Enabling and Enhancing Astrophysical Observations with Autonomous Systems
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Refactoring the Curiosity Rover's Sample Handling Architecture on Mars
Refactoring the Curiosity Rover's Sample Handling Architecture on Mars Vandi Verma Stephen Kuhn (abstracting the shared development effort of many) The research was carried out at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration. Copyright 2018 California Institute of Technology. U.S. Government sponsorship acknowledged. Introduction • The Mars Science Laboratory (“MSL”) hardware was architected to enable a fixed progression of activities that essentially enforced a campaign structure. In this structure, sample processing and analysis conflicted with any other usage of the robotic arm. • Unable to stow the arm and drive away • Unable to deploy arm instruments for in-situ engineering or science • Unable to deploy arm instruments or mechanisms on new targets • Sampling engineers developed and evolved a refactoring of this architecture in order to have it both ways Turn the hardware into a series of caches and catchments that could service all arm orientations. Enable execution of other arm activities with one “active” sample Page 2 11/18/20preserved such that additional portions could be delivered. The Foundational Risk Page 3 11/18/20 The Original Approach Page 4 11/18/20 Underpinnings of the original approach • Fundamentally, human rover planners simply could not keep track of sample in CHIMRA as it sluiced, stick- slipped, fell over partitions, pooled in catchments, etc. Neither could we update the Flight Software to model this directly. • But, with some simplifying abstraction of sample state and preparation of it into confined regimes of orientation, ground tools could effectively track sample. Rover planners’ use of Software Simulator was extended to enforce a chain of custody in commanded orientation, creating a faulted breakpoint upon violation that could be used to fix it. -
(PLEXIL) for Executable Plans and Command Sequences”, International Symposium on Artificial Intelligence, Robotics and Automation in Space (Isairas), 2005
V. Verma, T. Estlin, A. Jónsson, C. Pasareanu, R. Simmons, K. Tso, “Plan Execution Interchange Language (PLEXIL) for Executable Plans and Command Sequences”, International Symposium on Artificial Intelligence, Robotics and Automation in Space (iSAIRAS), 2005 PLAN EXECUTION INTERCHANGE LANGUAGE (PLEXIL) FOR EXECUTABLE PLANS AND COMMAND SEQUENCES Vandi Verma(1), Tara Estlin(2), Ari Jónsson(3), Corina Pasareanu(4), Reid Simmons(5), Kam Tso(6) (1)QSS Inc. at NASA Ames Research Center, MS 269-1 Moffett Field CA 94035, USA, Email:[email protected] (2)Jet Propulsion Laboratory, M/S 126-347, 4800 Oak Grove Drive, Pasadena CA 9110, USA , Email:[email protected] (3) USRA-RIACS at NASA Ames Research Center, MS 269-1 Moffett Field CA 94035, USA, Email:[email protected] (4)QSS Inc. at NASA Ames Research Center, MS 269-1 Moffett Field CA 94035, USA, Email:[email protected] (5)Robotics Institute, Carnegie Mellon University, Pittsburgh PA 15213, USA, Email:[email protected] (6)IA Tech Inc., 10501Kinnard Avenue, Los Angeles, CA 9002, USA, Email: [email protected] ABSTRACT this task since it is impossible for a small team to manually keep track of all sub-systems in real time. Space mission operations require flexible, efficient and Complex manipulators and instruments used in human reliable plan execution. In typical operations command missions must also execute sequences of commands to sequences (which are a simple subset of general perform complex tasks. Similarly, a rover operating on executable plans) are generated on the ground, either Mars must autonomously execute commands sent from manually or with assistance from automated planning, Earth and keep the rover safe in abnormal situations. -
Arxiv:1907.00616V1 [Astro-Ph.IM] 1 Jul 2019 282 75, Vol
Mem. S.A.It. Vol. 75, 282 c SAIt 2008 Memorie della The Transient High-Energy Sky and Early Universe Surveyor (THESEUS) L. Amati1, E. Bozzo2, P. O’Brien3, and D. G¨otz4 (on behalf of the THESEUS consortium) 1 INAF-OAS Bologna, via P. Gobetti 101, I-40129 Bologna, Italy e-mail: [email protected] 2 Department of Astronomy, University of Geneva, chemin d’Ecogia 16, 1290 Versoix, Switzerland 3 Department of Physics and Astronomy, University of Leicester, Leicester LE1 7RH, United Kingdom 4 CEA, Universit Paris-Saclay, F-91191 Gif-sur-Yvette, France Abstract. The Transient High-Energy Sky and Early Universe Surveyor (THESEUS) is a mission concept developed in the last years by a large European consortium and currently under study by the European Space Agency (ESA) as one of the three candidates for next M5 mission (launch in 2032). THESEUS aims at exploiting high-redshift GRBs for getting unique clues to the early Universe and, being an unprecedentedly powerful machine for the detection, accurate location (down to ∼arcsec) and redshift determination of all types of GRBs (long, short, high-z, under-luminous, ultra-long) and many other classes of transient sources and phenomena, at providing a substantial contribution to multi-messenger time- domain astrophysics. Under these respects, THESEUS will show a strong synergy with the large observing facilities of the future, like E-ELT, TMT, SKA, CTA, ATHENA, in the electromagnetic domain, as well as with next-generation gravitational-waves and neutrino detectors, thus greatly enhancing their scientific return. Key words. THESEUS – Space mission Concept – ESA – M5 – Gamma-ray Bursts – Cosmology – Gravitational Waves – Multi-messenger Astrophysics. -
Tiny ASTERIA Satellite Achieves a First for Cubesats 16 August 2018, by Lauren Hinkel and Mary Knapp
Tiny ASTERIA satellite achieves a first for CubeSats 16 August 2018, by Lauren Hinkel And Mary Knapp The ASTERIA project is a collaboration between MIT and NASA's Jet Propulsion Laboratory (JPL) in Pasadena, California, funded through JPL's Phaeton Program. The project started in 2010 as an undergraduate class project in 16.83/12.43 (Space Systems Engineering), involving a technology demonstration of astrophysical measurements using a Cubesat, with a primary goal of training early-career engineers. The ASTERIA mission—of which Department of Earth, Atmospheric and Planetary Sciences Class of 1941 Professor of Planetary Sciences Sara Seager is the Principal Investigator—was designed to demonstrate key technologies, including very Members of the ASTERIA team prepare the petite stable pointing and thermal control for making satellite for its journey to space. Credit: NASA/JPL- extremely precise measurements of stellar Caltech brightness in a tiny satellite. Earlier this year, ASTERIA achieved pointing stability of 0.5 arcseconds and thermal stability of 0.01 degrees Celsius. These technologies are important for A miniature satellite called ASTERIA (Arcsecond precision photometry, i.e., the measurement of Space Telescope Enabling Research in stellar brightness over time. Astrophysics) has measured the transit of a previously-discovered super-Earth exoplanet, 55 Cancri e. This finding shows that miniature satellites, like ASTERIA, are capable of making of sensitive detections of exoplanets via the transit method. While observing 55 Cancri e, which is known to transit, ASTERIA measured a miniscule change in brightness, about 0.04 percent, when the super- Earth crossed in front of its star. This transit measurement is the first of its kind for CubeSats (the class of satellites to which ASTERIA belongs) which are about the size of a briefcase and hitch a ride to space as secondary payloads on rockets used for larger spacecraft. -
Arxiv:2009.03244V1 [Astro-Ph.HE] 7 Sep 2020
Advances in Understanding High-Mass X-ray Binaries with INTEGRAL and Future Directions Peter Kretschmara, Felix Furst¨ b, Lara Sidolic, Enrico Bozzod, Julia Alfonso-Garzon´ e, Arash Bodagheef, Sylvain Chatyg,h, Masha Chernyakovai,j, Carlo Ferrignod, Antonios Manousakisk,l, Ignacio Negueruelam, Konstantin Postnovn,o, Adamantia Paizisc, Pablo Reigp,q, Jose´ Joaqu´ın Rodes-Rocar,s, Sergey Tsygankovt,u, Antony J. Birdv, Matthias Bissinger ne´ Kuhnel¨ w, Pere Blayx, Isabel Caballeroy, Malcolm J. Coev, Albert Domingoe, Victor Doroshenkoz,u, Lorenzo Duccid,z, Maurizio Falangaaa, Sergei A. Grebenevu, Victoria Grinbergz, Paul Hemphillab, Ingo Kreykenbohmac,w, Sonja Kreykenbohm nee´ Fritzad,ac, Jian Liae, Alexander A. Lutovinovu, Silvia Mart´ınez-Nu´nez˜ af, J. Miguel Mas-Hessee, Nicola Masettiag,ah, Vanessa A. McBrideai,aj,ak, Andrii Neronovh,d, Katja Pottschmidtal,am,Jer´ omeˆ Rodriguezg, Patrizia Romanoan, Richard E. Rothschildao, Andrea Santangeloz, Vito Sgueraag,Rudiger¨ Staubertz, John A. Tomsickap, Jose´ Miguel Torrejon´ r,s, Diego F. Torresaq,ar, Roland Walterd,Jorn¨ Wilmsac,w, Colleen A. Wilson-Hodgeas, Shu Zhangat Abstract High mass X-ray binaries are among the brightest X-ray sources in the Milky Way, as well as in nearby Galaxies. Thanks to their highly variable emissions and complex phenomenology, they have attracted the interest of the high energy astrophysical community since the dawn of X-ray Astronomy. In more recent years, they have challenged our comprehension of physical processes in many more energy bands, ranging from the infrared to very high energies. In this review, we provide a broad but concise summary of the physical processes dominating the emission from high mass X-ray binaries across virtually the whole electromagnetic spectrum. -
The XGIS Instrument On-Board THESEUS: the Detection Plane and On-Board Electronics
Downloaded from orbit.dtu.dk on: Sep 24, 2021 The XGIS instrument on-board THESEUS: The detection plane and on-board electronics Fuschino, F.; Campana, R.; Labanti, C.; Amati, L.; Virgilli, E.; Terenzi, L.; Bellutti, P.; Bertuccio, G.; Borghi, G.; Bune Jensen, L. C. Total number of authors: 35 Published in: Space Telescopes and Instrumentation 2020: Ultraviolet to Gamma Ray Link to article, DOI: 10.1117/12.2561002 Publication date: 2020 Document Version Publisher's PDF, also known as Version of record Link back to DTU Orbit Citation (APA): Fuschino, F., Campana, R., Labanti, C., Amati, L., Virgilli, E., Terenzi, L., Bellutti, P., Bertuccio, G., Borghi, G., Bune Jensen, L. C., Ficorella, F., Gandola, M., Gemelli, A., Grassi, M., Hedderman, P., Kuvvetli, I., la Rosa, G., Lorenzi, P., Malcovati, P., ... Zorzi, N. (2020). The XGIS instrument on-board THESEUS: The detection plane and on-board electronics. In J-W. A. den Herder, S. Nikzad, & K. Nakazawa (Eds.), Space Telescopes and Instrumentation 2020: Ultraviolet to Gamma Ray (Vol. 11444). [114448R] SPIE - International Society for Optical Engineering. Proceedings of SPIE, the International Society for Optical Engineering Vol. 11444 https://doi.org/10.1117/12.2561002 General rights Copyright and moral rights for the publications made accessible in the public portal are retained by the authors and/or other copyright owners and it is a condition of accessing publications that users recognise and abide by the legal requirements associated with these rights. Users may download and print one copy of any publication from the public portal for the purpose of private study or research. -
Real-Time Fault Detection and Situational Awareness for Rovers: Report on the Mars Technology Program Task
Real-time Fault Detection and Situational Awareness for Rovers: Report on the Mars Technology Program Task Richard Dearden, Thomas Willeke Frank Hutter fRIACS, QSS Group Inc.g / NASA Ames Research Center Fachbereich Informatik M.S. 269-3, Moffett Field, CA 94035, USA Technische Universitat¨ Darmstadt, Germany fdearden,[email protected] [email protected] Reid Simmons, Vandi Verma Sebastian Thrun Carnegie Mellon University Computer Science Department, Stanford University Pittsburg, PA 15213, USA 353 Serra Mall, Gates Bldg 154 freids,[email protected] Stanford, CA 94305, USA [email protected] Abstract— An increased level of autonomy is critical for 1. INTRODUCTION meeting many of the goals of advanced planetary rover mis- This paper reports the results from a study done as part of sions such as NASA’s 2009 Mars Science Lab. One impor- NASA’s Mars Technology Program entitled “Real-time Fault tant component of this is state estimation, and in particular Detection and Situational Awareness for Rovers”. The main fault detection on-board the rover. In this paper we describe goal of this project was to develop and demonstrate a fault- the results of a project funded by the Mars Technology Pro- detection technology capable of operating on-board a Mars gram at NASA, aimed at developing algorithms to meet this rover in real-time. requirement. We describe a number of particle filtering-based algorithms for state estimation which we have demonstrated Fault diagnosis is a critical task for autonomous operation of successfully on diagnosis problems including the K-9 rover systems such as spacecraft and planetary rovers. -
ASTERIA Data Guide
ASTERIA Data Users Guide (v2) Mary Knapp November 2019 1 Overview This document describes the formatting and idiosyncrasies of ASTERIA photometric data. ASTERIA is the Arcsecond Space Telescope Enabling Research In Astrophysics. 2 Brief ASTERIA System Description ASTERIA is a 6U (10 cm x 20 cm x 34 cm) CubeSat spacecraft. ASTERIA was launched August 2017 as payload to the International Space Station and deployed into orbit on November 20, 2017. ASTERIA's current orbit matches the ISS inclination and has an average altitude of approximately 400 km. In this orbit, ASTERIA experiences an average of 30 minutes in Earth's shadow (eclipse) and 60 minutes in sunlight. ASTERIA is 3-axis stabilized via a set of reaction wheels. The reaction wheels are part of the XACT attitude control system provided by Blue Canyon Technology (BCT). Torque rods are used for reaction wheel desaturation. ASTERIA carries a small refractive telescope (f/1.4, ∼85 mm). The telescope focuses light on a 2592 x 2192 pixel CMOS detector. The detector pixels are 6.5 microns, yielding a plate scale of ∼15 arcsec/pixel. The full field of view of the detector is ∼9 x 10 degrees. ASTERIA's camera is deliberately defocused in order to oversample the PSF. 3 Definitions List of definitions for acronyms and other terms with specific meanings in the context of ASTERIA. • Epoch: The spacecraft epoch refers to the bootcount of the spacecraft. An epoch begins when ASTE- RIA's flight computer reboots and sets time to January 1, 1970 (the zero point for Unix timestamps). • Uptime: Spacecraft time is relative and is tracked in seconds from flight computer boot. -
Exoplanet Program Analysis Group (Exopag) Report Astrophysics Advisory Committee (APAC) Meeting
Exoplanet Program Analysis Group (ExoPAG) Report Astrophysics Advisory Committee (APAC) Meeting Victoria Meadows (ExoPAG Chair) Oct 23rd, 2018 Credit: NASA ExoPAG EC Membership Victoria Meadows (Chair) University of Washington Tom Barclay Goddard Space Flight Center Jessie Christiansen NExScI/Caltech Rebecca Jensen-Clem UC-Berkeley Tiffany Glassman Northrup Grumman Aerospace Systems Eliza Kempton University of Maryland Dimitri Mawet Caltech Michael Meyer University of Michigan Tyler Robinson Northern Arizona University Chris Stark Space Telescope Science Institute Johanna Teske Carnegie Observatories -> DTM Alan Boss (Past Chair) Carnegie Institution of Washington Martin Still (ex officio) NASA Credit: NASA Status of SAGs and SIGs Year SAG or SIG Title Lead 2018 SAG 16 Exoplanet Biosignatures (closed) Domagal-Goldman 2018 SAG 17 Community Resources Needed for K2 and TESS Planetary Candidate Confirmation Ciardi & Pepper (requesting closeout at this meeting) -- SAG 19 Exoplanet imaging signal detection theory and rigorous contrast metrics (active - Mawet & Jensen-Clem closeout expected in 2019) -- SIG 2 Exoplanet Demographics (Initiated at last meeting) Christiansen & Meyer -- SAG 20 Impact of JWST Delay on Exoplanet Science (requesting initiation at this meeting) Teske & Deming Credit: NASA ExoPAG Recent Activities • Robinson led the ExoPAG EC in agenda development for the ExoPAG19 meeting to be held in Seattle, Jan 5-6, 2019, prior to the Winter AAS. – Mini-science symposium on characterization of nearby planetary systems. – Showcase for exoplanet inputs to the Decadal Survey. • Additional call for an ExEP-funded program to support student travel to the ExoPAG19 meetings. Deadline Nov 1. Stark to administer program with ExEP. • Closeout of SAG17 presented by Ciardi to ExoPAG18 on July 29th. -
AWS Ground Station Antenna ASTERIA AWS
N E T 3 0 8 - R Enabling automated astrophysics with AWS Ground Station Tom Soderstrom Shayn Hawthorne CTIO, JPL Office of the CIO Senior Manager, AWS Ground Station Amazon Web Services © 2019, Amazon Web Services, Inc. or its affiliates. All rights reserved. Agenda Intro to AWS Ground Station AWS Ground Station overview – customer view Demo ASTERIA AWS Ground Station experiment AWS Ground Station • Managed ground stations • No long-term commitments required • Simple, pay-as-you-go pricing – pay by the minute • Close proximity to AWS Regions • Self-service scheduling • First-come, first- served Traditional ground station challenges • Build, lease, or rent • Large up-front capital to build • Expensive and complex to maintain • Inelastic scaling • Opaque pricing • Scheduling conflicts and contention High-level architecture Customer VPC Downlink Antenna Tracking Mission data control processing EC2 Uplink Antenna Software radio / System data recovery Digitizer / Scheduling Tracking radio Telemetry and Control Self-service and automation through AWS Console and AWS APIs/SDK AWS Security and Identity Key events • Customers configure what they want to do (Mission Profile + Configs) • Customers reserve/schedule a Contact (Mission Profile + Configs + Satellite + Ground Station + Timing) • System executes the Contact Configuration • Customers create a Mission Profile consisting of multiple Configs to configure the antenna system for a contact • Configs and Mission Profiles are created via an API Mission Profile Dataflow Dataflow Edge Tracking Config -
Ariadne's Transformation
Bard College Bard Digital Commons Senior Projects Spring 2020 Bard Undergraduate Senior Projects Spring 2020 Ariadne’s Transformation: Presenting Femininity From Roman Poetry to Modern Opera Xinyi Wang Bard College, [email protected] Follow this and additional works at: https://digitalcommons.bard.edu/senproj_s2020 Part of the Classics Commons, and the Music Commons This work is licensed under a Creative Commons Attribution-Noncommercial-No Derivative Works 4.0 License. Recommended Citation Wang, Xinyi, "Ariadne’s Transformation: Presenting Femininity From Roman Poetry to Modern Opera" (2020). Senior Projects Spring 2020. 165. https://digitalcommons.bard.edu/senproj_s2020/165 This Open Access work is protected by copyright and/or related rights. It has been provided to you by Bard College's Stevenson Library with permission from the rights-holder(s). You are free to use this work in any way that is permitted by the copyright and related rights. For other uses you need to obtain permission from the rights- holder(s) directly, unless additional rights are indicated by a Creative Commons license in the record and/or on the work itself. For more information, please contact [email protected]. Ariadne’s Transformation: Presenting Femininity From Roman Poetry to Modern Opera Senior Project Submitted to The Division of Languages and Literature of Bard College by Xinyi Wang Annandale-on-Hudson, New York May 2020 Acknowledgments To my advisor Lauren Curtis, for her warm and inspiring presence, for guiding me through this project with constructive suggestions and valuable input, and for spending incredible time on polishing my thoughts and writing. To my tutor Emily Giangiulio, for her warm support, and for carefully helping me with grammar. -
Professor Sara Seager Massachusetts Institute of Technology
Professor Sara Seager Massachusetts Institute of Technology Address: Department of Earth Atmospheric and Planetary Science Building 54 Room 1718 Massachusetts Institute of Technology 77 Massachusetts Avenue Cambridge, MA, USA 02139 Phone: (617) 253-6779 (direct) E-mail: [email protected] Citizenship: US citizen since 7/20/2010 Birthdate: 7/21/1971 Professional History 1/2011–present: Massachusetts Institute of Technology, Cambridge, MA USA • Class of 1941 Professor (1/2012–present) • Professor of Planetary Science (7/2010–present) • Professor of Physics (7/2010–present) • Professor of Aeronautical and Astronautical Engineering (7/2017–present) 1/2007–12/2011: Massachusetts Institute of Technology, Cambridge, MA USA • Ellen Swallow Richards Professorship (1/2007–12/2011) • Associate Professor of Planetary Science (1/2007–6/2010) • Associate Professor of Physics (7/2007–6/2010) • Chair of Planetary Group in the Dept. of Earth, Atmospheric, and Planetary Sciences (2007–2015) 08/2002–12/2006: Carnegie Institution of Washington, Washington, DC, USA • Senior Research Staff Member 09/1999–07/2002: Institute for Advanced Study, Princeton NJ • Long Term Member (02/2001–07/2002) • Short Term Member (09/1999–02/2001) • Keck Fellow Educational History 1994–1999 Ph.D. “Extrasolar Planets Under Strong Stellar Irradiation” Department of Astronomy, Harvard University, MA, USA 1990–1994 B.Sc. in Mathematics and Physics University of Toronto, Canada NSERC Science and Technology Fellowship (1990–1994) Awards and Distinctions Academic Awards and Distinctions 2018 American Philosophical Society Member 2018 American Academy of Arts and Sciences Member 2015 Honorary PhD, University of British Columbia 2015 National Academy of Sciences Member 2013 MacArthur Fellow 2012 Raymond and Beverly Sackler Prize in the Physical Sciences 2012 American Association for the Advancement of Science Fellow 2007 Helen B.