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9 de enero de 2023
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Alternative analytic method for computing mean observation time in space-telescopes with spin-precession attitude motion

Publicado en:Advances In Aircraft And Spacecraft Science. 9 (5): 449-462 - 2022-09-01 9(5), DOI: 10.12989/aas.2022.9.5.449

Autores: Bermejo-Ballesteros J; Cubas J; Casas F; Martínez-González E

Afiliaciones

CSIC-UC - Instituto de Física de Cantabria (IFCA) - Autor o Coautor
Inst Fis Cantabria CSIC UC, Avda Castros S-N, E-39005 Santander, Spain - Autor o Coautor
Instituto Universitario de Microgravedad Ignacio Da Riva - Autor o Coautor
Univ Politecn Madrid, Inst Univ Ignacio Da Riva IDR UPM, Plaza Cardenal Cisneros 3, E-28040 Madrid, Spain - Autor o Coautor

Resumen

Space-telescopes placed in the Sun-Earth second Lagrange point (L2) observe the sky following a scan strategy that is usually based on a spin-precession motion. Knowing which regions of the sky will be more observed by the instrument is important for the science operations and the instrument calibration. Computing sky observation parameters numerically (discretizing time and the sky) can consume large amounts of time and computational resources, especially when high resolution is required. This problem becomes more critical if quantities are evaluated at detector level instead of considering the instrument entire Field of View (FoV). In previous studies, the authors have derived analytic solutions for quantities that characterize the observation of each point in the sky in terms of observation time according to the scan strategy parameters and the instrument FoV. Analytic solutions allow to obtain results faster than using numerical methods as well as capture detailed characteristics which can be overseen due to discretization limitations. The original approach is based on the analytic expression of the instrument trace over the sky. Such equations are implicit and thus requires the use of numeric solvers to compute the quantities. In this work, a new and simpler approach for computing one of such quantities (mean observation time) is presented. The quantity is first computed for pure spin motion and then the effect of the spin axis precession is incorporated under the assumption that the precession motion is slow compared to the spin motion. In this sense, this new approach further simplifies the analytic approach, sparing the use of numeric solvers, which reduces the complexity of the implementation and the computing time.

Palabras clave

scan strategyvisibilityAccess timeScan strategyVisibility

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Impacto bibliométrico. Análisis de la aportación y canal de difusión

El trabajo ha sido publicado en la revista Advances In Aircraft And Spacecraft Science, Q3 Agencia Scopus (SJR), su enfoque regional y su especialización en Aerospace Engineering, le otorgan un reconocimiento lo suficientemente significativo en un nicho concreto del conocimiento científico a nivel internacional.

Análisis de liderazgo de los autores institucionales

Existe un liderazgo significativo ya que algunos de los autores pertenecientes a la institución aparecen como primer o último firmante, se puede apreciar en el detalle: Primer Autor (BERMEJO BALLESTEROS, JUAN) .

el autor responsable de establecer las labores de correspondencia ha sido BERMEJO BALLESTEROS, JUAN.