Author:
Wang Rong,Wu Jin,Li Chong,Qi Shengbo,Meng Xiangrui,Wang Xinning,Zhang Chengxi
Abstract
Purpose
The purpose of this paper is to propose a high-precision attitude solution to solve the attitude drift problem caused by the dispersion of low-cost micro-electro-mechanical system devices in strap-down inertial navigation attitude solution of micro-quadrotor.
Design/methodology/approach
In this study, a three-stage attitude estimation scheme that combines data preprocessing, gyro drifts prediction and enhanced unscented Kalman filtering (UKF) is proposed. By introducing a preprocessing model, the quaternion orientation is calculated as the composition of two algebraic quaternions, and the decoupling feature of the two quaternions makes the roll and pitch components independent of magnetic interference. A novel real-time based on differential value (DV) estimation algorithm is proposed for gyro drift. This novel solution prevents the impact of quartic characteristics and uses the iterative method to meet the requirement of real-time applications. A novel attitude determination algorithm, the pre-process DV-UKF algorithm, is proposed in combination with UKF based on the above solution and its characteristics.
Findings
Compared to UKF, both simulation and experimental results demonstrate that the pre-process DV-UKF algorithm has higher reliability in attitude determination. The dynamic errors in the three directions of the attitude are below 2.0°, the static errors are all less than 0.2° and the absolute attitude errors tailored by average are about 47.98% compared to the UKF.
Originality/value
This paper fulfils an identified need to achieve high-precision attitude estimation when using low-cost inertial devices in micro-quadrotor. The accuracy of the pre-process DV-UKF algorithm is superior to other products in the market.
Reference31 articles.
1. A new partial robust adaptive modified maximum likelihood estimator;Chemometrics Intell. Lab. Syst,2020
2. Attitude-Independent magnetometer-bias determination: a survey;The Journal of the Astronautical Sciences,2003
3. GSA-based optimal backstepping controller with a fuzzy compensator for robust control of an autonomous quadrotor UAV;Aircr. Eng. Aerosp. Technol,2015
4. Continuous-discrete extended Kalman filter on matrix lie groups using concentrated gaussian distributions;Journal of Mathematical Imaging and Vision,2015
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献