Chinese Space Science and Technology
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Li Wanlin (Beijing Institute of Spacecraft Systems Engineering)
Online:
Abstract: This paper presents the formula of the initial values of theorbital parameters—celestial longitude φ_0 of the sun,right ascension ofascending node Ω_0 and argument of perigee ω_0,used for calculating orbitalheat flux received by satellite.The accuracy of calculation of these para-meters has met the requirements of thermal analysis of a satellite.
Li Wanlin (Beijing Institute of Spacecraft Systems Engineering). CALCULATION OF ORBITAL PARAMETERS Ψ__0,Ω_0 AND ω_0 USED FOR CALCULATING SPACE HEAT FLUX[J]. Chinese Space Science and Technology.
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URL: https://journal26.magtechjournal.com/kjkxjs/EN/
https://journal26.magtechjournal.com/kjkxjs/EN/Y1993/V13/I06/58
