Cooperation of Humans and Robots for Mars
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Lara (Lander Radioscience) on the Exomars 2020 Surface Platform
EPSC Abstracts Vol. 13, EPSC-DPS2019-891-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. LaRa (Lander Radioscience) on the ExoMars 2020 Surface Platform. Véronique Dehant1,2, Sébastien Le Maistre1, Rose-Marie Baland1, Özgür Karatekin1, Marie-Julie Péters1, Attilio Rivoldini1, Tim Van Hoolst1, Bart Van Hove1, Marie Yseboodt1, and Alexander Kosov3 (1) Royal Observatory of Belgium (ROB), Brussels, Belgium, (2) Université catholique de Louvain, Louvain-la-Neuve, Belgium, (3) Space Research Institute Russian Academy of Sciences (IKI), Moscow, Russia Abstract The surface platform Kazachok will house the radio science experiment LaRa (Lander Radioscience) to support specific scientific objectives of the ExoMars 2020 mission. The LaRa experiment is described and the scientific objectives and strategies are detailed in this presentation. Figure 1. LaRa principle. 1. Introduction 2. The LaRa instrument In the last decade, several missions and observations As LaRa performs a coherent retransmission of the have brought new data on the planet Mars, obtained uplink carrier to the downlink carrier, the downlink by either spacecraft orbiting around Mars or landers frequency is scaled by a constant multiplier, the and rovers on the surface. Among other things, the transponder ratio (880/749). By emitting the uplink information acquired will improve our understanding signal from Earth, the masers in the ground stations of Mars’ interior, evolution and habitability. Data ensure frequency stability of LaRa’s radiosignal. obtained by new space missions are driving further The LaRa instrument is built in collaboration with progress in this field. In 2020, the European Space other Belgian actors under the lead of ESA PRODEX, Agency ESA and the Russian space agency and ROB providing the instrument specifications. -
Mars Reconnaissance Orbiter Navigation Strategy for the Exomars Schiaparelli EDM Lander Mission
Jet Propulsion Laboratory California Institute of Technology Mars Reconnaissance Orbiter Navigation Strategy for the ExoMars Schiaparelli EDM Lander Mission Premkumar R. Menon Sean V. Wagner, David C. Jefferson, Eric J. Graat, Kyong J. Lee, and William B. Schulze AAS/AIAA Astrodynamics Specialist Conference San Antonio, Texas February 5–9, 2017 AAS Paper 17-337 © 2017 California Institute of Technology. Government Sponsorship Acknowledged. Mars Reconnaissance Orbiter Project Mars Reconnaissance Orbiter (Mission, Spacecraft and PSO) The Mars Reconnaissance Orbiter mission launched in August 2005 from the Cape Canaveral Air Force Station arriving at Mars in March 2006 started science operations in November 2006. MRO has completed 10 years since launch (50,000 orbits by Mar 2017) and to date has returned nearly 300 Terabytes of data. MRO Primary Science Orbit (PSO): • Sun-synchronous orbit ascending node at 3:00 PM ± 15 minutes Local Mean Solar Time (LMST) (daylight equatorial crossing) • Periapsis is frozen about the Mars South Pole • Near-repeat ground track walk (GTW) every 17-day, 211 orbit (short-term repeat) MRO targeting cycle, exact repeat after 4602 orbits. The nominal GTW is 32.45811 km West each 211 orbit cycle (maintained with periodic maneuvers). MRO Spacecraft: • Spacecraft Bus: 3-axis stabilized ACS system; 3-meter diameter High Gain Antenna; hydrazine propulsion system • Instrument Suite: HiRISE Camera, CRISM Imaging spectrometer, Mars Climate Sounder, Mars Color Imager, Context Camera, Shallow Subsurface Radar, Electra engineering payload (among other instrument payloads) 2/07/17 MRO support of ExoMars Schiaparelli Lander Overflight Relay PRM-3 4. MRO shall have good overflight pass geometry within the first 2 Sols after landing. -
TINA Small Force-Controlled Robotic Arm for Exploration and Small Satellites
DLR.de/en TINA Small force-controlled robotic arm for exploration and small satellites Brief description The robotic arm TINA is a four-axis space demonstrator to investigate autonomous operations during exploration missions on Earth. Aims The aim of the research project is to demonstrate the technology needed for a small, force-controlled robotic arm for use in space. By selecting specific components, it is possible to use TINA in Parties involved microgravity conditions as well as on Earth. DLR Institute of Robotics and Mechatronics Applications Facts and figures - Exploration, rover - Degrees of freedom: up to 7 - Controller: hard real time - Small satellites - Size: up to 2 m long - Radiation hardness: - Weight: 1.6 kg per joint various levels possible - Data transmission: - Tools: different end effectors can be Spacewire selected - Data rate: 3kHz - Supply voltage: +20V to +70V @DLR_en DLR.de/en TINA Small force-controlled robotic arm for exploration and small satellites The design of TINA follows the ‘qualifiable’ philosophy of DEXHAND [1], which uses industrial-grade compo- nents with a similar performance to their space equivalents and follows the ECSS guidelines closely, or uses the industrial-grade versions of radiation-hardened electronic components. This philosophy ensures that the transition to a fully qualified design can be achieved with a minimum number of changes. It also provides an almost perfect version for thermal and EMI modelling. Another big advantage is the low price compared to the fully qualified, radiation-hardened version, which allows the construction of multiple test arms for grasp- ing, object handling and many other applications. Each joint is made up of a brushless DC motor in combination with a resolver for commutation and position sensing, a harmonic drive gearbox, a brake for safety reasons and a torque sensor to give TINA the ability to ‘feel’. -
Back to the the Future? 07> Probing the Kuiper Belt
SpaceFlight A British Interplanetary Society publication Volume 62 No.7 July 2020 £5.25 SPACE PLANES: back to the the future? 07> Probing the Kuiper Belt 634089 The man behind the ISS 770038 Remembering Dr Fred Singer 9 CONTENTS Features 16 Multiple stations pledge We look at a critical assessment of the way science is conducted at the International Space Station and finds it wanting. 18 The man behind the ISS 16 The Editor reflects on the life of recently Letter from the Editor deceased Jim Beggs, the NASA Administrator for whom the building of the ISS was his We are particularly pleased this supreme achievement. month to have two features which cover the spectrum of 22 Why don’t we just wing it? astronautical activities. Nick Spall Nick Spall FBIS examines the balance between gives us his critical assessment of winged lifting vehicles and semi-ballistic both winged and blunt-body re-entry vehicles for human space capsules, arguing that the former have been flight and Alan Stern reports on his grossly overlooked. research at the very edge of the 26 Parallels with Apollo 18 connected solar system – the Kuiper Belt. David Baker looks beyond the initial return to the We think of the internet and Moon by astronauts and examines the plan for a how it helps us communicate and sustained presence on the lunar surface. stay in touch, especially in these times of difficulty. But the fact that 28 Probing further in the Kuiper Belt in less than a lifetime we have Alan Stern provides another update on the gone from a tiny bleeping ball in pioneering work of New Horizons. -
EMC18 Abstracts
EUROPEAN MARS CONVENTION 2018 – 26-28 OCT. 2018, LA CHAUX-DE-FONDS, SWITZERLAND EMC18 Abstracts In alphabetical order Name title of presentation Page n° Théodore Besson: Scorpius Prototype 3 Tomaso Bontognali Morphological biosignatures on Mars: what to expect and how to prepare not to miss them 4 Pierre Brisson: Humans on Mars will have to live according to both Martian & Earth Time 5 Michel Cabane: Curiosity on Mars : What is new about organic molecules? 6 Antonio Del Mastro Industrie 4.0 technology for the building of a future Mars City: possibilities and limits of the application of a terrestrial technology for the human exploration of space 7 Angelo Genovese Advanced Electric Propulsion for Fast Manned Missions to Mars and Beyond 8 Olivia Haider: The AMADEE-18 Mars Simulation OMAN 9 Pierre-André Haldi: The Interplanetary Transport System of SpaceX revisited 10 Richard Heidman: Beyond human, technical and financial feasibility, “mass-production” constraints of a Colony project surge. 11 Jürgen Herholz: European Manned Space Projects 12 Jean-Luc Josset Search for life on Mars, the ExoMars rover mission and the CLUPI instrument 13 Philippe Lognonné and the InSight/SEIS Team: SEIS/INSIGHT: Towards the Seismic Discovering of Mars 14 Roland Loos: From the Earth’s stratosphere to flying on Mars 15 EUROPEAN MARS CONVENTION 2018 – 26-28 OCT. 2018, LA CHAUX-DE-FONDS, SWITZERLAND Gaetano Mileti Current research in Time & Frequency and next generation atomic clocks 16 Claude Nicollier Tethers and possible applications for artificial gravity -
Exomars Schiaparelli Direct-To-Earth Observation Using GMRT
TECHNICAL ExoMars Schiaparelli Direct-to-Earth Observation REPORTS: METHODS 10.1029/2018RS006707 using GMRT S. Esterhuizen1, S. W. Asmar1 ,K.De2, Y. Gupta3, S. N. Katore3, and B. Ajithkumar3 Key Point: • During ExoMars Landing, GMRT 1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA, 2Cahill Center for Astrophysics, observed UHF transmissions and California Institute of Technology, Pasadena, CA, USA, 3National Centre for Radio Astrophysics, Pune, India Doppler shift used to identify key events as only real-time aliveness indicator Abstract During the ExoMars Schiaparelli separation event on 16 October 2016 and Entry, Descent, and Landing (EDL) events 3 days later, the Giant Metrewave Radio Telescope (GMRT) near Pune, India, Correspondence to: S. W. Asmar, was used to directly observe UHF transmissions from the Schiaparelli lander as they arrive at Earth. The [email protected] Doppler shift of the carrier frequency was measured and used as a diagnostic to identify key events during EDL. This signal detection at GMRT was the only real-time aliveness indicator to European Space Agency Citation: mission operations during the critical EDL stage of the mission. Esterhuizen, S., Asmar, S. W., De, K., Gupta, Y., Katore, S. N., & Plain Language Summary When planetary missions, such as landers on the surface of Mars, Ajithkumar, B. (2019). ExoMars undergo critical and risky events, communications to ground controllers is very important as close to real Schiaparelli Direct-to-Earth observation using GMRT. time as possible. The Schiaparelli spacecraft attempted landing in 2016 was supported in an innovative way. Radio Science, 54, 314–325. A large radio telescope on Earth was able to eavesdrop on information being sent from the lander to other https://doi.org/10.1029/2018RS006707 spacecraft in orbit around Mars. -
REASONS to MIND ASTEROIDS with the Rapid Progress Made In
ASTEROID MINING & ITS LEGAL IMPLICATIONS Neil Modi & Devanshu Ganatra Presentation ID- IAC- 16.E7.IP.23.x32357 REASONS TO MINE ASTEROIDS With the rapid progress made in technology, humans are taking huge steps in space today. There is huge potential in space, and particularly in asteroid mining. ENERGY CRISIS RARE EARTH METALS • Non-renewable fossil fuels like coal, oil currently account for 81% of • Many of the metals widely used in almost all industrial products the world’s primary energy. were always limited and are now in SHORT SUPPLY leading to skyrocketing manufacturing costs. • EARLIER, renewable energy could not compete with non-renewable sources because it relied on metals in short supply. Resources found • These include Platinum Group Metals (PMGS) and others like on asteroids would solve this problem completely. gold, cobalt, iron, molybdenum etc. Image Credit-The U.S. Energy Image Credit- FuelSpace.org- ‘How Asteroids Can Information Administration Save Mankind’ PROJECTED SCARCITY OF RESOURCES ON EARTH Image Credit-Shackleton Energy Company Image Credit- Chris Clugston’s ‘An Oil Drum- An Analysis’ (2010) THE NEED FOR WATER 1. SUPPORT SYSTEM FOR ASTRONAUTS- Since the main constituents of water HYDRATION AND OXYGEN are hydrogen and oxygen, it is a source of oxygen for life support. TO ASTRONAUTS 2. PROTECTION FROM RADIATION- Water absorbs and blocks infrared radiation, which means that by storing heat it helps to maintain temperature. 3. ROCKET FUEL- Rocket propellant is hydrogen and oxygen based, with a large percentage of the weight of a spacecraft taken up by fuel. 4. SPACE EXPLORATION- A GAS STATION IN SPACE KEY TO SPACE BLOCKS EXPLORATION WATER RADIATION Today billions of dollars are spent in rocket fuel to sustain space explorations. -
SPACE RESEARCH in POLAND Report to COMMITTEE
SPACE RESEARCH IN POLAND Report to COMMITTEE ON SPACE RESEARCH (COSPAR) 2020 Space Research Centre Polish Academy of Sciences and The Committee on Space and Satellite Research PAS Report to COMMITTEE ON SPACE RESEARCH (COSPAR) ISBN 978-83-89439-04-8 First edition © Copyright by Space Research Centre Polish Academy of Sciences and The Committee on Space and Satellite Research PAS Warsaw, 2020 Editor: Iwona Stanisławska, Aneta Popowska Report to COSPAR 2020 1 SATELLITE GEODESY Space Research in Poland 3 1. SATELLITE GEODESY Compiled by Mariusz Figurski, Grzegorz Nykiel, Paweł Wielgosz, and Anna Krypiak-Gregorczyk Introduction This part of the Polish National Report concerns research on Satellite Geodesy performed in Poland from 2018 to 2020. The activity of the Polish institutions in the field of satellite geodesy and navigation are focused on the several main fields: • global and regional GPS and SLR measurements in the frame of International GNSS Service (IGS), International Laser Ranging Service (ILRS), International Earth Rotation and Reference Systems Service (IERS), European Reference Frame Permanent Network (EPN), • Polish geodetic permanent network – ASG-EUPOS, • modeling of ionosphere and troposphere, • practical utilization of satellite methods in local geodetic applications, • geodynamic study, • metrological control of Global Navigation Satellite System (GNSS) equipment, • use of gravimetric satellite missions, • application of GNSS in overland, maritime and air navigation, • multi-GNSS application in geodetic studies. Report -
From Prometheus to Pistorius: a Genaelogy of Physical Ability
FROM PROMETHEUS TO PISTORIUS: A GENAELOGY OF PHYSICAL ABILITY by Stephanie J. Cork A thesis submitted to the Department of Sociology In conformity with the requirements for the degree of Masters of Arts Queen’s University Kingston, Ontario, Canada (September, 2011) Copyright ©Stephanie J. Cork, 2011 Abstract (Fragile Frames + Monstrosities)ModernWar + (Flagged Bodies + Cyborgs)PostmodernWar = dis-AbilityCyborged ii Acknowledgements A huge thank you goes out to: my friends, colleagues, office neighbours, mentors, family, defence committee, readers, editors and Steve. Thank you, also, to the Canadian and American troops as well as Paralympic athletes, Oscar Pistorius and Aimee Mullins for their inspiration, sorry, I have borrowed your stories to perpetuate my own academic success. Thanks also to Louise Bark for her endless patience and kindness, as well as a pint (or three!) at Ben’s Pub. Anne and Wendy and especially Michelle: you are lifesavers! Finally, my eternal gratitude to the: “greatest man alive,” Dr. Rob Beamish (Scott Mason 2011). iii Table of Contents Abstract............................................................................................................................................. i Acknowledgements......................................................................................................................... iii Table of Contents............................................................................................................................ iv Chapter 1: Introduction.....................................................................................................................1 -
Outline of Aurora Funding
Outline of Aurora funding The £3 million from the Aurora Science Programme has gone to the following 17 academics and individual scientists working at UK research organisations: 1. An improved understanding of Mars photochemistry using NOMAD and ACS measurements – Professor Paul Palmer, Edinburgh University - £73,442 The proposal aims to develop the existing photochemistry (the chemistry effects of light) to prepare for measurements collected by the NOMAD and ACS instruments aboard the Trace Gas Orbiter. They will develop the chemical mechanism so it can be used to interpret observed variations of atmospheric gases on Mars. 2. Dust storms and the dust transport cycle: their impact on the Martian climate in a multi annual reanalysis of MCS, THEMIS and TGO/ACS data – Professor Peter Read, Oxford University - £346,592 The proposal aims to improve our understanding of the Martian dust cycle, its impact on climate and the physical features of the Martian surface. Using a new approach towards analysing daily variations in the Martian atmosphere it is proposed to extend this dataset using measurements of the Martian atmosphere from the Mars Reconnaissance Orbiter and Mars Odyssey missions in orbit around Mars, and from the Atmospheric Chemistry Suite (ACS) on ESA's Trace Gas Orbiter mission when they become available. This may be useful for future spacecraft operations at the Martian surface, as well as to improve our understanding of both the present and past states of the Martian climate. 3. ExoMars TGO Guest Investigator Support – Dr Matt Balme, Open University - £56,367 This proposal seeks funding for a Guest Investigator position on ESA's ExoMars Trace Gas Orbiter mission. -
Prism Vol. 9, No. 2 Prism About Vol
2 021 PRISMVOL. 9, NO. 2 | 2021 PRISM VOL. 9, NO. 2 NO. 9, VOL. THE JOURNAL OF COMPLEX OPER ATIONS PRISM ABOUT VOL. 9, NO. 2, 2021 PRISM, the quarterly journal of complex operations published at National Defense University (NDU), aims to illuminate and provoke debate on whole-of-government EDITOR IN CHIEF efforts to conduct reconstruction, stabilization, counterinsurgency, and irregular Mr. Michael Miklaucic warfare operations. Since the inaugural issue of PRISM in 2010, our readership has expanded to include more than 10,000 officials, servicemen and women, and practi- tioners from across the diplomatic, defense, and development communities in more COPYEDITOR than 80 countries. Ms. Andrea L. Connell PRISM is published with support from NDU’s Institute for National Strategic Studies (INSS). In 1984, Secretary of Defense Casper Weinberger established INSS EDITORIAL ASSISTANTS within NDU as a focal point for analysis of critical national security policy and Ms. Taylor Buck defense strategy issues. Today INSS conducts research in support of academic and Ms. Amanda Dawkins leadership programs at NDU; provides strategic support to the Secretary of Defense, Chairman of the Joint Chiefs of Staff, combatant commands, and armed services; Ms. Alexandra Fabre de la Grange and engages with the broader national and international security communities. Ms. Julia Humphrey COMMUNICATIONS INTERNET PUBLICATIONS PRISM welcomes unsolicited manuscripts from policymakers, practitioners, and EDITOR scholars, particularly those that present emerging thought, best practices, or train- Ms. Joanna E. Seich ing and education innovations. Publication threshold for articles and critiques varies but is largely determined by topical relevance, continuing education for national and DESIGN international security professionals, scholarly standards of argumentation, quality of Mr. -
Grail): Extended Mission and Endgame Status
44th Lunar and Planetary Science Conference (2013) 1777.pdf GRAVITY RECOVERY AND INTERIOR LABORATORY (GRAIL): EXTENDED MISSION AND ENDGAME STATUS. Maria T. Zuber1, David E. Smith1, Sami W. Asmar2, Alexander S. Konopliv2, Frank G. Lemoine3, H. Jay Melosh4, Gregory A. Neumann3, Roger J. Phillips5, Sean C. Solomon6,7, Michael M. Watkins2, Mark A. Wieczorek8, James G. Williams2, Jeffrey C. Andrews-Hanna9, James W. Head10, Wal- ter S. Kiefer11, Isamu Matsuyama12, Patrick J. McGovern11, Francis Nimmo13, G. Jeffrey Taylor14, Renee C. Weber15, Sander J. Goossens16, Gerhard L. Kruizinga2, Erwan Mazarico3, Ryan S. Park2 and Dah-Ning Yuan2. 1Dept. of Earth, Atmospheric and Planetary Sciences, Massachusetts Institute of Technology, Cambridge, MA 02129, USA ([email protected]); 2Jet Propulsion Laboratory, California Institute of Technol- ogy, Pasadena, CA 91109, USA; 3NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA; 4Dept. of Earth and Atmospheric Sciences, Purdue University, West Lafayette, IN 47907, USA; 5Planetary Science Directorate, Southwest Research Institute, Boulder, CO 80302, USA; 6 Lamont-Doherty Earth Observatory, Columbia University, Palisades, NY 10964, USA; 7Dept. of Terrestrial Magnetism, Carnegie Institution of Washington, Washington, DC 20015, USA; 8Institut de Physique du Globe de Paris, 94100 Saint Maur des Fossés, France; 9Dept. of Geophysics and Center for Space Resources, Colorado School of Mines, Golden, CO 80401, USA; 10Dept. of Geological Sciences, Brown University, Providence, RI 02912, USA; 11Lunar and Planetary Institute, Houston, TX 77058, USA; 12Lunar and Planetary Laborato- ry, University of Arizona, Tucson, AZ 85721, USA; 13Dept. of Earth and Planetary Sciences, University of California, Santa Cruz, CA 95064, USA; 14Hawaii Institute of Geophysics and Planetology, University of Hawaii, Honolulu, HI 96822, USA; 15NASA Marshall Space Flight Center, Huntsville, AL 35805, USA, 16University of Maryland, Baltimore County, Baltimore, MD 21250, USA.