DocumentCode
2839317
Title
A low-cost attitude estimation system for UAV application
Author
Du, Dacheng ; Liu, Li ; Du, Xiaojing
Author_Institution
Sch. of Aerosp. Eng., Beijing Inst. of Technol., Beijing, China
fYear
2010
fDate
26-28 May 2010
Firstpage
4489
Lastpage
4492
Abstract
In this paper, a low-cost attitude estimation system is introduced. The system is developed with MEMS sensors including rate gyros and accelerometers. Composition and principle of the system are described. The rigid body kinematics is modeled with quaternion, such that eliminates attitude estimation singularities. The real-time Kalman filter is designed. Experiments were conducted in both static and dynamic conditions. The experimental results demonstrate that the algorithm and hardware are feasible and suitable for the application where critical accuracy and real-time requirements are needed.
Keywords
Kalman filters; accelerometers; aerospace robotics; attitude control; gyroscopes; mobile robots; remotely operated vehicles; robot dynamics; robot kinematics; sensors; Kalman filter; MEMS sensors; accelerometers; dynamic condition; low-cost attitude estimation system; micromechanical systems; quaternion; rate gyros; rigid body kinematics; static condition; unmanned aerial vehicles; Accelerometers; Aerospace electronics; Aircraft navigation; Attitude control; Kinematics; Micromechanical devices; Quaternions; Sensor systems; Unmanned aerial vehicles; Vehicle dynamics; Attitude estimate; Kalman filter; MEMS sensors; Quaternion;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2010 Chinese
Conference_Location
Xuzhou
Print_ISBN
978-1-4244-5181-4
Electronic_ISBN
978-1-4244-5182-1
Type
conf
DOI
10.1109/CCDC.2010.5498326
Filename
5498326
Link To Document