参考文献/References:
[1] 高宗余,李德胜. 多MEMS传感器姿态测量系统的研究[J]. 电光与控制,2010,17(3):68-70.
Gao Zongyu,Li Deshengd. Attitude measurement system based on multiple MEMS sensors[J]. Electronics Optics and Control,2010,17(3):68-70.(in Chinese)
[2]Lu Junjie,Zhou Jun,Lu Xiaodong,et al. The measurement correction of MEMS gyroscope based interlaced Kalman filter[J]. Advanced Materials Research,2011,301/303:1 083-1 088.
[3]朱荣,周兆英. 基于MEMS的姿态测量系统[J]. 测控技术,2002,21(10):6-13.
Zhu Rong,Zhou Zhaoying. A MEMS-based attitude reference system[J]. Measurement and Control Technology,2002,21(10):6-13.(in Chinese)
[4]David H Titterton,John L Weston. Strapdown Inertial Navigation Technology[M]. London,United Kingdom:Peter Peregrinus Ltd on behalf of the Institute of Electrical Engineers,2004:280-360.
[5]赵祚喜,罗锡文,李庆,等. 基于MEMS惯性传感器融合的水田激光平地机水平控制系统[J]. 农业工程学报,2008,24(6):119-124.
Zhao Zuoxi,Luo Xiwen,Li Qing,et al. Leveling control system of laser-controlled land leveler for paddy field based on MEMS inertial sensor fusion[J]. Transactions of the CSAE,2008,24(6):119-124.(in Chinese)
[6]李仁,曾庆双,陈希军. 一种低成本MEMS惯性传感器应用技术研究[J]. 传感技术学报,2009,22(11):1 670-1 673.
Li Ren,Zeng Qingshuang,Chen Xijun. Research on application technology of low cost MEMS INS sensor[J]. Chinese Journal of Sensors and Actuators,2009,22(11):1 670-1 673.(in Chinese)
[7]李雪莲,孙尧,莫宏伟. 微惯性传感器零点漂移融合滤波算法研究[J]. 传感器与微系统,2009,28(6):50-53.
Li Xuelian,Sun Yao,Mo Hongwei. Research on null drift fusion algorithm of micro inertial sensors[J]. Transducer and Microsystem Technologies,2009,28(6):50-53.(in Chinese)
[8]张谦,裴海龙,罗沛. 基于MEMS器件的姿态航向参考系统设计及应用[J]. 计算机工程与设计,2007,28(3):631-634.
Zhang Qian,Pei Hailong,Luo Pei. Design and implementation of AHRS based on MEMS units[J]. Computer Engineering and Design,2007,28(3):631-634.(in Chinese)
[9]陈永冰,钟斌. 惯性导航原理[M]. 北京:国防工业出版社,2007:13-232.
Chen Yongbing,Zhong Bin. Principles of Inertial Navigation[M]. Beijing:National Defence of Industrial Press,2007:13-232.(in Chinese)
[10]孙冬梅,田增山,韩令军. 捷联惯导系统中四元素法求解姿态角仿真模拟[J]. 弹箭与制导学报,2009,29(1):51-60.
Sun Dongmei,Tian Zengshan,Han Lingjun. Simulation on quaternion calculate attitude angle of the strapdown inertial navigation system[J]. Journal of Projectiles,Rockets,Missiles and Guidance,2009,29(1):51-60.(in Chinese)
[11]朱启举,秦永元,梅春波,等. 基于MEMS惯性器件的水平姿态解算方案设计[J]. 弹箭与制导学报,2013,33(5):35-40.
Zhu Qiji,Qin Yongyuqn,Mei Chunbo,et al. Horizontal attitude estimation using MEMS-based inertial sensors[J]. Journal of Projectiles,Rockets,Missiles and Guidance,2013,33(5):35-40.(in Chinese)
[12]屈重君,雷宝权,陈璞,等. 无位置输入的民机姿态航向误差修正算法[J]. 传感技术学报,2008,21(11):1 862-1 866.
Qu Zhongjun,Lei Baoquan,Chen Pu,et al. Error correction algorithm of attitude and heading for civil airplane without position inputs[J]. Chinese Journal of Sensors and Actuators,2008,21(11):1 862-1 866.(in Chinese)
[13]Analog Devices,Inc. ADIS16300 Datasheet[DB/OL].(2009-04)[2010-01-28]. http://www. analog. com/static/imported-files/d ata_sheets/ADIS16300.pdf.
[14]ARM Limited. CortexTM-M3 Technical reference manual[EB/OL].(2008-06)[2014-04-28]. http://wwww.arm.com.
[15]Jay A. Farrell. Aided Navigation:GPS with High Rate Sensors[M]. New York:Mc Graw Hill,2006:35-60.
[16]Crossbow Technology,Inc. AHRS500GA-Series User’s Manual:Revision B[M/OL]. [2014-07-30]. http://www.moog-crossbow.com.