کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1825865 1526467 2010 5 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Determination of spacecraft attitude and source position using non-aligned detectors in spin-stabilized satellites
موضوعات مرتبط
مهندسی و علوم پایه فیزیک و نجوم ابزار دقیق
پیش نمایش صفحه اول مقاله
Determination of spacecraft attitude and source position using non-aligned detectors in spin-stabilized satellites
چکیده انگلیسی
Conversely, it is shown how the attitude of a spin-axis stabilized satellite as well as the unknown position of a celestial source of high-energy photons may be determined using a detector whose view-axis is intentionally kept inclined and is known accurately beforehand. The case of three-axes stabilized satellites is also discussed.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Nuclear Instruments and Methods in Physics Research Section A: Accelerators, Spectrometers, Detectors and Associated Equipment - Volume 621, Issues 1–3, 1–21 September 2010, Pages 534-538
نویسندگان
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