or the SN (Space Network), with the SN, both operated by the NASA Goddard Space Flight Center (GSFC). The SN has of a number of Tracking and Data Relay Satellites (TDRS) in geosynchronous orbits. In addition, the European Space Agency operates a number of ground stations that may be used to track NASA deep space missions during the hours after launch. In addition, commercial companies operate ground stations that can communicate with NASA missions. The remainder of this book describes only the Deep Space Network operated for NASA by JPL. The lessons and techniques of the DSN replicate many comparable issues of the other networks. The lessons from the missions described in the following chapters are widely applicable to all deep space telecommunications systems. This includes post-launch support that was negotiated and planned using stations belonging to networks other than the DSN. The description and performance summary of the DSN in this chapter come from the DSN Telecommunications Link Design Handbook, widely known 15 16 Chapter 2 within NASA as the 810-5 document [1]. This modular handbook has been approved by the DSN Project Office, and its modules are updated to define current DSN capabilities. -
The Orion Spacecraft As a Key Element in a Deep Space Gateway
The Orion Spacecraft as a Key Element in a Deep Space Gateway A Technical Paper Presented by: Timothy Cichan Lockheed Martin Space [email protected] Kerry Timmons Lockheed Martin Space [email protected] Kathleen Coderre Lockheed Martin Space [email protected] Willian D. Pratt Lockheed Martin Space [email protected] July 2017 © 2014 Lockheed Martin Corporation Abstract With the Orion exploration vehicle and Space Launch System (SLS) approaching operational status, NASA and the international community are developing the next generation of habitats to serve as a deep space platform that will be the first of its kind, a cislunar Deep Space Gateway (DSG). The DSG is evolvable, flexible, and modular. It would be positioned in the vicinity of the Moon and allow astronauts to demonstrate they can operate for months at a time well beyond Low Earth Orbit. Orion is the next generation human exploration spacecraft being developed by NASA. It is designed to perform deep space exploration missions, and is capable of carrying a crew of 4 astronauts on independent free-flight missions up to 21 days, limited only by consumables. Because Orion meets the strict requirements for deep space flight environments (reentry conditions, deep-space communications, safety, radiation, and life support for example) it is a key element in a DSG and is more than just a transportation system. Orion has the capability to act as the command deck of any deep space piloted vehicle. To increase affordability and reduce the complexity and number of subsystem functions the early DSG must be responsible for, the DSG can leverage these unique deep space qualifications of Orion.