Inner Attitude Integration Algorithm Based on Fault Detection for Strapdown Inertial Attitude and Heading Reference System

被引:0
作者
Liu JianyeZhu YanhuaLai JizhouYu Yongjun Navigation Research CenterNanjing University of Aeronautics and AstronauticsNanjing China [210016 ]
机构
关键词
navigation; strapdown inertial attitude and heading reference system; inner attitude integration algorithm; internal damping; Kalman filter; residual chi-square test;
D O I
暂无
中图分类号
V448.2 [航天器制导与控制];
学科分类号
081105 ;
摘要
This article proposes a new inner attitude integration algorithm to improve attitude accuracy of the strapdown inertial attitude and heading reference system(SIAHRS),which,by means of a Kalman filter,integrates the calculated attitude from the accelerometers in inertial measuring unit(IMU),called damping attitudes,with those from the conventional IMU.As vehicle's acceleration could produce damping attitude errors,the horizontal outputs from accelerometers are firstly used to judge the vehicle's motion so as to determine whether the damping attitudes could be reasonably applied.This article also analyzes the limitation of this approach.Furthermore,it suggests a residual chi-square test to judge the validity of damping attitude measurement in real time,and accordingly puts forward proper information fusion strategy.Finally,the effectiveness of the proposed algorithm is proved through the experiments on a real system in dynamic and static states.
引用
收藏
页码:68 / 74
页数:7
相关论文
共 4 条
[1]  
Periodic Error Compensation for Quartz MEMS Gyroscope Drift of INS[J]. Xu Jianmao a, Zhang Haipeng b,c,*, Sun Junzhong c a College of Energy and Power Engineering, Huazhong University of Science and Technology, Wuhan 430074, China b School of Instrument Science and Opto-electronics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China c Mechanical and Electrical Equipment Research Institute, Qingdao Navy Submarine Academe, Qingdao 266071, China.Chinese Journal of
[2]   基于置信度加权的组合导航数据融合算法 [J].
徐田来 ;
崔平远 ;
崔祜涛 .
航空学报, 2007, (06) :1389-1394
[3]   基于神经网络的航天器GPS/INS组合定姿系统(英文) [J].
岳晓奎 ;
袁建平 .
Chinese Journal of Aeronautics, 2006, (03) :233-238
[4]   Formal Verification for Embedded System Designs [J].
Xi Chen ;
Harry Hsieh ;
Felice Balarin ;
Yosinori Watanabe .
Design Automation for Embedded Systems, 2003, 8 :139-153