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  Control of Self-Propelled Microjets Inside a Microchannel With Time-Varying Flow Rates

Magdanz, V., Sanchez, S., Schmidt, O. G., Khalil, I. S. M., & Misra, S. (2014). Control of Self-Propelled Microjets Inside a Microchannel With Time-Varying Flow Rates. IEEE Transactions on Robotics and Automation, 49-58. doi:10.1109/TRO.2013.2283929.

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 Creators:
Magdanz, V.1, Author
Sanchez, S.1, 2, Author           
Schmidt, O. G.1, 3, Author
Khalil, I. S. M4, Author
Misra, S.5, Author
Affiliations:
1Institute for Integrative Nanosciences, Leibniz Institute for Solid State and Materials Research Dresden, 01069 Dresden, Germany, ou_persistent22              
2Dept. Theory of Inhomogeneous Condensed Matter, Max Planck Institute for Intelligent Systems, Max Planck Society, ou_1497643              
3Materials Systems for Nanoelectronics, TU Chemnitz, TU Chemnitz, Germany, ou_persistent22              
4German University in Cairo, , New Cairo City 13411, Egypt, ou_persistent22              
5MIRA–Institute for Biomedical Technology and Technical Medicine, , University of Twente, 7500 AE Enschede, The Netherlands, ou_persistent22              

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Free keywords: Abt. Dietrich; Forschungsgruppe Sanchez; smart nano-bio devices;
 Abstract: We demonstrate the closed-loop motion control of self-propelled microjets inside a fluidic microchannel. The motion control of the microjets is achieved in hydrogen peroxide solution with time-varying flow rates, under the influence of the controlled magnetic fields and the self-propulsion force. Magnetic dipole mo- ment of the microjets is characterized using the U-turn and the rotating field techniques. The characterized magnetic dipole mo- ment has an average of 1.4 × 10 − 13 A.m 2 at magnetic field, linear velocity, and boundary frequency of 2 mT, 100 μ m/s, and 25 rad/s, respectively. We implement a closed-loop control system that is based on the characterized magnetic dipole moment of the mi- crojets. This closed-loop control system positions the microjets by directing the magnetic field lines toward the reference position. Experiments are done using a magnetic system and a fluidic mi- crochannel with a width of 500 μ m. In the absence of a fluid flow, our control system positions the microjets at an average velocity and within an average region-of-convergence (ROC) of 119 μ m/s and 390 μ m, respectively. As a representative case, we observe that our control system positions the microjets at an average velocity and within an average ROC of 90 μ m/s and 600 μ m and 120 μ m/s and 600 μ m when a flow rate of 2.5 μ l/min is applied against and along the direction of the microjets, respectively. Furthermore, the average velocity and ROC are determined throughout the flow range (0 to 7.5 μ l/min) to characterize the motion of the microjets inside the microchannel

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Language(s): eng - English
 Dates: 2014
 Publication Status: Issued
 Pages: -
 Publishing info: -
 Table of Contents: -
 Rev. Type: Peer
 Identifiers: DOI: 10.1109/TRO.2013.2283929
 Degree: -

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Title: IEEE Transactions on Robotics and Automation
Source Genre: Journal
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Publ. Info: New York, NY : IEEE
Pages: - Volume / Issue: - Sequence Number: - Start / End Page: 49 - 58 Identifier: ISSN: 1042-296X
CoNE: https://pure.mpg.de/cone/journals/resource/111099121186002