Design of Modular Power Management and Attitude Control Subsystems for a Microsatellite
المؤلفون المشاركون
Ali, Haider
Ali, Anwar
Mughal, M. Rizwan
Praks, Jaan
Khan, Shoaib Ahmed
Khan, M. Usman
المصدر
International Journal of Aerospace Engineering
العدد
المجلد 2018، العدد 2018 (31 ديسمبر/كانون الأول 2018)، ص ص. 1-13، 13ص.
الناشر
Hindawi Publishing Corporation
تاريخ النشر
2018-12-17
دولة النشر
مصر
عدد الصفحات
13
الملخص EN
The Electric Power System (EPS) and attitude control system (ACS) are the essential components of any satellite.
EPS and ACS efficiency and compactness are substantial for the proper operation and performance of the satellite’s entire mission life.
So, realizing the significance of EPS and ACS subsystems for any satellite, they have been assimilated and developed in modular forms focusing on efficiency and compactness.
The EPS is comprised of three modules called the solar panel module (SPM), power conditioning module (PCM), and power distribution module (PDM) while the ACS has an embedded magnetorquer coil.
For compactness and miniaturization purposes, the magnetorquer coil is embedded inside the SPM.
The components used are commercial off-the-shelf (COTS) components emphasizing on their power efficiency, small dimensions, and weight.
Latch-up protection systems have been designed and analyzed for CMOS-based COTS components, in order to make them suitable for space radioactive environment.
The main design features are modularity, redundancy, power efficiency, and to avoid single component failure.
The modular development of the EPS and ACS helps to reuse them for future missions, and as a result, the overall budget, development, and testing time and cost are reduced.
A specific satellite mission can be achieved by reassembling the required subsystems.
نمط استشهاد جمعية علماء النفس الأمريكية (APA)
Ali, Anwar& Khan, Shoaib Ahmed& Khan, M. Usman& Ali, Haider& Mughal, M. Rizwan& Praks, Jaan. 2018. Design of Modular Power Management and Attitude Control Subsystems for a Microsatellite. International Journal of Aerospace Engineering،Vol. 2018, no. 2018, pp.1-13.
https://search.emarefa.net/detail/BIM-1166896
نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)
Ali, Anwar…[et al.]. Design of Modular Power Management and Attitude Control Subsystems for a Microsatellite. International Journal of Aerospace Engineering No. 2018 (2018), pp.1-13.
https://search.emarefa.net/detail/BIM-1166896
نمط استشهاد الجمعية الطبية الأمريكية (AMA)
Ali, Anwar& Khan, Shoaib Ahmed& Khan, M. Usman& Ali, Haider& Mughal, M. Rizwan& Praks, Jaan. Design of Modular Power Management and Attitude Control Subsystems for a Microsatellite. International Journal of Aerospace Engineering. 2018. Vol. 2018, no. 2018, pp.1-13.
https://search.emarefa.net/detail/BIM-1166896
نوع البيانات
مقالات
لغة النص
الإنجليزية
الملاحظات
Includes bibliographical references
رقم السجل
BIM-1166896
قاعدة معامل التأثير والاستشهادات المرجعية العربي "ارسيف Arcif"
أضخم قاعدة بيانات عربية للاستشهادات المرجعية للمجلات العلمية المحكمة الصادرة في العالم العربي
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