کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1717677 1520081 2016 7 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Flexible platform based micro-satellite design method
ترجمه فارسی عنوان
روش طراحی میکروماهواره مبتنی بر پلت فرم انعطاف پذیر
کلمات کلیدی
طراحی ماهواره ؛ پلت فرم انعطاف پذیر؛ نرم افزار مبتنی بر کامپوننت؛ میکروماهواره
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
چکیده انگلیسی

This article proposes a flexible platform based satellite design methodology to achieve the aim of “Faster, Better and Cheaper” in a micro-satellite development process. The micro-satellite platform is divided into components-based software modules and hardware modules that comprise reconfigurable module, universal module and custom-built system in the proposed methodology. As a result, the micro-satellite platform possesses the flexible ability of rapid assembly/replacing according to diverse mission requirements. Application of hardware Plug and Play technology enables the universal module to rapidly connect to the satellite platform. Based on the software bus, the components-based software technique enhances the reuse percentage of the on-board software code, and improves the efficiency of the on-board software R&D. The single-axis air-bearing test bed is constructed based on proposed micro-satellite flexible platform design method using RS232 flywheel and RS422 fiber optic gyro (FOG), which illustrates the efficiency of the developed flexible design methodology.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 53, June 2016, Pages 162–168
نویسندگان
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