Quaternion-Based Aircraft Attitude Estimation
<p> Aircraft attitude estimation requires fusing several sensors in order to recover both high and low frequency information in an observable manner. This thesis explores the fusion of gyroscope integration, gravity vector estimation, and magnetic field vector estimation using a complementary...
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| Language: | EN |
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University of California, San Diego
2016
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| Online Access: | http://pqdtopen.proquest.com/#viewpdf?dispub=10133153 |