Modeling of Cantilever Based Power Harvester as an Innovative Power Source for RFID Tag

Author(s):  
Suresh S. Balpande ◽  
Sudhir B. Lande ◽  
Umesh Akare ◽  
Laxman Thakre
2014 ◽  
Vol 8 (1) ◽  
pp. 111-117
Author(s):  
Zhang Xiangdong ◽  
Li Changming ◽  
Gao Xiaoqiu ◽  
Li Lijie

A new design about the integration of temperature sensor and RFID tag is provided. This is a dual-tag design, in which the temperature element is connected to one of the RFID tag antennas to form a parallel structure. In this design, some of the functions of the sensor are transferred to the RFID reader so that some components of the sensor can be cut, reducing the production costs of existing design. By defining the signal strength of the first tag as a reference value, the problem of setting a standard is solved in the temperature detection process. RF module can be used to make the energy transformation without requiring the entire design to have an external continuous power source to provide energy. In addition, experimental data proves the feasibility of this design.


Author(s):  
Byeonggwi Mun ◽  
◽  
Changyong Rhee ◽  
Jae-Sik Kim ◽  
Junghoon Cha ◽  
...  
Keyword(s):  
Rf Power ◽  
Rfid Tag ◽  

2007 ◽  
Vol 55 (6) ◽  
pp. 1089-1097 ◽  
Author(s):  
Amin Shameli ◽  
Aminghasem Safarian ◽  
Ahmadreza Rofougaran ◽  
Maryam Rofougaran ◽  
Franco De Flaviis

1984 ◽  
Vol 75 ◽  
pp. 743-759 ◽  
Author(s):  
Kerry T. Nock

ABSTRACTA mission to rendezvous with the rings of Saturn is studied with regard to science rationale and instrumentation and engineering feasibility and design. Future detailedin situexploration of the rings of Saturn will require spacecraft systems with enormous propulsive capability. NASA is currently studying the critical technologies for just such a system, called Nuclear Electric Propulsion (NEP). Electric propulsion is the only technology which can effectively provide the required total impulse for this demanding mission. Furthermore, the power source must be nuclear because the solar energy reaching Saturn is only 1% of that at the Earth. An important aspect of this mission is the ability of the low thrust propulsion system to continuously boost the spacecraft above the ring plane as it spirals in toward Saturn, thus enabling scientific measurements of ring particles from only a few kilometers.


2015 ◽  
Vol 6 (4) ◽  
pp. 171-184
Author(s):  
Liangbo Xie ◽  
Jiaxin Liu ◽  
Yao Wang ◽  
Chuan Yin ◽  
Guangjun Wen

1993 ◽  
Vol 113 (6) ◽  
pp. 753-759 ◽  
Author(s):  
Kuniho Tanaka ◽  
Etsuo Sakoguchi ◽  
Eiji Yamada

2010 ◽  
Vol E93-C (6) ◽  
pp. 785-795
Author(s):  
Sung-Jin KIM ◽  
Minchang CHO ◽  
SeongHwan CHO
Keyword(s):  
Rfid Tag ◽  

Author(s):  
Z.G. Wen ◽  
F.D. Wang ◽  
D.Y. Zhao ◽  
Y.B. Wang
Keyword(s):  
Rfid Tag ◽  

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