Development of a radiation based heat model for satellite attitude determination

Abstract : This paper is focused on the development and verification of a heat attitude model (HAM) for satellite attitude determination. Within this context, the Sun and the Earth are considered as the main external sources of radiation that could effect the satellite surface temperature changes. Assuming that the satellite orbital position (navigational data) is known, the proposed HAM provides the satellite surface temperature with acceptable accuracy and also relates the net heat flux (NHF) of three orthogonal satellite surfaces to its attitude via the inertial to satellite transformation matrix. The proposed HAM simulation results are verified through comparison with commercial thermal analysis tools. The proposed HAM has been successfully utilized in some researches for attitude estimation, and further studies for practical implementations are still ongoing.
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Aerospace Science and Technology, Elsevier, 2018, 82-83, pp.479 - 486. 〈10.1016/j.ast.2018.09.031〉
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https://hal.inria.fr/hal-01929229
Contributeur : Hassen Fourati <>
Soumis le : mercredi 21 novembre 2018 - 09:46:18
Dernière modification le : jeudi 13 décembre 2018 - 21:54:49

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Amir Labibian, Seid Pourtakdoust, Alireza Alikhani, Hassen Fourati. Development of a radiation based heat model for satellite attitude determination. Aerospace Science and Technology, Elsevier, 2018, 82-83, pp.479 - 486. 〈10.1016/j.ast.2018.09.031〉. 〈hal-01929229〉

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