(Espacio) Comunicaciones de Congresos
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Examinando (Espacio) Comunicaciones de Congresos por Autor "Arruego, Ignacio"
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Ítem Acceso Abierto Advance Dust Devil Detection with AI using Mars2020 MEDA instrument(Europlanet, 2024-07-03) Apéstigue, Víctor; Mohino, Inma; Gil, Roberto; Toledo, D.; Arruego, Ignacio; Hueso, R.; Martínez, Germán M.; Lemmon, M. T.; Newman, C. E.; Genzer, María; De la Torre Juárez, M.; Rodríguez Manfredi, J. A.Mars’ dust cycle is a critical factor that drives the weather and climate of the planet. Airborne dust affects the energy balance that drives the atmospheric dynamic. Therefore, for studying the present-day and recent-past climate of Mars we need to observe and understand the different processes involved in the dust cycle. To this end, the Mars Environmental Dynamics Analyser (MEDA) station [1] includes a set of sensors capable of measuring the radiance fluxes, the wind direction and velocity, the pressure, and the humidity over the Martian surface. Combining these observations with radiative transfer (RT) simulations, airborne dust particles can be detected and characterized (optical depth, particle size, refractive index) along the day. The retrieval of these dust properties allows us to analyze dust storms or dust-lifting events, such as dust devils, on Mars [2][3]. Dust devils are thought to account for 50% of the total dust budget, and they represent a continuous source of lifted dust, active even outside the dust storms season. For these reasons, they have been proposed as the main mechanism able to sustain the ever-observed dust haze of the Martian atmosphere. Our radiative transfer simulations indicate that variations in the dust loading near the surface can be detected and characterized by MEDA radiance sensor RDS [4]. This study reanalyzes the dataset of dust devil detections obtained in [3] employing artificial intelligence techniques including anomaly detection based on autoencoders [5] and deep learning models [6] to analyze RDS and pressure sensor data. As we will show, preliminary results indicate that our AI models can successfully identify and characterize these phenomena with high accuracy. The final aim is to develop a powerful tool that can improve the database for the following sols of the mission, and subsequently extend its use for other atmospheric studies.Ítem Acceso Abierto Aerosol optical properties observed by MEDA Radiation an Dust Sensor (RDS) at Jezero Crater, Mars(Europlanet, 2024-07) Rodríguez Veloso, Raúl; Toledo, D.; Apéstigue, Víctor; Arruego, Ignacio; Lemmon, M. T.; Smith, Michael D.; Martínez, Germán M.; Vicente Retortillo, Álvaro; Jiménez Martín, Juan José; García Menéndez, Elisa; Viúdez Moreiras, Daniel; Sánchez Lavega, Agustín; Pérez Hoyos, S.; Sebastián, E.; De la Torre Juárez, M.; Rodríguez Manfredi, J. A.Aerosols on Mars are a primary elements for studying the interaction between the solar radiation and the atmosphere and surface. Depending on properties such as aerosol number density, particle radius, or refractive index, the impact of the aerosols can provide positive or negative radiative feedbacks on the dynamics of the atmosphere. Previous studies have revealed large temporal and spatial variability in the aerosol optical properties, emphasizing the necessity for continuous monitoring of these properties throughout the day and at multiple locations. To address these measurements, the Radiation and Dust Sensor (RDS) [1] is part of the Mars Environmental Dynamics Analyzer (MEDA) [2] payload onboard of the Mars 2020 rover Perseverance. RDS instrument compromises two sets of 8 photodiodes (RDS-DP) and a camera (RDS-SkyCam). One set of photodiodes is pointed upward, with each one covering a different wavelength range between 190-1200 nm. The other set is pointed sideways, 20 degrees above the horizon, and they are spaced 45 degrees apart in azimuth to sample all directions at a single wavelength. The analysis of these observations with a radiative transfer model [3] (Fig. 1) allow us to fit aerosol parameters such as the aerosol opacity at different wavelengths or the aerosol particle radius. In this work we will discuss some preliminary results for the first 100 sols of Mars 2020 mission.Ítem Acceso Abierto Front-End Electronic for Miniaturized LIDAR Signal Conditioning(Europlanet, 2024-07-03) Andrés Velasco, Santiago; Rivas Abalo, Joaquín; Arruego, Ignacio; Vázquez Yañez, G. A.; Montalvo Chacón, S.; Muñoz García, E.; Martín Ortega, A.; Jiménez Martín, Juan José; García Menéndez, Elisa; Moya Señas, AlbertoThe Miniaturized LIDAR for MARS Atmospheric Research (MiLi) project falls within the European Union funding program called Horizon Europe [1]. Within this general framework, the project being presented is classified under cluster 4 - Digital, Industry, and Space [2]. The investment in the different projects within this fourth point pursues the idea of global leadership of the European industry in key areas, through the development of competitive and trustworthy technologies. This sets the foundation for a competitive, digital, sustainable, and circular industry that allows for progress and innovation in global societal challenges.Ítem Acceso Abierto Generic Entry Probe Program (GEPP) – an international initiative promoting the development of European descent modules dedicated to the in situ(EGU General Assembly, 2024-05-13) Mousis, O.; Ambrosi, R.; André, N.; Andrews, J.; Apéstigue, Víctor; Atkinson, D.; Arruego, Ignacio; Blanc, M.; Boithias, H.; Bolton, S.; Bousquet, P.; Canup, R.; Cavalié, T.; Freeman, A.; Faye, F.; Ferri, F.; Glein, C.; Guelhan, A.; Hartogh, P.; Loehle, S.; Hue, V.; Lebreton, J. P.; Lemaistre, S.; Mooij, E.; Pichon, T.; Pinaud, G.; Steuer, D.; Toledo, D.; Rauer, H.; Vorburger, A.; Wurz, P.The international consortium GEPP has been set to conceptualize probe designs with appropriate payloads that would remain within the typical budget allocated for ESA M-class missions (currently 500 M€). The aims of the consortium are i) to conceptualize a line of generic planetary entry probes that could be targeted to the giant planets with very few modifications, ii) to make the international science community, ESA and its member states, conscious that there is an opportunity to supply a series of entry probes as part of future international collaborations, for example as part of the future NASA flagship mission towards Uranus (Uranus Orbiter Probe) or to any future NASA-led mission to the outer planets for an affordable budget, and iii) to demonstrate that an M-class budget could even fund several entry probes with well-prioritized science objectives. The model payload capabilities of each concept will be defined according to a carefully-designed science traceability matrix. Two extreme concepts shall be investigated by the GEPP Consortium, namely a highly capable parachute-descent probe including a typical payload of 30 kg of scientific instruments down to 10 bars, and a smaller parachute-descent probe designed to address top priority science objectives with selected key measurements that would address the ESA Cosmic Vision 2050 science objectives. This presentation will detail the scientific objectives for each entry probe design, as well as the content, organization and planning of the study, which is assumed to be completed by the end of 2025.Ítem Acceso Abierto Lunar In-situ Navigation and Communication Node - LUNINA(Europlanet, 2024-07-03) Haukka, H.; Kestilä, Antti; Arruego, Ignacio; Harri, Ari-Matti; Genzer, María; Apéstigue, Víctor; Hieta, M.; Camañes, Carmen; Ortega, Cristina; Kivekäs. Jarmo; Koskimaa, PetriLUNINA is an in-situ navigation and communication node. Proposed LUNINA platform is designed to be a compact, independent, cost effective, robust, and location independent navigation beacon and communication relay on the Moon that can operate 24/7.Ítem Acceso Abierto Mars environmental networks through the MarsConnect microprobes(Europlanet, 2025-01-23) Arruego, Ignacio; Apéstigue, Víctor; Bastide, L.; Azcue, J.; Gonzalo Melchor, Alejandro; Martínez Oter, J.; Caballero, N.; Liaño, G.; Torres, J.; González Guerrero, M.; Serrano, F.; De Mingo, J. R.; Rivas, J.; Andrés Santiuste, N.; Carrasco, I.; Fernández, M.; Reina, M.; Ruiz Carrasco, J. R.; Poyatos Martínez, David; Scaccabarozzi, D.; Frövel, M.; De la Torre, M. A.; Martín, S.; Pedraza, R.In the last 15 years the Payloads Department of INTA has developed a variety of compact sensors for different Mars exploration missions. This includes a magnetometer (72 g), a dust sensor (35 g; with UC3M, Spain) and a radiometer (114 g) for the MetNet penetrator [1]; a radiometer (25 g optical head, 56 g processor) for DREAMS (Schiaparelli) [2], [3]; a radiometer plus camera (1 kg) for MEDA on Perseverance [4], [5]; a 110 g dust sensor (with UC3M, Spain) [6] and a radiometer plus spectrometer (180 g) for the METEO package [7] on Kazachock lander (ExoMars’22) and a 0.5 kg nephelometer (with INAF and Politecnico di Milano, Italy) [8] for the Dust Complex on the same lander. Equally miniaturized sensors exist for the measurement of the most relevant environmental variables, such as radiative balance, air temperature, wind, humidity, pressure, dust saltation, electric field, etc. with enough flight heritage (or technology readiness level) on the same sensors’ suites on Perseverance and ExoMars, as well as Insight or Curiosity before [9]. In summary, a large portfolio of miniature sensors for environmental research is available at present. However, a qualitative leap on (in-situ) Mars climate science will only happen through the deployment of networks of environmental stations throughout large areas of the planet. Given the relevance of these measurement not only from a scientific point of view but also because of their importance for future human missions to Mars, this is an objective considered in several Mars exploration roadmaps such as ESA’s Terrae Novae 2030+ [10]. With this aim, we propose a microprobe named MarsConnect. It consists of a 10-12 kg probe with a rigid, deployable aeroshell/TPS and a 5-6 kg impactor/penetrator carrying up to 1 kg of environmental sensors. Many of these probes could be launched to Mars with a single carrier, to deploy meteorological networks. This works inherits different concepts from previous similar proposals, very specially MetNet and MiniPINS [11], but simplifying even more the EDL concept and reducing the mass, at the expense of an increased impact speed. The probe’s aeroshell is divided into a backshell and two halves of a frontshield that are opened in the low supersonic regime to drop the penetrator. This one is equipped with a drag-skirt that provides some braking and increases stability. The expected impact speed, highly dependent on the atmospheric density profile, entry conditions and landing altitude, ranges from less than 100 to 140 m/s. The whole system is designed to be compatible with a wide range of scenarios and landing sites and is sized to endure more than one Martian year operating on the planet’s surface.Ítem Acceso Abierto Microphysical modeling of methane ice clouds in the atmospheres of the Ice Giants(Europlanet, 2024-07-03) Toledo, D.; Rannou, P.; Irwin, Patrick Gerard Joseph; De Batz de Trenquelléon, Bruno; Apéstigue, Víctor; Roman, Michael; Arruego, Ignacio; Yela González, MargaritaVoyager 2 radio occultation measurements of Uranus and Neptune revealed a layer approximately 2-4 km thick near 1.2 and 1.6 bars, respectively, wherein the atmospheric refractivity exhibited a slope variation (1, 2). These findings were interpreted as indicating a region where methane gas was undergoing condensation, forming an ice cloud centered around this pressure level. While the formation of this putative cloud would explain the observed decrease in methane abundance with height above 1.2 and 1.6 bars, or the banded structure of Uranus through latitudinal variations in the opacity of this cloud, several recent works and observations do not provide direct evidence in favor of this cloud (3): (i) radiative transfer models show an enhancement in the scattering opacity at pressures near 4-6 bars, more consistent with the presence of H2S ice (4, 5); (ii) observations from ground-based telescopes (or observations from telescopes in orbit around the Earth) of methane clouds indicate cloud tops near 0.4 bars in both planets (6), approximately a scale height above the base of the putative methane cloud.Ítem Acceso Abierto The UMR: Uranus Multi-Experiment Radiometer for Haze and Clouds Characterization(Europlanet, 2024-07-03) Apéstigue, Víctor; Toledo, D.; Arruego, Ignacio; Irwin, P.; Rannou, P.; Gonzalo Melchor, Alejandro; Martínez Oter, J.; Ceballos Cáceres, J.; Azcue, J.; Jiménez Martín, Juan José; De Mingo, J. R.; Serrano, F.; Nuñez, J.; Andrés, S.; Torres Redondo, J.; Martín Ortega, A.; Yela González, Margarita; Sorribas, M.; Sebastián, E.; Vázquez García de la Vega, D.; Espejo, S.; Ragel, A.The present understanding of Uranus and Neptune has been derived primarily from terrestrial observations and observations conducted using space telescopes. Furthermore, a brief flyby conducted by the Voyager 2 spacecraft nearly three decades ago has contributed to our knowledge of these celestial bodies. Recently, the Decadal Survey [1] has identified a mission to Uranus as a high-priority objective for NASA's space exploration program and its ongoing missions to Mars and Europa. The main mission study [2] establishes the scientific priorities for an orbiter, including analyzing the planet's bulk composition and internal structure, magnetic field, atmosphere circulation, rings, and satellite system. On the other hand, the mission includes a descent probe, whose primary mission is obtaining data on the atmospheric noble gas abundances, noble gas isotope ratios, and thermal structure using a mass spectrometer and a meteorological package. Investigation of the vertically distributed aerosols (hazes and clouds) and their microphysical and scattering properties is required to comprehend the thermal structure and dynamics of Uranus' atmosphere. These aerosols play a crucial role in the absorption and reflection of solar radiation, which directly influences the planet’s energy balance. In this work, we present a lightweight radiometer instrument [3] to be included in the descent probe for studying the aerosols in the first km of the Uranus’ atmosphere. The UMR, the Uranus Multi-experiment Radiometer, takes its heritage from previous missions for Mars exploration [4-6], where its technology, including mixed-signal ASICs radiation hardened by design [7-8], has demonstrated its endurance for extreme environments of operation, using limited resources in terms of power consumption, mass and volume footprints, and data budget. These characteristics make this instrument a valuable probe’s payload for studying Uranus’ atmosphere with a high scientific return. In this contribution, we will present the actual design of the instrument and the future perspective before a possible announcement of opportunity.Ítem Acceso Abierto Turbulence statistics of terrestrial Mars-analog and Martian dust devils(EGU General Assembly, 2025-01-16) Karatekin, Özgür; Apéstigue, Víctor; Toledo, D.; Arruego, Ignacio; Franchi, Fulvio; Martínez, Germán M.; Berk Senel, CemConvective instabilities in the lowermost part of the atmosphere, so called the planetary boundary layer, can lead to the formation of convective vortices and form dust devils both on Earth and Mars. We performed mesoscale simulations for a Mars-analog terrestrial site, Makgadikgadi Pan - Botswana [1,2], where a state-of-the art field campaign was conducted to investigate the terrestrial dust devils, and the InSight landing site [3] using WRF/MarsWRF models [4,5]. We then combined our atmospheric modeling with in-situ observations of wind and pressure to perform a comparative boundary-layer meteorology study. We focused on the length and time of scales of turbulence and investigated the turbulent spectrum.Ítem Acceso Abierto Vortices and Dust Devils on Jezero Crater, Mars: inner thermal structure and dependence on surface properties(EGU General Assembly, 2024-05-16) Hueso, R.; Munguira, A.; Newman, C. E.; Martínez, Germán M.; Sánchez Lavega, Agustín; Del Río Gaztelurrutia, T.; Toledo, D.; Apéstigue, Víctor; Arruego, Ignacio; Pla García, J.; Lemmon, M. T.; Lorenz, Ralph; Vicente Retortillo, Álvaro; Navarro López, Sara; Stott, Alexander; Murdoch, N.; Gillier, M.; De la Torre Juárez, M.; Rodríguez Manfredi, J. A.
