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Assessment of new thermospheric mass density model using NRLMSISE-00 model, GRACE, Swarm-C, and APOD observations

Calabia, Andres, Tang, Geshi, and Jin, Shuanggen, 2019. Assessment of new thermospheric mass density model using NRLMSISE-00 model, GRACE, Swarm-C, and APOD observations. Journal of Atmospheric and Solar-Terrestrial Physics, 199:105207, doi:10.1016/j.jastp.2020.105207.

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BibTeX

@ARTICLE{2019JASTP.19905207C,
       author = {{Calabia}, Andres and {Tang}, Geshi and {Jin}, Shuanggen},
        title = "{Assessment of new thermospheric mass density model using NRLMSISE-00 model, GRACE, Swarm-C, and APOD observations}",
      journal = {Journal of Atmospheric and Solar-Terrestrial Physics},
     keywords = {Thermospheric mass density, GRACE, Swarm, APOD, NRLMSISE-00},
         year = 2019,
        month = mar,
       volume = {199},
          eid = {105207},
        pages = {105207},
     abstract = "{Thermospheric mass density estimates from in-situ observations along
        satellite orbits are difficult to validate due to their inherent
        spatiotemporal sparse nature, and difficulties related to drag-
        force modeling and estimation of actual mass density state.
        Current upper atmospheric models are unable to accurately
        represent the actual thermospheric variability, and in-situ
        observations are far to fulfill the minimum requirements in
        practical applications. In this manuscript, the new
        Thermospheric Mass Density Model (TMDM) is based on the fit of
        solar flux, annual, Local Solar Time (LST), and magnetospheric
        proxies into the Principal Component Analysis (PCA) of 13 years
        of accelerometer-based mass density estimates derived from the
        GRACE (Gravity Recovery and Climate Experiment) mission. We
        employ the NRLMSISE-00 model and estimates from APOD
        (Atmospheric density detection and Precise Orbit Determination),
        Swarm-C, and GRACE satellites, and assess the new model,
        including statistical analyses, and a Precise Orbit
        Determination (POD) scheme. We compare 2 years of APOD and
        Swarm-C estimates, and study the dynamic orbit propagation of
        the 3 missions under different mass density input schemes and
        different magnetospheric activity conditions. The results with
        TMDM show similar differences in the dynamically propagated
        orbits from NRLMSISE-00 and in-situ observations. The
        statistical analyses show that NRLMSISE-00 overestimates about
        20\%, and TMDM underestimates about 20\%, the in-situ
        observations.}",
          doi = {10.1016/j.jastp.2020.105207},
       adsurl = {https://ui.adsabs.harvard.edu/abs/2019JASTP.19905207C},
      adsnote = {Provided by the SAO/NASA Astrophysics Data System}
}

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