Persona: González Fernández, Luis Miguel
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Instituto Nacional de Técnica Aeroespacial
El Instituto Nacional de Técnica Aeroespacial es el Organismo Público de Investigación (OPI) dependiente del Ministerio de Defensa. Además de realizar actividades de investigación científica y de desarrollo de sistemas y prototipos en su ámbito de conocimiento, presta servicios tecnológicos a empresas, universidades e instituciones.
El INTA está especializado en la investigación y el desarrollo tecnológico, de carácter dual, en los ámbitos de la Aeronáutica, Espacio, Hidrodinámica, Seguridad y Defensa.
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González Fernández
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Luis Miguel
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Publicación Acceso Abierto Feasibility Design of MiLi, a Miniaturized Lidar for Mars Observation(IEEE Xplore, 2024-06-04) Scaccabarozzi, Diego; Potemkin, Kirill; Saggin, Bortolino; Vieira, Elimar; Giovanni Corti, Marco; Martina, Chiara; Appiani, Andrea; Martín-Ortega, Alberto; Arruego, Ignacio; Jiménez Martín, Juan José; González Fernández, Luis Miguel; Sanz Palomino, Miguel; Garranzo, Daniel; García-Moreno, Andrea; Fernandez Rodriguez, Marianela; Muñoz Rebate, Nacho; Braukhane, Andy; Quantius, DominikThis work describes the feasibility design of MiLi, a miniaturized lidar under development to operate on Mars. Atmospheric lidars could be employed to study atmospheric dust and ice-based clouds, but typically those types of instruments exhibit considerable mass and are characterized by high power consumption, so they cannot be easily retrofitted aboard landers. The MiLi project, funded by the European Union, aims to develop a compact, lightweight lidar for detailed atmospheric analysis of the Red Planet. The development of this instrument, which seeks to overcome the typical limitations of lidars, may increase the availability of this type of remote sensing technology in the context of planetary missions and wants to deliver precise characterization of Martian atmospheric dust and ice-based clouds. The feasibility study encompasses the design requirements, material selection, and evaluation of different design configurations to ensure the instrument's performance and survival in extreme conditions, posing the basis for the development of the instrument's mechanical architecture. Overall design procedure was based on the trade-off between the mass budget and the instrument performances. Assessment of the mechanical resistance was performed by using quasi-static and modal numerical analyses.
