碩士 / 國立成功大學 / 航空太空工程學系碩博士班 / 97 / Recreation business in aviation has grown dramatically in recently year. Compare to the navigation instrument in mechanical architecture, precision electronics technology makes modern aviation instruments and equipments much tinier, more affordable and more applicable in different situation. Present Micro-Electro-Mechanical Sensor (MEMS) technology has drastically improving sensor size, weight, price and power consumption for high accuracy, high reliability and high stability as another option for navigation purpose. One of critical problem in using MEMS sensors is that the performance is poor when compare to other navigation sensors such as ring laser or fibre-optic gyros. Apply MEMS sensor in vehicle positioning directly will conduct intolerable result. For acceptable application purpose, augment with other position technologies such as GPS in order to limit the integration error must be done when choose MEMS sensors.This thesis focuses on implementation of a GPS/INS integrated system which includes calibration and testing each component in the architecture such as accelerometer, gyro, pitot tube and electric compass.
| Identifer | oai:union.ndltd.org:TW/097NCKU5295105 |
| Date | January 2009 |
| Creators | Chang-wen Hung, 洪長文 |
| Contributors | Chin-E Lin, 林清一 |
| Source Sets | National Digital Library of Theses and Dissertations in Taiwan |
| Language | en_US |
| Detected Language | English |
| Type | 學位論文 ; thesis |
| Format | 86 |
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