About Nano-JASMINE Satellite System and Project Status
نویسندگان
چکیده
منابع مشابه
Low Earth Orbit Nano Satellite Electrical Power System Design
The following text shows the requirements for LEO satellite’s EPS design, namely the initial mission assessment, the available power budget, the filtering components sizing, the finalized circuit design and the expected efficiency for optimal operation point. One early assessment was the reliability of the photovoltaic array system in terms of how the cells should be laid out: whether in parall...
متن کاملGain-scheduled EKF for Nano-satellite Attitude Determination System
Extended Kalman filter (EKF) has been widely used for attitude determination in various satellite missions. However, it 1 requires an extensive computational power which is not suitable for nano-satellite application. This paper proposes a gain-scheduled 2 EKF (GSEKF) to reduce the computational requirement in nano-satellite attitude determination process. The proposed GSEKF 3 eliminates the on...
متن کاملSocial Media and the Jasmine Revolution
2 1541-1672/11/$26.00 © 2011 IEEE IEEE INTELLIGENT SYSTEMS Published by the IEEE Computer Society Letters to the Editor: Send letters, including a reference to the article in question, to [email protected]. Letters will be edited for clarity and length. Articles: If you’re interested in submitting an article for publication, see our author guidelines at www.computer.org/ intelligent/author.ht...
متن کاملSCCC Turbo Equalizer/Decoder for X-band Nano Satellite High-Speed Downlink System
Nano satellite technologies have been recognized as potential candidates for new satellite applications. We have developed a X-band downlink system for nano satellite employing Consultative Committee for Space Data Systems (CCSDS) 131.2-B-1 signaling formats with a modulation symbol rate of 100 Msps. Since nano satellites with a mass of less than 50 kg have more constraints than typical large s...
متن کاملApplication of Multiple system on a chip technology systems in micro-nano satellite integrated electronic systems
This paper mainly describes the way that using (multiple chip module)MCM technology to optimize and improve design of small satellite's electronic system from application requirement view. Research on MCM based on Silicon wafer is carried out, combined with software and IC integration technology. Finally, the ultimate realization is Miniaturization, integration, standardization of the design of...
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ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
سال: 2010
ISSN: 1884-0485
DOI: 10.2322/tastj.8.tf_7