A low-cost attitude heading reference system by combination of GPS and magnetometers and MEMS inertial sensors for mobile applications

Yong Li, Andrew Dempster, Binghao Li, Jinling Wang, Chris Rizos

School of Surveying and Spatial Information Systems, University of New South Wales, Sydney, NSW 2052, Australia.

DOI:                 

Abstract

This paper describes a prototype system for attitude and heading determination. A L1-only GPS receiver is integrated with microelectromechanical gyroscopes, accelerometers and magnetometers. In contrast to a multi-antenna/multi-receiver GPS attitude determination system, this system uses a single antenna/single receiver configuration to derive standalone velocity and acceleration solutions from the GPS L1 carrier phase measurements. No reference station is needed to form differences of carrier phase measurements for the velocity and acceleration calculation. The GPSderived acceleration is further used in the attitude determination by combination with the three-dimension acceleration sensed by the accelerometers. The magnetometers sense the Earth’s magnetic field intensity, and can give the heading estimation regardless of the status of the host platform. To satisfy real-time applications, infinite impulse response differentiators instead of finite impulse response differentiators are used to derive the acceleration from GPS. The algorithms have been implemented and their efficiency demonstrated by experiments.

Keywords

Attitude determination, micro-electromechanical system, inertial units, GPS

Conflicts of Interest

The authors declare no conflicts of interest.

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