摘要
针对陀螺稳定平台的漂移问题,建立了陀螺稳定跟踪装置在不同工作模式下陀螺漂移的数学模型,指出稳定模式下包含常值漂移和相关漂移的陀螺低频噪声是影响稳定精度的主要原因。提出一种自适应实时估计算法,采用卡尔曼滤波框架和滤波器收敛判据,结合Sage-Husa滤波和加权Sage-Husa滤波算法,利用跟踪器跟踪静止目标时输出的脱靶量信号对陀螺常值漂移和相关漂移进行估计。实验结果表明:该算法能够在系统模型和噪声特性均不准确的情况下使用,收敛时间小于3s,估计均方差小于0.02(°)/s,具有良好的鲁棒性和自适应能力。
An adaptive real-time estimate algorithm is proposed to address the problem of gyro-stabilized platform drift. First, the major work mode of the gyro-stabilized and tracking equipment is analyzed. Then, a gyro drift model under the stabilization mode and the track mode is established, which indicates that the gyro low frequency noise composed of the con- stant bias and related bias is the main cause of stabilization error. The algorithm adopts the Kalman filter framework and em- ploys filter convergence criterion combining Sage-Husa filter and weighted Sage-Husa filter to estimate the constant and re- lated drifts of gyros. Experiment results show that the convergence time is less than 3 s and the estimation standard deviation is less than 0.02 （°）/s under the condition of non-exact system model and noise characteristics, which demonstrates the ro- bustness and adaptive ability of the algorithm.
出处
《航空学报》
EI
CAS
CSCD
北大核心
2012年第6期1044-1051,共8页
Acta Aeronautica et Astronautica Sinica
基金
国家自然科学基金(50805144)
湖南省自然科学基金(09JJ4029)~~
