This paper describes a robust and simple algorithm for an attitude and heading reference system (AHRS) based on low-cost MEMS inertial and magnetic sensors. The proposed approach relies on a gain-scheduled complementary filter, augmented by an acceleration-based switching architecture to yield robust performance, even when the vehicle is subject to strong accelerations. Experimental results are provided for a road captive test during which the vehicle dynamics are in high-acceleration mode and the performance of the proposed filter is evaluated against the output from a conventional linear complementary filter.
Kang, CW; Park, CG. Attitude estimation with accelerometers and gyros using fuzzy tuned Kalman filter. Proceedings of the European Control Conference, Budapest, Hungary, 23–26 August 2009; pp. 3713–3718.
[3]
Li, Y; Mahmoud, E; Anthony, C. Andrew,G.D. Performance evaluation of AHRS Kalman filter for MojoRTK system. Proceedings of International Global Navigation Satellite Systems Society IGNSS Symposium, Queensland, Australia, 1–3 December 2009.
[4]
Wang, M; Yang, Y; Ronald, RH; Zhang, Y. Adaptive filter for a miniature MEMS based attitude and heading reference system. Proceedings of IEEE Position Location and Navigation Symposium, Monterey, CA, USA, 26–29 April 2004; pp. 193–200.
[5]
Demoz, GE. A low-cost GPS/inertial Attitude Heading Reference System (AHRS) for general aviation applications. Proceedings of Position Location and Navigation Symposium, Palm Springs, CA, USA, 20–23 April 1998; pp. 518–525.
[6]
Euston, M; Coote, P; Mahony, R; Kim, J; Hamel, T. A complementary filter for attitude estimation of a fixed-wing UAV. Proceedings of IEEE/RSJ International Conference on Intelligent Robots and Systems, 22–26 September 2008; Acropolis Convention Center: Nice, France; pp. 340–345.
John, LC; Yang, C. Nonlinear attitude filtering methods. J. Guid. Contr. Dynam 2007, 30, 12–28, doi:10.2514/1.22452.
[9]
Baerveldt, AJ; Klang, R. A low-cost and low-weight attitude estimation system for an autonomous helicopter. Proceedings of IEEE International Conference on Intelligent Engineering Systems, Budapest, Hungary, 15–17 September 1997; pp. 391–395.
[10]
Hong, SK. Fuzzy logic based closed-loop strapdown attitude system for unmanned aerial vehicle (UAV). Sens. Actuat. A Phys 2003, 107, 109–118, doi:10.1016/S0924-4247(03)00353-4.
[11]
Hong, SK. Compensation of nonlinear thermal bias drift of Resonant Rate Sensor (RRS) using fuzzy logic. Sens. Actuat. A Phys 1999, 78, 143–148, doi:10.1016/S0924-4247(99)00241-1.
[12]
Hong, SK. Minimal-drift heading measurement using a MEMS gyro for indoor mobile robots. Sensors 2008, 8, 7287–7299, doi:10.3390/s8117287.
[13]
Tri-Axis Inertial sensor with Magnetometer, ADIS16405;; Analog Devices: Norwood, MA, USA, 2009.