• JSTS:Journal of Semiconductor Technology and Science
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• 제7권2호
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• pp.110-119
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• 2007

A new two-dimensional analytical model for dual-material double-gate fully-depleted SOI MOSFET with Pearson-IV type Doping Distribution is presented. An investigation of electrical MOSFET parameters i.e. drain current, transconductance, channel resistance and device capacitance in DM DG FD SOI MOSFET is carried out with Pearson-IV type doping distribution as it is essential to establish proper profiles to get the optimum performance of the device. These parameters are categorically derived keeping view of potential at the center (${\phi}_c$) of the double gate SOI MOSFET as it is more sensitive than the potential at the surface (${\phi}_s$). The proposed structure is such that the work function of the gate material (both sides) near the source is higher than the one near the drain. This work demonstrates the benefits of high performance proposed structure over their single material gate counterparts. The results predicted by the model are compared with those obtained by 2D device simulator ATLAS to verify the accuracy of the proposed model.

• 대한의용생체공학회:의공학회지
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• 제24권1호
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• pp.31-36
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• 2003

본 논문에서는 일정한 충격하중을 제공하여 충격특성을 정량적으로 측정할 수 있는 시스템을 개발하고 당뇨화 안창의 소재에 대한 감쇠지수, 중앙주파수, 반발계수 등을 통하여 6종류의 당뇨화 소재와 3종류의 다밀도 당뇨화 안창의 충격특성을 측정하였다. Podian, Plastazote black, Plastazote white, Flexible PU foam, Podialene 200 blue, Podia flex 소재 중에서 감쇠지수와 반발계수는 Podian이 우수하였으며, Flexible PU foam 소재의 중앙주파수가 가장 작음을 알 수 있었다. 3종의 다밀도 안창인 AP 안창, OS 안창, PW 안창을 각각 세 부위로 나누어 안창의 종류와 부위별 충격특성을 비교한 결과 발뒤꿈치 부분이 충격완화 효과가 가장 우수함을 확인할 수 있었다. 반발계수와 중앙주파수에서는 OS 안창이 AP 안창보다 충격완화 효과가 우수함을 보였으나, 감쇠지수는 서로 유사한 견과를 보였다. PW 안창은 두 겹의 폴리우레탄이 전체에 분포되어 있으므로 부위별로 유사한 충격흡수정도를 나타내었다.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2003년도 한국우주과학회보 제12권2호
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• pp.63-63
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• 2003

There are many actuators and sensors used for attitude control system for KOMPSAT such as Reaction Wheel Assembly, Magnetic Torque Assembly, Dual Thruster Module, Solar array Drive, Three Axis Magnetometer, Conical Earth Sensor, Fine Sun Sensor Assembly, Coarse Sun Sensor Assembly, Gyro Reference Assembly and so on. For KOMPSA T satellite it has been considered using the Magnetic Torquer (MTQ) generating the magnetic dipole moment. In general, the magnetic dipole moment for satellite attitude control system is used for dumping out the excessive reaction wheel momentum so that the reaction wheel speed is not saturated. The objective of this study is to analyze the magnetic field characteristics generated by the Magnetic Torquer using the Maxwell 2D Field Simulator software. Currently, the developing model (DM) of the MTQ is being developed and manufactured at a company under the supervision of KARL MTQ is an electromagnet consisting of a ferromagnetic cylindrical core on which an excitation coil is wound. A current is passed through the coil to produce a dipole momentum in the ferromagnetic core. The configuration of the MTQ will be introduced in the presentation. The 2 dimensional model of the MTQ is drawn as axisymmetric models in RZ plane, and each corresponding material is assigned to the each MTQ object, the core, coil, and background. After the boundary conditions, current sources, and solution parameters are set up, the magnetic field intensities, directions, and other values specified by users can be calculated by using the finite element analysis. The theoretical magnetic field quantities obtained by the Maxwell 2D Simulator can be used for the basis of the development of the MTQ.