Attitude Determination Using a MEMS-Based Flight Information Measurement Unit

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...

Full description

Bibliographic Details
Main Authors: Yu-Heng Lin, I.-Chiang Wang, Der-Ming Ma, Jaw-Kuen Shiau
Format: Article
Language:English
Published: MDPI AG 2011-12-01
Series:Sensors
Subjects:
attitude determination
quaternion
flight information measurement unit
extended Kalman filter
Online Access:http://www.mdpi.com/1424-8220/12/1/1/

Internet

http://www.mdpi.com/1424-8220/12/1/1/

Similar Items