Temperature compensation method of laser gyroscope based on PSO-BP neural network

被引:0
|
作者
Zhang W. [1 ]
Wang T. [1 ]
Wang L. [1 ]
Tao T. [1 ]
机构
[1] Xi'an Aerospace Precision Mechatronics Institute, Xi'an
关键词
Bias stability; Bias temperature error model; Laser gyroscope; Neural network; Particle swarm optimization;
D O I
10.13695/j.cnki.12-1222/o3.2022.05.015
中图分类号
学科分类号
摘要
After the laser strapdown inertial navigation system(SINS) is powered on and started, the bias of the laser gyro will undergo a process of dynamic change to stability with the temperature change, which will affect the application accuracy of the SINS. Therefore, a temperature compensation method for laser gyro based on particle swarm optimization-back propagation (PSO-BP) neural network is proposed. PSO is used to find the optimal weights and thresholds of the neural network model. Temperature and temperature gradient are used as independent variables to establish a network of gyro zero-bias compensation model. Temperature test results within the working temperature range of the laser SINS show that compared with the traditional BP neural network algorithm, the training speed of the proposed PSO-BP neural network model is improved by 4 times. The model fitting accuracy is higher. The problem that the BP algorithm is easy to fall into the local optimal solution is avoided. After compensation by PSO-BP algorithm, the gyro bias stability is improved by 60%, which further verifies the validity of the model. © 2022, Editorial Department of Journal of Chinese Inertial Technology. All right reserved.
引用
收藏
页码:652 / 657
页数:5
相关论文
共 14 条
  • [1] Li Y, Fu L, Wang L, Et al., Laser gyro temperature error compensation method based on NARX neural network embedded into extended Kalman filter, International Conference on Guidance, Navigation and Control, ICGNC 2020, pp. 3309-3320, (2020)
  • [2] Liang H, He J, Chen S, Et al., Temperature compensation method of the laser gyro inertial navigation based on heterogeneous kernel functions relevance vector machine, China Measurement & Test, 3, 25, pp. 1-8, (2022)
  • [3] Weng J, Bian X, Kou K, Et al., Optimization of ring laser gyroscope bias compensation algorithm in variable temperature environment, Sensors (Switzerland), 20, 2, (2020)
  • [4] Yang H., Effect of Temperature Error on the Temperature Compensation Accuracy of RLG's Bias, Optics & Optoelectronic Technology, 12, pp. 98-100, (2014)
  • [5] Zhuo C, He J, Hao R, Et al., Temperature experiment and compensation algorithm design for fiber gyros in rapid startup inertial navigation system, 7th International Conference on Electrical Engineering, Control and Robotics, 1887, 1, (2021)
  • [6] Qu D, Lu Y, Tao Y, Et al., Study of laser gyro temperature compensation technique on LINS, 2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS), pp. 1-6, (2019)
  • [7] Seo Y B, Yu H, Yu M, Et al., Compensation method of gyroscope bias hysteresis error with temperature and rate of temperature using deep neural networks, 2018 18th International Conference on Control, Automation and Systems (ICCAS), pp. 1072-1076, (2018)
  • [8] Xu X, Lai J, Lv P, Et al., Autonomous navigation method based on model parameters identification of TVSMM, Journal of Chinese Inertial Technology, 29, pp. 428-436, (2021)
  • [9] Wu J, Huang T, Zhu Z, Et al., Cold starting temperature time-related compensation model of inertial sensors based on particle swarm optimization algorithm, Review of Scientific Instruments, 92, 6, (2021)
  • [10] Tong L, Qin F, Feng K, Et al., Segmentation compensation method for FOG temperature error based on particle swarm optimization algorithm, Journal of Chinese Inertial Technology, 27, pp. 505-509, (2019)