کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
5486806 1399484 2016 9 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Asteroid rotation control via a tethered solar sail
ترجمه فارسی عنوان
کنترل چرخش سیارک از طریق بادبان خورشیدی تنگ
موضوعات مرتبط
مهندسی و علوم پایه علوم زمین و سیارات علوم فضا و نجوم
چکیده انگلیسی
The rotation of asteroids causes difficulties in the exploration of asteroids or prevention of asteroids impact on the Earth. We propose to use a solar sail to control, i.e., slow down or stop the rotational motion of an asteroid. First, the dynamic model of a tethered solar sail in the rotating gravitational field of an asteroid is presented. An optimal control method is employed to determine the control law of the tethered solar sail. The optimal control problem is converted into a nonlinear programming problem with the Gauss pseudospectral method. Simulation results show that this method can effectively slow down or even stop the rotation of an asteroid. A solar sail of 105 m2 can stop the rotation of the asteroid Apophis in 1000 days.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Advances in Space Research - Volume 58, Issue 11, 1 December 2016, Pages 2304-2312
نویسندگان
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