CNN Classification of Mars Imagery for the PDS Imaging Atlas
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Cassis Observations of Fresh Bright Slope Streak Candidates in Arabia Terra
EPSC Abstracts Vol. 13, EPSC-DPS2019-1720-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. CaSSIS observations of fresh bright slope streak candidates in Arabia Terra A.Valantinas1, N. Thomas1, A. Pommerol1, P. Becerra1, E. Hauber2, L. L. Tornabene3, G. Cremonese4 and the CaSSIS Team1. 1Physikalisches Institut, University of Bern, Sidlerstrasse 5, 3012 Bern, Switzerland ([email protected]), 2Deutsches Zentrum für Luft-und Raumfahrt, Institut für Planetenforschung, Berlin, Germany, 3CPSX, Earth Sci., Western University, London, Canada, 4Osservatorio Astronomico di Padova, INAF, Padova, Italy. 1. Introduction distributions on a grid of ~16,000 hexa-gons, each 20 km in diameter. Bright slope streaks are elusive increased albedo sur- face features found on Martian slopes in low thermal 3. Results inertia regions [1, 2]. These elongated features are thought to result from the more common dark slope Our study reveals plausibly fresh bright slope streaks streaks [3, 4], which gradually fade or brighten with in several locations in Arabia Terra. For example, time [5]. Several hypotheses attempt to explain dark two images taken by CTX show a region with several slope streak origin. Dry-based models encompass dark slope streaks, but bright slope streaks in this dust mass wasting, avalanching or granular flows [1, location are only visible in CaSSIS (see Fig. 1). 6-7]. Aqueous models include subsurface aquifers, However, some bright slope streaks can be seen in lubricated dust flows and ground staining from saline both CTX frames, outside of the area shown in the fluids [8-12]. Various properties of dark slope streak figure. -
Change Detection in Mars Orbital Images Using Dynamic Landmarking
CHANGE DETECTION IN MARS ORBITAL IMAGES USING DYNAMIC LANDMARKING. Kiri L. Wagstaff1, Julian Panetta2, Adnan Ansar1, Melissa Bunte3, Ronald Greeley3, Mary Pendleton Hoffer3, and Nor- bert Schorghofer¨ 4, 1Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Dr., Pasadena, CA 91109 USA ([email protected]), 2California Institute of Technology, 1200 E. California Blvd., Pasadena, CA 91125 USA, 3Arizona State University, School of Earth and Space Exploration, Box 871404, Tempe, AZ 85287 USA, 4University of Hawaii, Institute of Astronomy, 2680 Woodlawn Dr., Honolulu, HI 96822 USA. Introduction: As of December 2009, there are a histogram h of pixel values in a window surrounding p: more than 1,500,000 orbital images of Mars available on 255 X the Planetary Data System’s Imaging Node (from Mars S(p) = h(i)|I(p) − i|, Odyssey, Mars Express, Mars Global Surveyor, and Mars i=0 Reconnaissance Orbiter). The volume of image data is steadily increasing, as is the number of repeat images that where h(i) is the histogram count for grayscale value allow for the possibility of detecting surface changes such i and I(p) is the intensity of pixel p. Computing the as dark slope streaks [1], new impact craters and gul- salience of every pixel in the image yields a salience map. lies [2], ground ice excavated by fresh impact craters [3], To find landmarks, we specify a salience threshold to gen- etc. The number of overlapping image pairs is growing erate contours around high-salience regions. For each quickly enough that there is a need for automated meth- landmark, we extract the following attributes: mean and ods for detecting and characterizing those changes. -
Planetary Report Report
The PLANETARYPLANETARY REPORT REPORT Volume XXIX Number 1 January/February 2009 Beyond The Moon From The Editor he Internet has transformed the way science is On the Cover: Tdone—even in the realm of “rocket science”— The United States has the opportunity to unify and inspire the and now anyone can make a real contribution, as world’s spacefaring nations to create a future brightened by long as you have the will to give your best. new goals, such as the human exploration of Mars and near- In this issue, you’ll read about a group of amateurs Earth asteroids. Inset: American astronaut Peggy A. Whitson who are helping professional researchers explore and Russian cosmonaut Yuri I. Malenchenko try out training Mars online, encouraged by Mars Exploration versions of Russian Orlan spacesuits. Background: The High Rovers Project Scientist Steve Squyres and Plane- Resolution Camera on Mars Express took this snapshot of tary Society President Jim Bell (who is also head Candor Chasma, a valley in the northern part of Valles of the rovers’ Pancam team.) Marineris, on July 6, 2006. Images: Gagarin Cosmonaut Training This new Internet-enabled fun is not the first, Center. Background: ESA nor will it be the only, way people can participate in planetary exploration. The Planetary Society has been encouraging our members to contribute Background: their minds and energy to science since 1984, A dust storm blurs the sky above a volcanic caldera in this image when the Pallas Project helped to determine the taken by the Mars Color Imager on Mars Reconnaissance Orbiter shape of a main-belt asteroid. -
Geomorphological Indication of Ancient, Recent, and Possibly Present-Day Aqueous Activity on Mars
地学雑誌 Journal of Geography(Chigaku Zasshi) 125(1)121–132 2016 doi:10.5026/jgeography.125.121 Geomorphological Indication of Ancient, Recent, and Possibly Present-day Aqueous Activity on Mars James M. DOHM* and Hideaki MIYAMOTO* [Received 31 March, 2015; Accepted 5 December, 2015] Abstract This paper overviews water sculpted Martian landscapes, ancient through to possibly present day, which have become more pronounced through each new orbiting, landing, and roving mission. Geomorphological evidence of ancient aqueous activity associated with lakes and putative oceans includes a diversity of features. Features include sedimentary sequences, debris flows, fluvial valleys, alluvial fans, giant polygons, and glacial and periglacial landscapes. Arguably one of the most significant geomorphological indicators of a paleoocean is deltaic landforms identified along a topographic zonal boundary which correlates with reported putative shorelines. Other evidence includes distinct geochemical/mineralogical/elemental signatures of aqueous weathering. In addition, relatively high-resolution imaging cameras onboard the Mars Global Surveyor, Mars Odyssey, and Mars Reconnaissance Orbiter have detailed features which indicate recent and possibly present-day aqueous activity such as slope streaks, slope linea, gullies which occur along faults and fractures and source from geologic contacts and tectonic structures, and possible open-system pingos, among other feature types. Ancient, recent, and possibly present-day features point to both surface and subsurface aqueous environments throughout time, and thus making Mars a prime target to address the ever- important question of whether life exists beyond the Earth. Key words: Mars, geomorphology, hydrology, oceans, outflow channel, gullies, slope linea Mitchell and Wilson, 2003). Perhaps the most I.Introduction surprising finding from the post-Viking mission Mars' missions continue to reveal aqueous- are a variety of features that indicate the Mars modified Martian landscapes. -
THE MARS 2020 ROVER ENGINEERING CAMERAS. J. N. Maki1, C
51st Lunar and Planetary Science Conference (2020) 2663.pdf THE MARS 2020 ROVER ENGINEERING CAMERAS. J. N. Maki1, C. M. McKinney1, R. G. Willson1, R. G. Sellar1, D. S. Copley-Woods1, M. Valvo1, T. Goodsall1, J. McGuire1, K. Singh1, T. E. Litwin1, R. G. Deen1, A. Cul- ver1, N. Ruoff1, D. Petrizzo1, 1Jet Propulsion Laboratory, California Institute of Technology (4800 Oak Grove Drive, Pasadena, CA 91109, [email protected]). Introduction: The Mars 2020 Rover is equipped pairs (the Cachecam, a monoscopic camera, is an ex- with a neXt-generation engineering camera imaging ception). The Mars 2020 engineering cameras are system that represents a significant upgrade over the packaged into a single, compact camera head (see fig- previous Navcam/Hazcam cameras flown on MER and ure 1). MSL [1,2]. The Mars 2020 engineering cameras ac- quire color images with wider fields of view and high- er angular/spatial resolution than previous rover engi- neering cameras. Additionally, the Mars 2020 rover will carry a new camera type dedicated to sample op- erations: the Cachecam. History: The previous generation of Navcams and Hazcams, known collectively as the engineering cam- eras, were designed in the early 2000s as part of the Mars Exploration Rover (MER) program. A total of Figure 1. Flight Navcam (left), Flight Hazcam (middle), 36 individual MER-style cameras have flown to Mars and flight Cachecam (right). The Cachecam optical assem- on five separate NASA spacecraft (3 rovers and 2 bly includes an illuminator and fold mirror. landers) [1-6]. The MER/MSL cameras were built in two separate production runs: the original MER run Each of the Mars 2020 engineering cameras utilize a (2003) and a second, build-to-print run for the Mars 20 megapixel OnSemi (CMOSIS) CMOS sensor Science Laboratory (MSL) mission in 2008. -
Operation and Performance of the Mars Exploration Rover Imaging System on the Martian Surface
Operation and Performance of the Mars Exploration Rover Imaging System on the Martian Surface Justin N. Maki Jet Propulsion Laboratory California Institute of Technology Pasadena, CA USA [email protected] Todd Litwin, Mark Schwochert Jet Propulsion Laboratory California Institute of Technology Pasadena, CA USA Ken Herkenhoff United States Geological Survey Flagstaff, AZ USA Abstract - The Imaging System on the Mars Exploration Rovers has successfully operated on the surface of Mars for over one Earth year. The acquisition of hundreds of panoramas and tens of thousands of stereo pairs has enabled the rovers to explore Mars at a level of detail unprecedented in the history of space exploration. In addition to providing scientific value, the images also play a key role in the daily tactical operation of the rovers. The mobile nature of the MER surface mission requires extensive use of the imaging system for traverse planning, rover localization, remote sensing instrument targeting, and robotic arm placement. Each of these activity types requires a different set of data compression rates, surface Figure 1. The Mars Exploration Spirit Rover, as viewed by coverage, and image acquisition strategies. An overview the Navcam shortly after lander egress early in the mission. of the surface imaging activities is provided, along with a presents an overview of the operation and performance of summary of the image data acquired to date. the MER Imaging System. Keywords: Imaging system, cameras, rovers, Mars, 1.2 Imaging System Design operations. The MER cameras are classified into five types: Descent cameras, Navigation cameras (Navcam), Hazard Avoidance 1 Introduction cameras (Hazcam), Panoramic cameras (Pancam), and Microscopic Imager (MI) cameras. -
Of Curiosity in Gale Crater, and Other Landed Mars Missions
44th Lunar and Planetary Science Conference (2013) 2534.pdf LOCALIZATION AND ‘CONTEXTUALIZATION’ OF CURIOSITY IN GALE CRATER, AND OTHER LANDED MARS MISSIONS. T. J. Parker1, M. C. Malin2, F. J. Calef1, R. G. Deen1, H. E. Gengl1, M. P. Golombek1, J. R. Hall1, O. Pariser1, M. Powell1, R. S. Sletten3, and the MSL Science Team. 1Jet Propulsion Labora- tory, California Inst of Technology ([email protected]), 2Malin Space Science Systems, San Diego, CA ([email protected] ), 3University of Washington, Seattle. Introduction: Localization is a process by which tactical updates are made to a mobile lander’s position on a planetary surface, and is used to aid in traverse and science investigation planning and very high- resolution map compilation. “Contextualization” is hereby defined as placement of localization infor- mation into a local, regional, and global context, by accurately localizing a landed vehicle, then placing the data acquired by that lander into context with orbiter data so that its geologic context can be better charac- terized and understood. Curiosity Landing Site Localization: The Curi- osity landing was the first Mars mission to benefit from the selection of a science-driven descent camera (both MER rovers employed engineering descent im- agers). Initial data downlinked after the landing fo- Fig 1: Portion of mosaic of MARDI EDL images. cused on rover health and Entry-Descent-Landing MARDI imaged the landing site and science target (EDL) performance. Front and rear Hazcam images regions in color. were also downloaded, along with a number of When is localization done? MARDI thumbnail images. The Hazcam images were After each drive for which Navcam stereo da- used primarily to determine the rover’s orientation by ta has been acquired post-drive and terrain meshes triangulation to the horizon. -
The Mars Science Laboratory (Msl) Navigation Cameras (Navcams)
42nd Lunar and Planetary Science Conference (2011) 2738.pdf THE MARS SCIENCE LABORATORY (MSL) NAVIGATION CAMERAS (NAVCAMS). J. N. Maki1, D. Thiessen1, A.Pourangi1, P. Kobzeff1, L. Scherr1, T. Elliott1, A. Dingizian1, Beverly St. Ange1, 1Jet Propulsion La- boratory/California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109. Introduction: The Mars Science Laboratory (MSL) The camera plate, which also holds the Mastcam and Rover (scheduled for launch in November/December Chemcam instruments, is mounted to a 0.85-meter 2011) will fly four Navigation Cameras (Navcams). high Remote Sensing Mast (RSM), which points the The key requirements of the Navcam imaging system cameras in the azimuth and elevation directions. The are: 1) provide terrain context for traverse planning RSM is attached to the rover deck, which is 1.1 meters and Mastcam/Chemcam pointing, 2) provide a 360- above the nominal surface. The resultant configura- degree field of regard at <1 mrad/pixel angular resolu- tion places the Navcams 1.9 meters above the Martian tion, 3) provide stereo ranging data out to 100 m, and surface (0.4 meters higher than the MER Navcams). 4) use of a broadband, visible filter. The Navcams The MSL Navcams are build-to-print copies were built at the Jet Propulsion Laboratory in Pasade- of the Mars Exploration Rover (MER) cameras, which na, CA. are described in detail in [1]. The main difference Instrument Details: The mounting locations of the between the MER and MSL cameras is that the MSL Navcams are shown in figure 1. Navcams have slightly more powerful heaters to allow operation at colder ambient temperatures. -
A Multi-Resolution 3D Reconstruction Tool: Exemplar Using MSL Navcam PDS and Mastcam PIO Imagery
EPSC Abstracts Vol. 8, EPSC2013-584-3, 2013 European Planetary Science Congress 2013 EEuropeaPn PlanetarSy Science CCongress c Author(s) 2013 A Multi-resolution 3D Reconstruction Tool: Exemplar using MSL NavCam PDS and MastCam PIO imagery Y. Tao, J.-P. Muller Imaging Group, Mullard Space Science Laboratory, Dept. of Space and Climate Physics, University College London, Holmbury St. Mary, Dorking, Surrey, RH56NT, UK ([email protected]; [email protected]) Abstract Based on the development work done during the PRoVisG project, we have extended our wide The acquisition of multi-resolution ground level baseline stereo reconstruction tool to be able to imaging data from different cameras onboard the produce multi-resolution 3D products via co- NASA MSL Curiosity, such as the Hazcams, registration of images from different cameras. In this Navcams, Mastcam and MAHLI, enable us to study a paper, we demonstrate this data fusion capability particular area/objects at various levels of detail. using the publicly released NavCam stereo PDS data However, to analyze the structural differences to provide 3D terrain context and co-registered properly or to do any extensive classification and MastCam images from the NASA Public Information recognition requires 3D information as well as the Office (PIO) website in order to reconstruct a high- 2D data from all of these cameras. This requires 3D resolution 3D colour model. reconstruction and co-registration of stereo rover and non-stereo rover imagery. 2. Methods In this paper, we describe the operation of a stereo We initially use the CAHVOR camera model stored reconstruction tool (StRec) with examples on 3D in the PDS header for intra-stereo reconstruction and ground reconstruction from both stereo and non- inter-stereo network building. -
Detecção Automática E Análise Temporal De Slope Streaks Na Superfície De Marte
UNIVERSIDADE ESTADUAL PAULISTA Faculdade de Ciências e Tecnologia Programa de Pós-Graduação em Ciências Cartográficas FERNANDA PUGA SANTOS CARVALHO DETECÇÃO AUTOMÁTICA E ANÁLISE TEMPORAL DE SLOPE STREAKS NA SUPERFÍCIE DE MARTE TESE Presidente Prudente 2016 FERNANDA PUGA SANTOS CARVALHO DETECÇÃO AUTOMÁTICA E ANÁLISE TEMPORAL DE SLOPE STREAKS NA SUPERFÍCIE DE MARTE Tese apresentada ao Programa de Pós-Graduação em Ciências Cartográficas para a obtenção do título de doutor pela Faculdade de Ciências e Tecnologia da Universidade Estadual Paulista “Júlio de Mesquita Filho” Campus de Presidente Prudente. Área de concentração: Computação de Imagens Orientador: Professor Titular Erivaldo Antônio da Silva. Coorientador: Dr. Pedro Miguel Berardo Duarte Pina. Presidente Prudente Março de 2016 FICHA CATALOGRÁFICA Carvalho, Fernanda Puga Santos. C323d Detecção automática e análise temporal de slope streaks na superfície de Marte / Fernanda Puga Santos Carvalho. - Presidente Prudente : [s.n], 2016 76 f. : il. Orientador: Erivaldo Antônio da Silva Coorientador: Pedro Miguel Berardo Duarte Pina Tese (doutorado) - Universidade Estadual Paulista, Faculdade de Ciências e Tecnologia Inclui bibliografia 1. Slope streaks. 2. Detecção automática. 3. Análise temporal. I. Carvalho, Fernanda Puga Santos. II. Silva, Erivaldo Antônio da III. Pina, Pedro Miguel Berardo Duarte. IV. Universidade Estadual Paulista. Faculdade de Ciências e Tecnologia. V. Detecção automática e análise temporal de slope streaks na superfície de Marte. AGRADECIMENTOS Gostaria de registrar o meu sincero agradecimento a todos que contribuíram de forma direta e indireta para o desenvolvimento deste trabalho. À minha família, em especial ao meu marido André, cujo apoio e incentivo incondicional foram fundamentais para realização deste meu sonho. Ao professor Erivaldo, pela confiança na minha capacidade em desenvolver uma tese de doutorado e pelo apoio de sempre. -
The Mars Science Laboratory Engineering Cameras
Space Sci Rev DOI 10.1007/s11214-012-9882-4 The Mars Science Laboratory Engineering Cameras J. Maki · D. Thiessen · A. Pourangi · P. Kobzeff · T. Litwin · L. Scherr · S. Elliott · A. Dingizian · M. Maimone Received: 21 December 2011 / Accepted: 5 April 2012 © Springer Science+Business Media B.V. 2012 Abstract NASA’s Mars Science Laboratory (MSL) Rover is equipped with a set of 12 en- gineering cameras. These cameras are build-to-print copies of the Mars Exploration Rover cameras described in Maki et al. (J. Geophys. Res. 108(E12): 8071, 2003). Images returned from the engineering cameras will be used to navigate the rover on the Martian surface, de- ploy the rover robotic arm, and ingest samples into the rover sample processing system. The Navigation cameras (Navcams) are mounted to a pan/tilt mast and have a 45-degree square field of view (FOV) with a pixel scale of 0.82 mrad/pixel. The Hazard Avoidance Cameras (Hazcams) are body-mounted to the rover chassis in the front and rear of the vehicle and have a 124-degree square FOV with a pixel scale of 2.1 mrad/pixel. All of the cameras uti- lize a 1024 × 1024 pixel detector and red/near IR bandpass filters centered at 650 nm. The MSL engineering cameras are grouped into two sets of six: one set of cameras is connected to rover computer “A” and the other set is connected to rover computer “B”. The Navcams and Front Hazcams each provide similar views from either computer. The Rear Hazcams provide different views from the two computers due to the different mounting locations of the “A” and “B” Rear Hazcams. -
High Concentrations of Manganese and Sulfur in Deposits on Murray Ridge, Endeavour Crater, Marsk
American Mineralogist, Volume 101, pages 1389–1405, 2016 High concentrations of manganese and sulfur in deposits on Murray Ridge, Endeavour Crater, Marsk RAYMOND E. ARVIDSON1,*, STEVEN W. SQUYreS2, RICHARD V. MOrrIS3, ANDrew H. KNOLL4, RALF GELLerT5, BENTON C. CLArk6, JEFFreY G. CATALANO1, BRAD L. JOLLIFF1, SCOTT M. MCLENNAN7, KENNETH E. HerkeNHOFF8, SCOTT VANBOMMEL5, DAVID W. MITTLEFEHLDT3, JOHN P. GROTZINger9, EDWARD A. GUINNESS1, JEFFreY R. JOHNSON10, JAMES F. BELL III11, WILLIAM H. FArrAND6, NATHAN STEIN1, VALerIE K. FOX1, MATTHew P. GOLOMbek12, MArgAreT A.G. HINKLE1, WENDY M. CALVIN13, AND PAULO A. DE SOUZA JR.14 1Department of Earth and Planetary Sciences, Washington University in Saint Louis, St. Louis, Missouri 63130, U.S.A. 2Department of Astronomy, Cornell University, Ithaca, New York 14853, U.S.A. 3Johnson Space Center, Houston, Texas 77058, U.S.A. 4Department of Organismic and Evolutionary Biology, Harvard University, Cambridge, Massachusetts 02138, U.S.A. 5Department of Physics, University of Guelph, Guelph, Ontario N1G 2W1, Canada 6Space Science Institute, Boulder, Colorado 80301, U.S.A. 7Department of Geosciences, Stony Brook University, Stony Brook, New York 11794, U.S.A. 8U.S. Geological Survey, Astrogeology Science Center, Flagstaff, Arizona 86001, U.S.A. 9Division of Geological and Planetary Sciences, California Institute of Technology, Pasadena, California 91125, U.S.A. 10Johns Hopkins University, Applied Physics Laboratory, Laurel, Maryland 20723, U.S.A. 11School of Earth & Space Exploration, Arizona State University, Tempe, Arizona 85281, U.S.A. 12California Institute of Technology/Jet Propulsion Laboratory, Pasadena, California 91011 13Geological Sciences and Engineering, University of Nevada, Reno, Nevada 89503, U.S.A. 14CSIRO Digital Productivity Flagship, Hobart, Tasmania 7004, Australia ABSTRACT Mars Reconnaissance Orbiter HiRISE images and Opportunity rover observations of the ~22 km wide Noachian age Endeavour Crater on Mars show that the rim and surrounding terrains were densely fractured during the impact crater-forming event.