Attitude Determination Using a MEMS-Based Flight Information Measurement Unit
Obtaining precise attitude information is essential for aircraft navigation and control. This paper presents the results of the attitude determination using an in-house designed low-cost MEMS-based flight information measurement unit. This study proposes a quaternion-based extended Kalman filter to...
Main Authors: | , , , |
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Format: | Article |
Language: | English |
Published: |
MDPI AG
2011-12-01
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Series: | Sensors |
Subjects: | |
Online Access: | http://www.mdpi.com/1424-8220/12/1/1/ |