کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
9506333 1631840 2005 11 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Optimization out-of-orbit plane changes using aeroassisted maneuvers
کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه ریاضیات ریاضیات کاربردی
پیش نمایش صفحه اول مقاله
Optimization out-of-orbit plane changes using aeroassisted maneuvers
چکیده انگلیسی
The problem of optimizing the fuel consumption needed for orbital maneuvers is investigated. The normal to the orbit components of the atmospheric drag and lift forces are obtained. The temporal variations in the inclination using Lagrange planetary equation are derived, then are integrated over one revolution. A numerical example is given. The velocity variations required to perform the propulsive maneuvers due to engines on board the satellite are calculated. The performance gain using aerodynamic forces combined with propulsive ones is achieved. The comparison between the totally propulsive maneuvers and partly propulsive with atmospheric maneuvers are illustrated and discussed.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Applied Mathematics and Computation - Volume 170, Issue 2, 15 November 2005, Pages 1303-1313
نویسندگان
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