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Design of Electronic Gyroscope

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dc.contributor.author Ahmed, Abuagla omer Al-Amin
dc.contributor.author Mohammed, Ahmed babeker talha
dc.contributor.author Salih, Alageba Alshazli Mohammed
dc.contributor.author Ahmed, Mohamed Hamza Abed almaged
dc.contributor.author bd-elwahaab, Taqwa
dc.date.accessioned 2016-02-06T08:57:36Z
dc.date.available 2016-02-06T08:57:36Z
dc.date.issued 2015-10-01
dc.identifier.citation Ahmed,Abuagla omer Al-Amin.Design of Electronic Gyroscope/Abuagla omer Al-Amin Ahmed...{etal} ; Osman imam.-khartoum :Sudan University of Sciences and Technology,College of Engineering,2015.-57p:ill;28cm.-Bachelors search en_US
dc.identifier.uri http://repository.sustech.edu/handle/123456789/12659
dc.description Bachelors search en_US
dc.description.abstract This thesis present a micro electromechanical system-inter digital transducer (MEMS-IDT) surface acoustic wave (SAW) gyroscope with an 80MHz central frequency on a 128° YX lithium-Nobelium tri-oxide(LiNbO3) wafer. The developed MEMS-IDT gyroscope is composed of a two-port SAW resonator, a dual delay line oscillator, and metallic dots. The SAW resonator provides a stable standing wave, and the vibrating metallic dot at an anti node of the standing wave induces the second SAW in the normal direction of its vibrating axis. The dual delay line oscillator detects the Carioles effect (gyro phenomena) by comparing the resonant frequencies between two oscillators through the interference effect. The coupling of k-wave MATLAB added tool box modeling was used to extract the optimal design parameters prior to simulation. In the electrical testing by the network analyzer, the simulated SAW resonator and delay lines showed low insertion loss and similar operation frequencies between a resonator and delay lines. When the device was rotated, the resonant frequency differences between two oscillators linearly varied owing to the Carioles force. The obtained sensitivity was approximately 119 1000 in the angular rate range of 0- . Satisfactory linearity and superior directivity were also observed in the test. en_US
dc.description.sponsorship Sudan University of Sciences and Technology en_US
dc.language.iso en en_US
dc.publisher Sudan University of Sciences and Technology en_US
dc.subject Electronic Gyroscope en_US
dc.subject Aeronautical Engineering en_US
dc.subject Design of Electronic Gyroscope en_US
dc.title Design of Electronic Gyroscope en_US
dc.type Thesis en_US


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