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A Micro-Machined Gyroscope for Rotating Aircraft
AbstractIn this paper we present recent work on the design, fabrication by silicon micromachining, and packaging of a new gyroscope for stabilizing the autopilot of rotating aircraft. It operates based on oscillation of the silicon pendulum between two torsion girders for detecting the Coriolis force. The oscillation of the pendulum is initiated by the rolling and deflecting motion of the rotating carrier. Therefore, the frequency and amplitude of the oscillation are proportional to the rolling frequency and deflecting angular rate of the rotating carrier, and are measured by the sensing electrodes. A modulated pulse with constant amplitude and unequal width is obtained by a linearizing process of the gyroscope output signal and used to control the deflection of the rotating aircraft. Experimental results show that the gyroscope has a resolution of 0.008 °/s and a bias of 56.18 °/h.
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MDPI and ACS Style
Yan, Q.; Zhang, F.; Zhang, W. A Micro-Machined Gyroscope for Rotating Aircraft. Sensors 2012, 12, 9823-9828.View more citation formats
Yan Q, Zhang F, Zhang W. A Micro-Machined Gyroscope for Rotating Aircraft. Sensors. 2012; 12(7):9823-9828.Chicago/Turabian Style
Yan, Qingwen; Zhang, Fuxue; Zhang, Wei. 2012. "A Micro-Machined Gyroscope for Rotating Aircraft." Sensors 12, no. 7: 9823-9828.