Variable and Fixed Step Integrations for Dynamic Orbit Determination of LEO Satellites
محل انتشار: هشتمین کنفرانس انجمن هوافضای ایران
سال انتشار: 1388
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 1,985
فایل این مقاله در 7 صفحه با فرمت PDF قابل دریافت می باشد
- صدور گواهی نمایه سازی
- من نویسنده این مقاله هستم
استخراج به نرم افزارهای پژوهشی:
شناسه ملی سند علمی:
AEROSPACE08_414
تاریخ نمایه سازی: 5 شهریور 1388
چکیده مقاله:
Multi-step integrators can be classified either as single or double integrators. The single integrators are designed for first-order differential equations whereas the double integrators solve second-order differential equations and calculate position of the satellite directly from its acceleration. When force model include drag effect, we also need satellite’s velocity. Therefore, single integrators are required. The most popular single integrators are Adams-Bashforth-Moulton and Shampine-Gordon which the former is a multi step fixed step-size technique and the latter is a multi step variable step-size technique. Our numerical results illustrate the Shampine-Gordon method is more stable than the Adams-Bashforth-Moulton method.
کلیدواژه ها:
Dynamic Orbit Determination-LEO Satellites-Multi Step Integrators-Shampine Gordon-Adams Bashforth Moulton
نویسندگان
Mohammad Ali Sharifi
Faculty of Engineering, University of Tehran, Iran
Meysam Mahooti
Faculty of Engineering, University of Tehran, Iran