Analytical and simulation results of micro-ring resonator system using two eyes imaging model

Tanaram, C.; Phatharacorn, Prateep; Chiangga, Surasak; Yupapin, Preecha P.

doi:10.14419/ijsw.v3i2.4881

Cited by 3 publications

(1 citation statement)

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“…The WGM theory concern is given, the simulation results using the suitable ring device parameters related to the fabrication technology are also given. The mathematical model is used to explain the pattern formation of WGM for a single Panda ring resonator, which is shown in Figure , where the electric field output ( E wgm ) is given by

E_{WGM} (ρ, f) = \frac{4 π csch (k_{0 n} \frac{π a}{2})}{a^{2} J_{1}^{2} (k_{0 n} a)} [\frac{x_{1} \sqrt{κ_{1}}}{\sqrt{1 - 2 x_{1} y_{1} e^{- \frac{α}{2} L} \cos (k_{n} L) + e^{- α L} x_{1}^{2} y_{1}^{2}}}] \times \frac{(w A_{0}) \sqrt{k_{0} n_{0}}}{B^{\frac{1}{4}}} J_{0} (k_{0 n} ρ) true \int_{0}^{a} J_{0} true(k_{0 n} ρ true) true[ρ - true(\frac{A}{2 true(B + C ρ^{2} true)} + \frac{C}{4 B} true) ρ^{3} true] d ρ

where…”

Section: Theoretical Backgroundmentioning

confidence: 99%

Micropropulsion generation model and simulation by WGM acceleration within a Panda ring resonator system

Siriroj

Techidheera

Phatharacom

et al. 2016

Micro & Optical Tech Letters

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A microbeam accelerator is modeled and simulated using the analogy of whispering gallery mode (WGM) generated by light within a nonlinear microring resonator system, which is called a Panda ring structure and made by an InGaAsP/InP material. The WGM mode is generated after the suitable ring parameters and optical input introducing into the system, especially, the suitable two nonlinear side ring radii are employed. From which, the required multiple propulsion (acceleration) of WGM beams is achieved using the multiple vertical Panda ring layout (several layers). The accelerated WGM beams of the multiple ring circuits can be obtained by the coincident of the multiple Panda rings. The simulation result shows that the proposed ring resonator system can be potentially fabricated within the microscale range and used for a microthruster, in which the required driven force can be used to drive the spacecraft or satellite to the target destination, which is known as a thrust propellant. For example, the result of the propulsion of 2.619–66.81 μN can be obtained by a single device system, which means that the larger volume or area can be used to produce more propulsion output. For further application, the suitable input source such as the infrared light source can also be used to for the micro‐heat source, in which the large area of the device array may be useful for large area micro‐heat source usage. © 2016 Wiley Periodicals, Inc. Microwave Opt Technol Lett 59:377–380, 2017

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