The Design of Strapdown Inertial AHRS Based on MEMS

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Abstract:

A method of low cost strapdown inertial Attitude and Heading Reference System based on MEMS is implemented in this paper. Based on the analysis of the modules, the proper selection of the core processor and the inertial devices, the hardware components of the system is presented; Using the gradient-descent algorithm which is based on quaternion, it can finish the calculation of the attitude; This AHRS can realize the real-time extraction, calculation and the output of the information.

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Periodical:

Advanced Materials Research (Volumes 756-759)

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518-522

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Online since:

September 2013

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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[1] Zh.L. Deng. Inertial technology. Harbin: Harbin Institute of Technology Press, (2006).

Google Scholar

[2] Y.B. Chen, B. Zhong. The principle of inertial navigation. Beijing: National Defence Industry Press, (1990).

Google Scholar

[3] Zh. Tian. The development and application of embedded system. Beijing: Beijing University of Aeronautics and Astronautics Press, (2004).

Google Scholar

[4] Honeywell Company. 3-Axis Digital Compass IC HMC5883L. Honeywell, March (2011).

Google Scholar

[5] Sebastian O.H. Madgwick. An efficient orientation filter for inertial and inertial/magnetic sensor arrays. April 30, (2010).

Google Scholar

[6] Y.Y. Qin. Inertial navigation. Beijing: Science Press, (2006).

Google Scholar