The First Decadal Plan for Australian Space Science, Not the Final Version
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Mission to Jupiter
This book attempts to convey the creativity, Project A History of the Galileo Jupiter: To Mission The Galileo mission to Jupiter explored leadership, and vision that were necessary for the an exciting new frontier, had a major impact mission’s success. It is a book about dedicated people on planetary science, and provided invaluable and their scientific and engineering achievements. lessons for the design of spacecraft. This The Galileo mission faced many significant problems. mission amassed so many scientific firsts and Some of the most brilliant accomplishments and key discoveries that it can truly be called one of “work-arounds” of the Galileo staff occurred the most impressive feats of exploration of the precisely when these challenges arose. Throughout 20th century. In the words of John Casani, the the mission, engineers and scientists found ways to original project manager of the mission, “Galileo keep the spacecraft operational from a distance of was a way of demonstrating . just what U.S. nearly half a billion miles, enabling one of the most technology was capable of doing.” An engineer impressive voyages of scientific discovery. on the Galileo team expressed more personal * * * * * sentiments when she said, “I had never been a Michael Meltzer is an environmental part of something with such great scope . To scientist who has been writing about science know that the whole world was watching and and technology for nearly 30 years. His books hoping with us that this would work. We were and articles have investigated topics that include doing something for all mankind.” designing solar houses, preventing pollution in When Galileo lifted off from Kennedy electroplating shops, catching salmon with sonar and Space Center on 18 October 1989, it began an radar, and developing a sensor for examining Space interplanetary voyage that took it to Venus, to Michael Meltzer Michael Shuttle engines. -
Sixty Years of Australia in Space
Journal & Proceedings of the Royal Society of New South Wales, vol. 153, part 1, 2020, pp. 46–57. ISSN 0035-9173/20/010046-12 Sixty years of Australia in space Kerrie Dougherty Space Humanities Department, International Space University, Strasbourg, France Email: [email protected] Abstract Australia’s involvement in space activities commenced in 1957, at the beginning of the Space Age, with space tracking and sounding rocket launches at Woomera. By 1960, Australia was considered one of the leading space-active nations and in 1967 became one of the earliest countries to launch its own satellite. Yet by 1980, Australia’s space prominence had dwindled, with the country lacking both a national space agency and a coherent national space policy. Despite attempts in the latter part of the 1980s to develop an Australian space industry, the lack of a coherent and consistent national space policy and an effective co-ordinating body, left Australia constantly “punching below its weight” in global space activities until the Twenty First Century. This paper will briefly examine the often-contradictory history of Australian space activities from 1957 to the announcement of the Australian Space Agency in 2017, providing background and context for the later papers in this issue. Introduction Launchpad: the Woomera or 60,000 years the Indigenous people of Rocket Range FAustralia have looked to the sky, using “If the Woomera Range did not already exist, the stars to determine their location, find the proposal that Australia should engage in their way across the land and mark the a program of civil space research would be passage of the seasons and the best times unrealistic”. -
Aerospace, Defense, and Government Services Mergers & Acquisitions
Aerospace, Defense, and Government Services Mergers & Acquisitions (January 1993 - April 2020) Huntington BAE Spirit Booz Allen L3Harris Precision Rolls- Airbus Boeing CACI Perspecta General Dynamics GE Honeywell Leidos SAIC Leonardo Technologies Lockheed Martin Ingalls Northrop Grumman Castparts Safran Textron Thales Raytheon Technologies Systems Aerosystems Hamilton Industries Royce Airborne tactical DHPC Technologies L3Harris airport Kopter Group PFW Aerospace to Aviolinx Raytheon Unisys Federal Airport security Hydroid radio business to Hutchinson airborne tactical security businesses Vector Launch Otis & Carrier businesses BAE Systems Dynetics businesses to Leidos Controls & Data Premiair Aviation radios business Fiber Materials Maintenance to Shareholders Linndustries Services to Valsef United Raytheon MTM Robotics Next Century Leidos Health to Distributed Energy GERAC test lab and Technologies Inventory Locator Service to Shielding Specialities Jet Aviation Vienna PK AirFinance to ettain group Night Vision business Solutions business to TRC Base2 Solutions engineering to Sopemea 2 Alestis Aerospace to CAMP Systems International Hamble aerostructure to Elbit Systems Stormscope product eAircraft to Belcan 2 GDI Simulation to MBDA Deep3 Software Apollo and Athene Collins Psibernetix ElectroMechanical Aciturri Aeronautica business to Aernnova IMX Medical line to TransDigm J&L Fiber Services to 0 Knight Point Aerospace TruTrak Flight Systems ElectroMechanical Systems to Safran 0 Pristmatic Solutions Next Generation 911 to Management -
Jjmonl 1712.Pmd
alactic Observer John J. McCarthy Observatory G Volume 10, No. 12 December 2017 Holiday Theme Park See page 19 for more information The John J. McCarthy Observatory Galactic Observer New Milford High School Editorial Committee 388 Danbury Road Managing Editor New Milford, CT 06776 Bill Cloutier Phone/Voice: (860) 210-4117 Production & Design Phone/Fax: (860) 354-1595 www.mccarthyobservatory.org Allan Ostergren Website Development JJMO Staff Marc Polansky Technical Support It is through their efforts that the McCarthy Observatory Bob Lambert has established itself as a significant educational and recreational resource within the western Connecticut Dr. Parker Moreland community. Steve Barone Jim Johnstone Colin Campbell Carly KleinStern Dennis Cartolano Bob Lambert Route Mike Chiarella Roger Moore Jeff Chodak Parker Moreland, PhD Bill Cloutier Allan Ostergren Doug Delisle Marc Polansky Cecilia Detrich Joe Privitera Dirk Feather Monty Robson Randy Fender Don Ross Louise Gagnon Gene Schilling John Gebauer Katie Shusdock Elaine Green Paul Woodell Tina Hartzell Amy Ziffer In This Issue "OUT THE WINDOW ON YOUR LEFT"............................... 3 REFERENCES ON DISTANCES ................................................ 18 SINUS IRIDUM ................................................................ 4 INTERNATIONAL SPACE STATION/IRIDIUM SATELLITES ............. 18 EXTRAGALACTIC COSMIC RAYS ........................................ 5 SOLAR ACTIVITY ............................................................... 18 EQUATORIAL ICE ON MARS? ........................................... -
INTERNATIONAL Call for Papers & Registration of Interest
ORGANIZED BY: HOSTED BY: st 71 INTERNATIONAL ASTRONAUTICAL CONGRESS 12–16 October 2020 | Dubai, United Arab Emirates Call for Papers & Registration of Interest Second Announcement SUPPORTED BY: Inspire, Innovate & Discover for the Benefit of Humankind IAC2020.ORG Contents 1. Message from the International Astronautical Federation (IAF) 2 2. Message from the Local Organizing Committee 2 3. Message from the IPC Co-Chairs 3 4. Messages from the Partner Organizations 4 5. International Astronautical Federation (IAF) 5 6. International Academy of Astronautics (IAA) 10 7. International Institute of Space Law (IISL) 11 8. Message from the IAF Vice President for Technical Activities 12 9. IAC 2020 Technical Sessions Deadlines Calendar 49 10. Preliminary IAC 2020 at a Glance 50 11. Instructions to Authors 51 Connecting @ll Space People 12. Space in the United Arab Emirates 52 www.iafastro.org IAF Alliance Programme Partners 2019 1 71st IAC International Astronautical Congress 12–16 October 2020, Dubai 1. Message from the International Astronautical Federation (IAF) 3. Message from the International Programme Committee (IPC) Greetings! Co-Chairs It is our great pleasure to invite you to the 71st International Astronautical Congress (IAC) to take place in Dubai, United Arab Emirates On behalf of the International Programme Committee, it is a great pleasure to invite you to submit an abstract for the 71st International from 12 – 16 October 2020. Astronautical Congress IAC 2020 that will be held in Dubai, United Arab Emirates. The IAC is an initiative to bring scientists, practitioners, engineers and leaders of space industry and agencies together in a single platform to discuss recent research breakthroughs, technical For the very first time, the IAC will open its doors to the global space community in the United Arab Emirates, the first Arab country to advances, existing opportunities and emerging space technologies. -
MOP2019 Program Book.Pdf
1 Access Sakura Hall (Katahira campus) From Jun. 3 (Mon) to Jun. 6 (Thu) 10-min walk from Aoba-dori Inchibancho station (subway EW line) Route from the subway station https://www.tohoku.ac.jp/map/en/?f=KH_E01 Google Maps https://goo.gl/maps/VHjgQ9jumBLjexf77 Aoba Science Hall (Aobayama campus) Jun. 7 (Fri) 3-min walk from Aobayama station (subway EW line) Route from the subway station https://www.tohoku.ac.jp/map/en/?f=AY_H04 Google Maps https://goo.gl/maps/keQ1qyWia1cc7dYw6 2 Campus map (Katahira) University Cafeteria Katahira campus Meeting room Meeting room (2F, ESPACE ) (Katahira Hal) (3-6 June) North gate Main gate Meeting point for excursion on 6 June (12:00) Sakura Hall (https://www.tohoku.ac.jp/map/en/?f=KH) EV(to 1F) EV(to 2F) Registration Coffee Poster Oral Sakura Hall session session Entrance WC WC WC WC 2F 1F 3 Campus map (Aobayama) Aoba Science Aobayama campus Hall (7 June) Exit N1 Subway EW-line Aobayama Station (https://www.tohoku.ac.jp/map/en/?f=AY) 4 Excursion June 6 (Thu) – 12:15 Getting on a bus near the venue – 13:10 Arriving at Matsushima area – 13:10-14:50 Lunch time We have no reservation. There are many restaurants along the street nearby the coast. – 15:00-16:00 Getting on a boat ① – 16:00-17:45 Sightseeing Tickets of the Zuiganji-temple ② and Date Masamune Historical Meseum ③ will be provided. Red circles in the map are recommended. – 17:45 Getting on a bus – 18:45 Arriving at central Sendai near the banquet place ② ② ① ③ ① http://www.matsushima- kanko.com/uploads/Image/files/matsushimagaikokugomap2018.pdf 5 Banquet Date: Jun. -
Simple Regret Minimization for Contextual Bandits
Simple Regret Minimization for Contextual Bandits Aniket Anand Deshmukh* 1, Srinagesh Sharma* 1 James W. Cutler2 Mark Moldwin3 Clayton Scott1 1Department of EECS, University of Michigan, Ann Arbor, MI, USA 2Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI, USA 3Climate and Space Engineering, University of Michigan, Ann Arbor, MI, USA Abstract 1 Introduction The multi-armed bandit (MAB) is a framework for There are two variants of the classical multi- sequential decision making where, at every time step, armed bandit (MAB) problem that have re- the learner selects (or \pulls") one of several possible ceived considerable attention from machine actions (or \arms"), and receives a reward based on learning researchers in recent years: contex- the selected action. The regret of the learner is the tual bandits and simple regret minimization. difference between the maximum possible reward and Contextual bandits are a sub-class of MABs the reward resulting from the chosen action. In the where, at every time step, the learner has classical MAB setting, the goal is to minimize the sum access to side information that is predictive of all regrets, or cumulative regret, which naturally of the best arm. Simple regret minimization leads to an exploration/exploitation trade-off problem assumes that the learner only incurs regret (Auer et al., 2002a). If the learner explores too little, after a pure exploration phase. In this work, it may never find an optimal arm which will increase we study simple regret minimization for con- its cumulative regret. If the learner explores too much, textual bandits. Motivated by applications it may select sub-optimal arms too often which will where the learner has separate training and au- also increase its cumulative regret. -
Progress Towards Fedsat 2001 A'stralian Space Odyssey
SCC99-IX-6 Progress Towards FedSat 2001 A’stralian Space Odyssey Stephen Russell and Mirek Vesely Cooperative Research Centre for Satellite Systems, VIPAC Engineers and Scientists Ltd 21 King William St, Kent Town, South Australia, 5067 email: [email protected] ph. +618 8362 5445 fax. +618 8362 0793 Chris Graham Cooperative Research Centre for Satellite Systems CSIRO Telecommunications and Industrial Physics GPO Box 1483, Canberra ACT 2601, Australia email: [email protected] ph. +612 6216 7285 fax +612 6216 7272 and Mike Petkovic Cooperative Research Centre for Satellite Systems, Auspace Ltd, PO Box 17, Mitchell ACT 2911, Australia email: [email protected] ph. +612 6242 2611 fax +612 6241 6664 Abstract. In mid-1997, the Australian Government approved the setting up of a Cooperative Research Centre for Satellite Systems (CRCSS) to promote Australian space research. A key outcome of the research activities is intended to be the launching of a research satellite - FedSat- by the year 2001, the centenary year of Australian Federation. This will be the first Australian built satellite since 1970, and vital a step towards Australia's re- entry into the satellite business. This talk describes the aims of the FedSat mission; the design of the overall system; and provides up-to-date details of progress towards project completion. Neither the options of a turn-key contract, nor of Introduction building the whole system from scratch, have The FedSat satellite is, like its earlier sisters been taken. Instead, the CRCSS has opted to WRESAT and OSCAR V, a micro-satellite. take the middle road – buying a platform from However, with a mass of only 58 kilograms, she an experienced provider, with accompanying is packed with a selection of scientific payloads technology transfer, and building, assembling that are unusually complex for a nation stepping and testing the system themselves. -
CURRICULUM VITAE 21St July 2013 DAVID JOHN SOUTHWOOD
CURRICULUM VITAE 21st July 2013 DAVID JOHN SOUTHWOOD Personal Information Personal details: Date/Place of Birth 30 June 1945/Torquay (UK) Marital Status Married Nationality: British Email: [email protected] (work) Languages: English (native), French (qualified to A level, reading writing and conversation, very good), German (Inst. Ling. General), Spanish (O level, reading/writing very good, speaking good) Private interests Reading, Walking, Railways, Film and Theatre -------------------------------------- Professional Employment History Currently: Senior Research Investigator: Imperial College, London, SW72AZ, UK. Past Administrative Positions Director of Science and Robotic Exploration, (July 15th 2008-30th April 2011) European Space Agency, 8-10 Rue Mario-Nikis, 75738, Paris, Cedex 15, France. Director of Science, European Space Agency, Paris, France (May 2001-July 2008) Head, Earth Observation Science Strategy, in Directorate of Applications, European Space Agency, Paris, France (March 1999 - March 2000) Head, Earth Observation Strategy, in Directorate of Science, European Space Agency, Paris, France (October 1997 - February 1999) Head of Physics Department (Blackett Laboratory), Imperial College, London. (September 1994 - September 1997). Head of Space and Atmospheric Physics Group (Space Physics 1984-1986), Physics Department, Imperial College London (September 1984 - July 1990, September 1995 – September 1997), -------------------------------------- Academic Positions Professor of Physics, Physics Department, Imperial College -
Precision Magnetometers for Aerospace Applications: a Review
sensors Review Precision Magnetometers for Aerospace Applications: A Review James S. Bennett 1,† , Brian E. Vyhnalek 2,†, Hamish Greenall 1 , Elizabeth M. Bridge 1 , Fernando Gotardo 1 , Stefan Forstner 1 , Glen I. Harris 1 , Félix A. Miranda 2,* and Warwick P. Bowen 1,* 1 School of Mathematics and Physics, The University of Queensland, St. Lucia, QLD 4072, Australia; [email protected] (J.S.B.); [email protected] (H.G.); [email protected] (E.M.B.); [email protected] (F.G.); [email protected] (S.F.); [email protected] (G.I.H.) 2 NASA Glenn Research Center, Cleveland, OH 44135, USA; [email protected] * Correspondence: [email protected] (F.A.M.); [email protected] (W.P.B.) † These authors contributed equally to this work. Abstract: Aerospace technologies are crucial for modern civilization; space-based infrastructure underpins weather forecasting, communications, terrestrial navigation and logistics, planetary observations, solar monitoring, and other indispensable capabilities. Extraplanetary exploration— including orbital surveys and (more recently) roving, flying, or submersible unmanned vehicles—is also a key scientific and technological frontier, believed by many to be paramount to the long-term survival and prosperity of humanity. All of these aerospace applications require reliable control of the craft and the ability to record high-precision measurements of physical quantities. Magnetometers deliver on both of these aspects and have been vital to the success of numerous missions. In this review Citation: Bennett, J.S.; Vyhnalek, paper, we provide an introduction to the relevant instruments and their applications. -
Practice No. PD-ED-1207
PRACTICENO. PD-ED-1207 PAGE1OF 1 OF5 PREFERRED RELIABILITY MAGNETIC DESIGN CONTROL PRACTICES FOR SCIENCE INSTRUMENTS Practice: Design flight subsystems with low residual dipole magnetic fields to maintain the spacecraft’s total static and dynamic magnetic fields within science requirements. Benefit: Provides for a magnetically clean spacecraft, which increases the quality and accuracy of interplanetary and planetary magnetic field data gathered during the mission. Programs That Certified Usage: Mariner series, Voyager (VGR), Galileo (GLL), Ulysses. Center to Contact for Information: Jet Propulsion Laboratory (JPL). Implementation Method: Because the dipolar portion of a spacecraft’s magnetic field at its magnetometer experiment sensor location dominates the nondipolar part, each spacecraft subsystem is assigned a maximum allowable dipole magnetic field specification based on the magnetometer sensor sensitivity and the distance between the bulk of the subsystems and the sensor location. A typical maximum dipolar field allocation is 10 nanoTeslas (gammas) at a distance of 1 meter from the geometric center of a spacecraft’s subsystem, assuming the magnetometer sensor is mounted at the end of an 8-meter boom. To ensure that each subsystem will meet its respective dipole field specification, several design practices are observed during the early stages of the subsystem design. These practices include: 1. Magnetic Shielding of Magnetic Components A magnetic source can be enclosed in a high permeability material shield, which in effect confines the source’s JET magnetic flux to within the walls of the shield enclosure. PROPULSION The shield should be completely enveloping, with the LABORATORY PRACTICENO. PD-ED-1207 PAGE2OF 2 OF5 MAGNETIC DESIGN CONTROL FOR SCIENCE INSTRUMENTS minimum number of holes and cutouts. -
Single Antenna Attitude Determination for Fedsat
COVER SHEET This is the author version of article published as: Wang, Charles and Walker, Rodney A. and Enderle, Werner (2002) Single Antenna Attitude Determination for FedSat. In Proceedings Institute of Navigation GPS-02. Copyright 2002 (please consult author) Accessed from http://eprints.qut.edu.au Single Antenna Attitude Determination for FedSat Mr Charles Wang, Cooperative Research Centre for Satellite Systems, Brisbane, Australia Dr Rodney A. Walker, Cooperative Research Centre for Satellite Systems, Brisbane, Australia Associate Professor Werner Enderle, Cooperative Research Centre for Satellite Systems, Brisbane, Australia Australian Cooperative Research Centre for Satellite Biography Systems. He was a co-investigator of the EQUATOR-S GPS experiment that first proved the possibility of main Mr Charles Wang completed his undergraduate study at and side-lobe tracking of GPS satellites from Queensland University of Technology with Bachelor of geosynchronous altitudes and above. Aerospace Avionic Engineering in Oct 2000. During year 2001, Charles Wang has undertaken further study Abstract in Master of Engineering Science (Communication and Computing) at QUT and graduated with first class FedSat is the first satellite to be launched by Australia honours. From Aug 2002, Charles Wang started the for 30 years. It is will be a scientific spacecraft with a Masters of Engineering by research at the Cooperative number of experimental payloads. These payloads Research Centre for Satellite Systems (CRCSS) in the comprise of a single antenna GPS receiver, a 3-axis Faculty of Built Environment and Engineering at QUT. magnetometer, a Ka Band transponder and a re- He is working in the area of “Global Positioning System configurable computing payload.