bias potential potential 中文意思是什麼
bias potential potential
解釋
偏置電位-
In a ccp system, there is a discontiguous characteristic on tuned substrate self - bias. when the impedance between substrate and ground was made increasingly inductive, a large negative dc potential developed on the substrate
在ccp （ capacitivecouplingplasma ）中調諧基片偏壓具有不連續變化現象，當基片之間為漸增的感抗時，基片上會產生漸增的負偏壓。 -
The performance of modulators employing mqw is governed by the quantum confined stark effect. in order to simplify the analysis of mqw, we obtain an explicit formula concerning the correlations between the gaas / gaalas quantum well widths of finite potential barrier structure and those of infinite potential barrier structure under the condition that the ground state energies are equal at zero bias states. then the transfer matrix method is used to investigate the optical field distribution in the mqw waveguide based on five - step asymmetric coupled quantum well structure that is really used in the modulator
本論文首先根據量子限制stark效應，發展了等效寬度思想，提出了把單量子阱結構的有限深勢阱的分析轉化為無限深勢阱模型的顯式公式，從而大大簡化了電場下量子阱結構的分析；接著利用轉移矩陣，把周期性的量子阱結構簡化為三層結構，得到了實際採用的非對稱三阱結構量子阱的場分佈，並討論了量子阱結構的偏振特性。 -
Next, basing on discrete electric potential, plots the distributing figure of the electic potential and electic field, and analyzes relationship between the operational characteristics of static induction transistor and the structure parameter and bias voltage
其次依據求得的離散電位值，繪制相應的電位分布圖形和電場分布圖形。最後通過對圖形的分析，解析有機靜電感應三極體的工作特性與器件結構參數和所加偏壓的關系。 -
It is found that by applying a forward bias of about 6 volts in vacuum, s - type negative differencial resistance ( ndr ) phenomena were found in such structure, which is of potential application
並在實驗中首次發現在經過真空處理后的al n - zno p - si異質結中表現出了類似gainp algainp量子阱等結構的s型負阻（ ndr ）現象。 -
Through the analysis of the attitude dynamic equation, the potential energy function is derived. the relationships of attitude varieties are derived from energy function and angle momentum equation and thus the attitude control laws of bias momentum satellite are put forward
通過對衛星姿態動力學方程分析，得出衛星的勢函數，結合衛星的勢函數和角動量方程導出各姿態之間變化關系，提出利用地磁場實現偏置動量輪衛星姿態穩定的控制規律。
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