Development and Control of Micro-Ionic Thrusters for Centimeter-Scale Aerial Robots

dc.contributor.advisorFULLER, SAWYER B
dc.contributor.authorHari Prasad, Hari Krishna
dc.date.accessioned2020-08-14T03:32:41Z
dc.date.available2020-08-14T03:32:41Z
dc.date.issued2020-08-14
dc.date.submitted2020
dc.descriptionThesis (Master's)--University of Washington, 2020
dc.description.abstractAs we go smaller and smaller, we take inspiration from Biology to design our Engineered machines. Currently, most centimeter-scale aerial robots use complicated, failure-prone insect-inspired flapping-wing mechanisms to propel themselves. In Electrohydrodynamics (EHD), corona discharge generates a flow of ions in an electric field between two electrodes; the high-velocity ions transfer their kinetic energy to neutral air molecules through collisions, accelerating the gas and thus creating thrust. This mechanism produces thrust without the need for any moving parts, scales favorably with diminishing size, and is a sparsely explored propulsion mechanism. In this work, laser-based microfabrication of EHD-thruster is explored. Following this, high-voltage Pulse-Width-Modulation (PWM) (achieved using a high-voltage power MOSFET) is established as a means of modulating thrust with sufficient bandwidth to perform closed-loop control.
dc.embargo.termsOpen Access
dc.format.mimetypeapplication/pdf
dc.identifier.otherHariPrasad_washington_0250O_21534.pdf
dc.identifier.urihttp://hdl.handle.net/1773/46103
dc.language.isoen_US
dc.rightsCC BY
dc.subjectcorona discharge
dc.subjectelectrohydrodynamics
dc.subjectpulse width modulation
dc.subjectMechanical engineering
dc.subject.otherMechanical engineering
dc.titleDevelopment and Control of Micro-Ionic Thrusters for Centimeter-Scale Aerial Robots
dc.typeThesis

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