DocumentCode :
593029
Title :
Attitude and Heading Reference System for Quadrotor Based on MEMS Sensors
Author :
Qiang Jiang ; Yong Zeng ; Qiang Liu ; Hua Jing
Author_Institution :
Sch. of Aeronaut. & Astronaut., UESTC, Chengdu, China
fYear :
2012
fDate :
8-10 Dec. 2012
Firstpage :
1090
Lastpage :
1093
Abstract :
This paper deals with designing and implementation of Attitude and Heading Reference System (AHRS) which based on data fusion of multi-sensor. And it presents an approach of designing a low cost AHRS which used Micro Electronic Mechanical System (MEMS). In our approach, AHRS is made up of a 3-axes MEMS accelerometers, a 3-axes MEMS rate-gyros, an electronic compass and a FPGA which is used as the signal processor. Furthermore, a rotation quaternion and a Kalman Filter were the options as multi-sensor data fusion and integration. Finally, an experiment was introduced to analyze the attitude data carried on quadrotor. The simulation test shows when the carrier is in dynamic environment, the attitudes error are within 2°. The results show that the designed AHRS provided stabilized attitude and heading angles in dynamic conditions which improved the quadrotor´s attitude and heading control.
Keywords :
Kalman filters; accelerometers; aircraft instrumentation; aircraft navigation; attitude control; compasses; field programmable gate arrays; gyroscopes; inertial navigation; microsensors; position control; sensor fusion; FPGA; Kalman filter; MEMS accelerometers; MEMS rate-gyros; MEMS sensor; attitude control; attitude reference system; electronic compass; heading control; heading reference system; microelectronicmechanical system; multisensor data fusion; quadrotor; rotation quaternion; signal processor; Attitude control; Data integration; Equations; Kalman filters; Micromechanical devices; Quaternions; Sensors; AHRS; Kalman; quadrotor; quaternion;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2012 Second International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4673-5034-1
Type :
conf
DOI :
10.1109/IMCCC.2012.257
Filename :
6429093
Link To Document :
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