Xing Li, Hang Yijun, Xiong Zhi, Liu Jianye, Wan Zhong
College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211100, China.
Sensors (Basel). 2016 Oct 16;16(10):1716. doi: 10.3390/s16101716.
This paper describes a disturbance acceleration adaptive estimate and correction approach for an attitude reference system (ARS) so as to improve the attitude estimate precision under vehicle movement conditions. The proposed approach depends on a Kalman filter, where the attitude error, the gyroscope zero offset error and the disturbance acceleration error are estimated. By switching the filter decay coefficient of the disturbance acceleration model in different acceleration modes, the disturbance acceleration is adaptively estimated and corrected, and then the attitude estimate precision is improved. The filter was tested in three different disturbance acceleration modes (non-acceleration, vibration-acceleration and sustained-acceleration mode, respectively) by digital simulation. Moreover, the proposed approach was tested in a kinematic vehicle experiment as well. Using the designed simulations and kinematic vehicle experiments, it has been shown that the disturbance acceleration of each mode can be accurately estimated and corrected. Moreover, compared with the complementary filter, the experimental results have explicitly demonstrated the proposed approach further improves the attitude estimate precision under vehicle movement conditions.
本文描述了一种用于姿态参考系统(ARS)的干扰加速度自适应估计与校正方法,以提高车辆运动条件下的姿态估计精度。所提出的方法依赖于卡尔曼滤波器,在该滤波器中估计姿态误差、陀螺仪零偏误差和干扰加速度误差。通过在不同加速度模式下切换干扰加速度模型的滤波器衰减系数,对干扰加速度进行自适应估计和校正,进而提高姿态估计精度。通过数字仿真在三种不同的干扰加速度模式(分别为非加速度、振动加速度和持续加速度模式)下对该滤波器进行了测试。此外,所提出的方法也在车辆运动实验中进行了测试。通过所设计的仿真和车辆运动实验表明,每种模式下的干扰加速度都能够被准确估计和校正。而且,与互补滤波器相比,实验结果明确表明所提出的方法在车辆运动条件下进一步提高了姿态估计精度。