Title :
Design of multi-sensor attitude determination systems
Author :
Gebre-egziabher, Demoz ; Hayward, Roger C. ; Powell, J. David
Author_Institution :
Dept. of Aerosp. Eng. & Mech., Minnesota Univ., Minneapolis, MN, USA
fDate :
4/1/2004 12:00:00 AM
Abstract :
The design of inexpensive multi-sensor attitude determination systems is discussed. The systems discussed fuse information from a triad of solid state rate gyros with an aiding system mechanized using GPS or magnetometers and accelerometers. Euler angle and quaternion-based sensor fusion algorithms are developed. Methods for gain scheduling and estimator pole placement are presented. Using simulation and flight test results, it is shown that quaternion-based algorithms simplify gain scheduling and improve transient response.
Keywords :
Global Positioning System; accelerometers; attitude control; attitude measurement; magnetometers; sensor fusion; Euler angle; GPS; accelerometers; estimator pole placement; gain scheduling; magnetometers; multisensor attitude determination systems; quaternion-based sensor fusion algorithm; solid state rate gyros; transient response; Accelerometers; Aerospace simulation; Fuses; Global Positioning System; Magnetometers; Position measurement; Sensor fusion; Solid state circuits; State feedback; Testing;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.2004.1310010