کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
5486291 1399456 2017 39 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Solar sail equilibria with albedo radiation pressure in the circular restricted three-body problem
ترجمه فارسی عنوان
تعادل بادبان خورشیدی با فشار تابش آلبدو در حلقه دایره ای محدود شده است
کلمات کلیدی
بادبان خورشیدی، محدودیت مشکل سه بدن، آلبدو، لامبرتین، منطقه نفوذ،
موضوعات مرتبط
مهندسی و علوم پایه علوم زمین و سیارات علوم فضا و نجوم
چکیده انگلیسی
Solar Radiation Pressure (SRP) and albedo effects are investigated in the circular restricted three-body problem for a system consisting of the Sun, a reflective minor body and a solar sail. As an approximation of albedo radiation pressure (ARP), the minor body is treated as Lambertian with reflected flux scattered by the bidirectional reflectance distribution function. Incorporating ARP, which is a function of SRP, into the solar sail equations of motion renders additional artificial equilibrium points in a volume between the L1 and L2 points which is defined as the region of influence. Based on the model, characterization of the findings are provided that are theoretically applicable to any body with discernible albedo such as for instance Earth, Mars or an asteroid. Example results are presented for a Sun-Vesta system which show that the inclusion of ARP generates artificial equilibrium points requiring solar sail designs with very low mass-to-area ratio. The equilibrium points are found to be unstable in general but asymptotic stability may be enforced with sail attitude feedback control.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Advances in Space Research - Volume 59, Issue 4, 15 February 2017, Pages 1112-1127
نویسندگان
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