Starling1: Swarm Technology Demonstration
Total Page:16
File Type:pdf, Size:1020Kb

Load more
Recommended publications
-
CZ-Space Day Intro
16.7.2010 ESA TECHNOLOGY → PROGRAMMES AND STRATEGY Czech Space Technology Day - GSTP July 2010 CONTENTS • The European Space Agency -ESA • Space Technology • ESA’s Technology Programmes • Doing business with ESA • ESA’s Long Term Plan 2 1 16.7.2010 → THE EUROPEAN SPACE AGENCY PURPOSE OF ESA “To provide for and promote, for exclusively peaceful purposes, cooperation among European states in space research and technology and their space applications. ” - Article 2 of ESA Convention 4 2 16.7.2010 ESA FACTS AND FIGURES • Over 30 years of experience • 18 Member States • Five establishments, about 2000 staff • 3.7 billion Euro budget (2010) • Over 60 satellites designed, tested and operated in flight • 17 scientific satellites in operation • Five types of launcher developed • Over 190 launches 5 18 MEMBER STATES Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxembourg, Norway, the Netherlands, Portugal, Spain, Sweden, Switzerland and the United Kingdom. Canada takes part in some programmes under a Cooperation Agreement. Hungary, Romania, Poland, Slovenia, and Estonia are European Cooperating States. Cyprus and Latvia have signed Cooperation Agreements with ESA. 6 3 16.7.2010 ACTIVITIES ESA is one of the few space agencies in the world to combine responsibility in nearly all areas of space activity. • Space science • Navigation • Human spaceflight • Telecommunications • Exploration • Technology • Earth observation • Operations • Launchers 7 ESA PROGRAMMES All Member States participate (on In addition, -
Orbital Debris Quarterly News 22-1
National Aeronautics and Space Administration Orbital Debris Quarterly News Volume 22, Issue 1 February 2018 Inside... Two Anomalous Events in GEO Summer 2017 was marred by two apparently platform. Spacecraft dry mass is estimated to be on Space Debris Sensor anomalous events in the geosynchronous orbit the order of 2000 kg. On-board stored energy sources Launches Aboard (GEO) belt. Both incidents have been observed by include fuel and pressurized components, as well as the commercial space situation awareness providers, but as battery subsystem. SpaceX-13 2 of 26 December 2017 no debris from either event have The Indonesian GEO communications spacecraft entered the public catalog. TELKOM-1 (1999-042A, SSN catalog number 25880) SEM Analysis The GEO communications spacecraft AMC-9 experienced an energetic event on or about 25 August Results of (International Designator 2003-024A, U.S. Strategic 2017, after over 18.1 years on-orbit—3 years past Returned ISS Command [USSTRATCOM] Space Surveillance its nominal operational lifetime. An examination of Network [SSN] catalog number 27820), formerly known the Two Line Element data indicates an observable PMA-2 Cover 4 as GE-12, experienced an energetic event estimated to change in spacecraft orbit between 26 and 29 August. have occurred at approximately 07:10 GMT on 17 June At the beginning of this time interval, approximately CubeSat Study 2017, after approximately 14 years on-orbit. Fig. 1 Project Review 6 depicts the orbital evolution of the spacecraft in 2017. continued on page 2 SES, the spacecraft owner- operator, described this AMC‐9 (SSN 27820, 2003‐024A) 360 36300 Space Debris Sensor event as a “serious anomaly.” Installation 8 Following this event, the 36200 spacecraft began a westward 300 Monthly Object Type drift in the GEO belt. -
ACT-RPR-SPS-1110 Sps Europe Paper
62nd International Astronautical Congress, Cape Town, SA. Copyright ©2011 by the European Space Agency (ESA). Published by the IAF, with permission and released to the IAF to publish in all forms. IAC-11-C3.1.3 PROSPECTS FOR SPACE SOLAR POWER IN EUROPE Leopold Summerer European Space Agency, Advanced Concepts Team, The Netherlands, [email protected] Lionel Jacques European Space Agency, Advanced Concepts Team, The Netherlands, [email protected] In 2002, a phased, multi-year approach to space solar power has been published. Following this plan, several activities have matured the concept and technology further in the following years. Despite substantial advances in key technologies, space solar power remains still at the weak intersections between the space sector and the energy sector. In the 10 years since the development of the European SPS Programme Plan, both, the space and the energy sectors have undergone substantial changes and many key enabling technologies for space solar power have advanced significantly. The present paper attempts to take account of these changes in view to assess how they influence the prospect for space solar power work for Europe. Fresh Look Study as well as the work on a European I INTRODUCTION sail tower concept by Klimke and Seboldt [16], [17]. Based on these results, which re-confirmed the The concept of generating solar power in space and principal technical viability of space solar power transmitting it to Earth to contribute to terrestrial energy concepts, the focus of the first phase of the European systems has received period attention since P. Glaser SPS programme plan has been to enlarge the evaluation published the first engineering approach to it in 1968 scope of space solar power by including expertise from [1]. -
→ Space for Europe European Space Agency
number 153 | February 2013 bulletin → space for europe European Space Agency The European Space Agency was formed out of, and took over the rights and The ESA headquarters are in Paris. obligations of, the two earlier European space organisations – the European Space Research Organisation (ESRO) and the European Launcher Development The major establishments of ESA are: Organisation (ELDO). The Member States are Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxembourg, the ESTEC, Noordwijk, Netherlands. Netherlands, Norway, Poland, Portugal, Romania, Spain, Sweden, Switzerland and the United Kingdom. Canada is a Cooperating State. ESOC, Darmstadt, Germany. In the words of its Convention: the purpose of the Agency shall be to provide for ESRIN, Frascati, Italy. and to promote, for exclusively peaceful purposes, cooperation among European States in space research and technology and their space applications, with a view ESAC, Madrid, Spain. to their being used for scientific purposes and for operational space applications systems: Chairman of the Council: D. Williams (to Dec 2012) → by elaborating and implementing a long-term European space policy, by recommending space objectives to the Member States, and by concerting the Director General: J.-J. Dordain policies of the Member States with respect to other national and international organisations and institutions; → by elaborating and implementing activities and programmes in the space field; → by coordinating the European space programme and national programmes, and by integrating the latter progressively and as completely as possible into the European space programme, in particular as regards the development of applications satellites; → by elaborating and implementing the industrial policy appropriate to its programme and by recommending a coherent industrial policy to the Member States. -
UNDERSTANDING MATHEMATICS to UNDERSTAND PLATO -THEAETEUS (147D-148B Salomon Ofman
UNDERSTANDING MATHEMATICS TO UNDERSTAND PLATO -THEAETEUS (147d-148b Salomon Ofman To cite this version: Salomon Ofman. UNDERSTANDING MATHEMATICS TO UNDERSTAND PLATO -THEAETEUS (147d-148b. Lato Sensu, revue de la Société de philosophie des sciences, Société de philosophie des sciences, 2014, 1 (1). hal-01305361 HAL Id: hal-01305361 https://hal.archives-ouvertes.fr/hal-01305361 Submitted on 20 Apr 2016 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. UNDERSTANDING MATHEMATICS TO UNDERSTAND PLATO - THEAETEUS (147d-148b) COMPRENDRE LES MATHÉMATIQUES POUR COMPRENDRE PLATON - THÉÉTÈTE (147d-148b) Salomon OFMAN Institut mathématique de Jussieu-PRG Histoire des Sciences mathématiques 4 Place Jussieu 75005 Paris [email protected] Abstract. This paper is an updated translation of an article published in French in the Journal Lato Sensu (I, 2014, p. 70-80). We study here the so- called ‘Mathematical part’ of Plato’s Theaetetus. Its subject concerns the incommensurability of certain magnitudes, in modern terms the question of the rationality or irrationality of the square roots of integers. As the most ancient text on the subject, and on Greek mathematics and mathematicians as well, its historical importance is enormous. -
Mapping the Meaning of Knowledge in Design Research Kristina Niedderer University of Hertfordshire
V.2:2 April 2007 www.designresearchsociety.org Design Research Society ISSN 1752-8445 Mapping the Meaning of Knowledge in Design Research Kristina Niedderer University of Hertfordshire Knowledge plays a vital role in our life This question has arisen for design in Table of Contents: in that it reflects how we understand the UK, as well as more generally for the world around us and thus deter- creative and practice-led disciplines Articles: 1 Mapping the Meaning of Knowledge mines how we act upon it. In this sense, (CPDs), because research regulations in Design Research knowledge is of particular importance and requirements in the UK remain Kristina Niedderer for designers because they act to shape silent about what knowledge and our world. Conventionally, knowledge understanding mean in the context of 3 Call for Papers: Design Research creation has been assumed by (design) their specifications while implicitly pri- Quarterly research. However developments of oritising propositional knowledge over Case Studies in Research: Knowledge using practice within research have knowledge that cannot be expressed in and Inquiry pointed to knowledge creation within that form (Niedderer 2007). and through practice. This has raised This has led to a number of prob- Listings: the question of the meaning, role and lems concerning the role and format 14 Current Research in Design: format of knowledge in both research of knowledge in research and practice ToCs from Leading Design Journals and practice, and about the compatibil- in the UK. For example, because of the ity between knowledge of research and language-based mode of proposition- 21 Upcoming Events Worldwide practice. -
Marko Malink (NYU)
Demonstration by reductio ad impossibile in Posterior Analytics 1.26 Marko Malink (New York University) Contents 1. Aristotle’s thesis in Posterior Analytics 1. 26 ................................................................................. 1 2. Direct negative demonstration vs. demonstration by reductio ................................................. 14 3. Aristotle’s argument from priority in nature .............................................................................. 25 4. Priority in nature for a-propositions ............................................................................................ 38 5. Priority in nature for e-, i-, and o-propositions .......................................................................... 55 6. Accounting for Aristotle’s thesis in Posterior Analytics 1. 26 ................................................... 65 7. Parts and wholes ............................................................................................................................. 77 References ............................................................................................................................................ 89 1. Aristotle’s thesis in Posterior Analytics 1. 26 At the beginning of the Analytics, Aristotle states that the subject of the treatise is demonstration (ἀπόδειξις). A demonstration, for Aristotle, is a kind of deductive argument. It is a deduction through which, when we possess it, we have scientific knowledge (ἐπιστήμη). While the Prior Analytics deals with deduction in -
Phenomenal Concepts and the Problem of Acquaintance
Paul Livingston Phenomenal Concepts and the Problem of Acquaintance Abstract: Some contemporary discussion about the explanation of consciousness substantially recapitulates a decisive debate about ref- erence, knowledge, and justification from an earlier stage of the ana- lytic tradition. In particular, I argue that proponents of a recently popular strategy for accounting for an explanatory gap between phys- ical and phenomenal facts — the so-called ‘phenomenal concept strategy’ — face a problem that was originally fiercely debated by Schlick, Carnap, and Neurath. The question that is common to both the older and the contemporary discussion is that of how the presence or presentation of phenomenal experiences can play a role in justify- ing beliefs or judgments about them. This problem is, moreover, the same as what was classically discussed as the problem of acquain- tance. Interestingly, both physicalist and non-physicalist proponents of the phenomenal concept strategy today face this problem. I con- sider briefly some recent attempts to solve it and conclude that, although it is prima facie very plausible that acquaintance exists, we have, as yet, no good account of it. My aim in this paper is to demonstrate that proponents of a recently popular physicalist strategy for explaining consciousness — what has been called the phenomenal concept strategy — share with certain anti-physicalist phenomenal realists a common problem, which was also a problem for Schlick, Carnap, and Neurath in the days of the Vienna Circle. Though it has implications for ontology and metaphys- ics, this problem is essentially one about justification: how can judg- ments, claims, or beliefs about phenomenal experience be justified, at Correspondence: Email: [email protected] Journal of Consciousness Studies, 20, No. -
Techedsat Satellite Project Techedsat Formal Orbital Debris
TechEdSat Satellite Project TES-03-XS008 Orbital Debris Assessment Report (ODAR) Rev A TechEdSat Formal Orbital Debris Assessment Report (ODAR) In accordance with NPR 8715.6A, this report is presented as compliance with the required reporting format per NASA-STD-8719.14, APPENDIX A. Report Version: A (4/2/2012) DAS Software Used in This Analysis: DAS v2.0 Page 1 of 34 TechEdSat Satellite Project TES-03-XS008 Orbital Debris Assessment Report (ODAR) Rev A Page 2 of 34 TechEdSat Satellite Project TES-03-XS008 Orbital Debris Assessment Report (ODAR) Rev A Record of Revisions Affected Description of Rev Date Author (s) Pages Change Ali Guarneros Luna, A 4/2/2012 All Initial Release Christopher Hartney, Page 3 of 34 TechEdSat Satellite Project TES-03-XS008 Orbital Debris Assessment Report (ODAR) Rev A Table of Contents Self-assessment and OSMA assessment of the ODAR using the format in Appendix A.2 of NASA-STD-8719.14: Assessment Report Format Mission Description ODAR Section 1: Program Management and Mission Overview ODAR Section 2: Spacecraft Description ODAR Section 3: Assessment of Spacecraft Debris Released during Normal Operations ODAR Section 4: Assessment of Spacecraft Intentional Breakups and Potential for Explosions. ODAR Section 5: Assessment of Spacecraft Potential for On-Orbit Collisions ODAR Section 6: Assessment of Spacecraft Postmission Disposal Plans and Procedures ODAR Section 7: Assessment of Spacecraft Reentry Hazards ODAR Section 8: Assessment for Tether Missions Appendix A: Acronyms Appendix B: Battery Data Sheet Appendix C: Wiring Schematics Page 4 of 34 TechEdSat Satellite Project TES-03-XS008 Orbital Debris Assessment Report (ODAR) Rev A Selfassessment and OSMA assessment of the ODAR using the format in Appendix A.2 of NASASTD8719.14: A self assessment is provided below in accordance with the assessment format provided in Appendix A.2 of NASA-STD-8719.14. -
The Annual Compendium of Commercial Space Transportation: 2012
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2012 February 2013 About FAA About the FAA Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 51 United States Code, Subtitle V, Chapter 509 (formerly the Commercial Space Launch Act). FAA AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA AST is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA AST’s website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2013) NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. • i • Federal Aviation Administration’s Office of Commercial Space Transportation Dear Colleague, 2012 was a very active year for the entire commercial space industry. In addition to all of the dramatic space transportation events, including the first-ever commercial mission flown to and from the International Space Station, the year was also a very busy one from the government’s perspective. It is clear that the level and pace of activity is beginning to increase significantly. -
Cluster Keeping Algorithms for the Satellite Swarm Sensor Network Project
5th Federated and Fractionated Satellite Systems Workshop November 2-3, 2017, ISAE SUPAERO – Toulouse, France Cluster Keeping Algorithms for the Satellite Swarm Sensor Network Project Eviatar Edlerman and Pini Gurfil Technion – Israel Institute of Technology, Haifa 32000, Israel [email protected]; [email protected] Abstract This paper develops cluster control algorithms for the Satellite Swarm Sensor Network (S3Net) project, whose main aim is to enable fractionation of space-based remote sensing, imaging, and observation satellites. A methodological development of orbit control algorithms is provided, supporting the various use cases of the mission. Emphasis is given on outlining the algorithms structure, information flow, and software implementation. The methodology presented herein enables operation of multiple satellites in coordination, to enable fractionation of space sensors and augmentation of data provided therefrom. 1. INTRODUCTION In the field of earth observation from space, modern approaches show a trend of moving away from the classical single satellite missions, where one satellite includes a complete set of sensors and instruments, towards fractionated and distributed sensor missions, where multiple satellites, possibly carrying different types of sensors, act in a formation or swarm. Such missions promise an increase of imaging quality, an increase of service quality and, in many cases, a decrease of deployment costs for satellites that can become smaller and less complex due to mission requirements. Need for incremental deployment can be caused by funding limitations or issues. Although a combination of funds from different interest groups is possible, it can be difficult to achieve. A higher degree of independence for service providers can be enabled through lower cost satellites that allow integration into satellite swarms. -
Cubesat-Services.Pdf
Space• Space Station Station Cubesat CubesatDeployment Services Deployment Services NanoRacks Cubesat Deployer (NRCSD) • 51.6 degree inclination, 385-400 KM • Orbit lifetime 8-12 months • Deployment typically 1-3 months after berthing • Soft stowage internal ride several times per year Photo credit: NASA NRCSD • Each NRCSD can deploy up to 6U of CubeSats • 8 NRCSD’s per airlock cycle, for a total of 48U deployment capability • ~2 Air Lock cycles per mission Photo Credit: NanoRacks LLC Photo credit: NASA 2. Launched by ISS visiting vehicle 3. NRCSDs installed by ISS Crew 5. Grapple by JRMS 4. JEM Air Lock depress & slide 6. NRCSDs positioned by JRMS table extension 1. NRCSDs transported in CTBs 7. Deploy 8. JRMS return NRCSD-MPEP stack to slide table; 9. ISS Crew un-install first 8 NRCSDs; repeat Slide table retracts and pressurizes JEM air lock install/deploy for second set of NRCSDs NanoRacks Cubesat Mission (NR-CM 3 ) • Orbital Sciences CRS-1 (Launched Jan. 9, 2014) • Planet Labs Flock1A, 28 Doves • Lithuanian Space Assoc., LitSat-1 • Vilnius University & NPO IEP, LituanicaSat-1 • Nanosatisfi, ArduSat-2 • Southern Stars, SkyCube • University of Peru, UAPSat-1 Photo credit: NASA Mission Highlights Most CubeSats launched Two countries attain in a single mission space-faring status World’s largest remote Kickstarter funding sensing constellation • NR-CM3 • Orbital Science CRS-1, Launch Jan 9, 2014 • Air Lock Cycle 1, Feb 11-15, 2014 Dove CubeSats • Deployers 1-8 (all Planet Labs Doves) Photo credit: NASA • NR-CM3 • Orbital Science CRS-1,