منابع مشابه
Development of a Responsive Small Spacecraft
The development of a small spacecraft bus is presented. The approach applied seeks to respond to the requirements of potential users as represented by a large data base of payload missions, while minimizing cost. The development results in a general purpose spacecraft design that is responsive to a wide range of mission requirements, and provides a clear definition of capabilities and interface...
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متن کاملSSC09-IV-2 System outline of small standard bus and ASNARO spacecraft
ASNARO (Advanced Satellite with New system ARchitecture for Observation) system outline including payload characteristics and bus architecture is presented in this paper. ASNARO, which is being developed by NEC and USEF under the contract with NEDO, is a LEO satellite for the earth observation by optical sensor in sub-meter class. The bus module of the ASNARO is highly adaptive for various miss...
متن کاملDevelopment and On‐Orbit Demonstration of Lithium‐ Ion Capacitor‐Based Power System for Small Spacecraft
Lithium‐ion capacitors (LICs) offer higher energy density and specific energy than do traditional electric double‐layer capacitors (EDLCs). In spacecraft power systems where traditional lithium‐ion batteries (LIBs) have been used with shallow depth of discharge (DoD) in order to achieve long‐cycle life, LICs would potentially be an alternative to secondary batteries. Firstly, this chapter prese...
متن کاملHierarchichal Current Control Design For Electromagnetic Aircraft Launching System
This paper describes an approach to hierarchichal modular control for an electromagnetic aircraft launching system for the aircraft carrier of the future. The purposes are to analyze the possibility of improving the control performance using efficient evaluation of switching conditions, and to explore the different options for the basic control design and the way in which these designs will be ...
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ژورنال
عنوان ژورنال: Izvestiâ vysših učebnyh zavedenij. Priborostroenie
سال: 2016
ISSN: 0021-3454
DOI: 10.17586/0021-3454-2016-59-6-482-488