期刊文献+

一种基于自适应滤波的GPS滚转角估计方法 被引量:4

A roll angle estimation method using GPS based on adaptive filter
下载PDF
导出
摘要 全球定位系统(GPS)测姿技术主要是利用GPS载波相位和信号功率2种方法,但是测量信息单一且独立,针对旋转载体的测姿问题,提出一种基于自适应滤波的GPS滚转角估计方法,通过融合GPS接收机天线信号功率和多普勒频率信息测量载体滚转角和滚转角速度。利用当前统计模型对滚转角和滚转角速度测量进行系统建模,根据滚转角预测估计值选取量测量,并提出自适应滤波,采用滚转角加速度估计自适应滤波算法,实现了对系统噪声方差阵的自适应调整,避免了滚转角加速度最值的选取问题,降低了噪声的影响。通过仿真验证了基于自适应滤波的GPS滚转角估计方法的可行性,结果表明该方法的测量精度高于无迹卡尔曼滤波(UKF)。 The two main techniques for Global Positioning System(GPS) attitude measurement are to use GPS carrier phase and signal power, but the measurement information is single and independent. Aimed at the problem of attitude measurement of a spinning vehicle, a roll angle estimation method using GPS based on adaptive filter is proposed, which measures the roll angle and roll angular velocity by combining signal power and Doppler frequency information of GPS receiver antenna. The system model of the roll angle and roll angular velocity measurement is established by using the current statistical model, the measurements are selected according to the predicted estimation value of the roll angle, and an adaptive filter is proposed. The adaptive filter algorithm of roll angular acceleration estimation is used to realize the adaptive adjustment of the variance matrix of the system noise, which avoids the selection of the roll angle acceleration maximum value and reduces the effect of noise. The feasibility of the roll angle estimation method using GPS based on adaptive filter is verified by simulation, and the results show that the measurement accuracy of the method is higher than that of Unscented Kalman Filter(UKF).
作者 刘阳 李怀建 杜小菁 LIU Yang;LI Huaijian;DU Xiaojing(School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China)
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2020年第6期1177-1183,共7页 Journal of Beijing University of Aeronautics and Astronautics
关键词 全球定位系统(GPS) 当前统计模型 无迹卡尔曼滤波(UKF) 自适应滤波 姿态测量 Global Positioning System(GPS) current statistical model Unscented Kalman Filter(UKF) adaptive filter attitude measurement
  • 相关文献

参考文献10

二级参考文献72

  • 1孙东,周凤岐,周军.基于载波相位差分GPS的多航天器编队飞行相对导航[J].弹箭与制导学报,2003,23(S3):364-367. 被引量:4
  • 2范胜林,胡国辉,林雪原,袁信.GPS定位定向系统的研制[J].仪器仪表学报,2004,25(6):820-824. 被引量:15
  • 3范小军,刘锋,秦勇,张军.基于STF的“当前”统计模型及自适应跟踪算法[J].电子学报,2006,34(6):981-984. 被引量:45
  • 4王军政,沈伟,赵江波.机动目标跟踪中机动频率的自适应调整[J].北京理工大学学报,2007,27(1):38-41. 被引量:12
  • 5熊伟,伍岳,孙振冰,王泽民.多频数据组合在周跳探测和修复上的应用[J].武汉大学学报(信息科学版),2007,32(4):319-322. 被引量:39
  • 6Wang Kang, Liu Li, Du Xiaojing, Xie Peng. GPS/SINS Integrated Navigation System Hardware-in-the-Loop Simulation with GPS Receiver [C]// AIAA Modeling and Simulation Technologies Conference and Exhibit 20-23 August 2007, Hilton Head, South Carolina, USA. USA: AIAA, 2007.
  • 7SPIRENT Communications. SimGEN Software User Manual [K]. May 2004. England, 2005.
  • 8Dewayne R Brown, Derrek B. Dunn. Trajectory Visualization by Using Global Positioning Systems (GPS) [C]// IEEE, 2005. USA: IEEE, 2005.
  • 9Lee H, Kwangjin K, Heeyoung P, et al. Roll estimation of a smart munition using a magnetometer based on an unscented Kalman filter[C]// Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit. Honolulu, Hawaii, 2008: 1-13.
  • 10Kutlu A, Haciyev C, Tekinalp O. Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data[C]// Proceedings of the 3rd International Conference on Recent Advances in Space Technologies. Istanbul, Turkey. 2007, Vol.l: 458-461.

共引文献39

同被引文献37

引证文献4

二级引证文献10

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部