Attitude Determination Based On a MEMS Flight Information Measurement Unit: Application of Extended Kalman Filter
碩士 === 淡江大學 === 航空太空工程學系碩士班 === 98 === This thesis studies the attitude determination using a MEMs flight information measurement unit. A quaternion-base extended Kalman filter to integrate the traditional quaternion and gravitational methods for attitude determination algorithm is proposed in the...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2010
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| Online Access: | http://ndltd.ncl.edu.tw/handle/55156309209294841598 |