[3] WANG M, YANG Y C, HATCH R R, et al.Adaptive filter for a miniature MEMS based attitude and heading refe-rence system[C]//Position Location and Navigation Symposium, 2004:193-200.
[5] CASTELLANOS J F G, LESECQ S, MARCHAND N, et al.A low cost air data attitude heading reference system for the tourism airplane applications[C]//Sensor, IEEE,2005.doi:10.1109/ICSENS.2005.1597968.
[6] ZHANG R H, JIA H G, CHEN T, et al.Attitude solution enginccring for strapdown inertial navigation system based on quaternion algorithm[J].Optics Precision Engineering, 2008, 16(10):1963-1970.
[7] ANGRISANO A.GNSS/INS Integration methods[D].Calgary:University of Calgary, 2010.
[8] GUERRERO-CASTELIANOS J F, MADRIGAL-SASTRE H, DURAND S, et al.Design and implementation of an attitude and heading reference system[C]//The 8th International Conference on Electrical Engineering, Computing Science and Automatic Control, Program and Abstract Book, 2011:1-5.
[11] DENTI E, GALATOLO R, SCHETTINI F.An AHRS based on a Kalman filter for the integration of intertial, magnet-ometric an GPS data[C]//The 27th Internation Congress of the Aeronautical Sciences, 2010:1-9.