Carrier angular motion isolation and modulation method of dual-axis rotation inertial navigation system

被引:0
|
作者
Zhu T. [1 ]
Wang L. [1 ]
Wang Y. [2 ]
Ren Y. [1 ]
Sun Y. [3 ]
机构
[1] Department of Aerospace Science and Technology, Space Engineering University, Beijing
[2] No. 63961 Unit of PLA, Beijing
[3] School of Instrumentation and Optoelectronic Engineering, Beihang University, Beijing
关键词
Angular motion isolation; Inertial measurement unit; Inertial navigation; Rotational modulation;
D O I
10.19650/j.cnki.cjsi.J2006910
中图分类号
学科分类号
摘要
In traditional dual-axis rotation inertial navigation system (DRINS), the inertial measurement unit (IMU) is rotated regularly to modulate the inertial device error based on the carrier coordinate system. However, irregular carrier angular motion of the carrier will affect the modulation effect. Aiming at this problem, the mathematical relationship among IMU sensitive data, carrier attitude and dual-axis rotation angles is analyzed. Then a method of carrier angular motion isolation based on dual-axis rotation mechanism is proposed. On this basis, aiming at the problems of difficulty in control, cumulative control error and measurement delay of angular rate of rotation axis existing in angular rate control method in carrier angular motion isolation, a dual-axis rotation isolation and modulation method based on angle control is proposed. The theoretical analysis and simulation result based on vehicle test data show that the proposed method can isolate the carrier angular motion effectively. Compared with traditional rotation modulation method, the modulation effect of the proposed method is significant, and the navigation position error could be reduced by more than 50% in most surface motion applications. © 2020, Science Press. All right reserved.
引用
收藏
页码:66 / 75
页数:9
相关论文
共 19 条
  • [1] WANG W D, WAN ZH Y., Initial alignment for miniaturized SINS, Journal of Electronic Measurement and Instrumentation, 33, 8, pp. 16-22, (2019)
  • [2] ISHIBASHI S, TSUKIOKA S, YOSHIDA H, Et al., Accuracy improvement of an inertial navigation system brought about by the rotational motion, Oceans 2007 Europe International Conference, pp. 1-5, (2007)
  • [3] XU C S, MIAO L J, ZHOU Z Q., A self-calibration method of inner lever arms for dual-axis rotation inertial navigation systems, Measurement Science and Technology, 30, 12, pp. 1-9, (2019)
  • [4] HU P D, XU P, CHEN B X, Et al., A self-calibration method for the installation errors of rotation axes based on the asynchronous rotation of rotational inertial navigation systems, IEEE Transactions on Industrial Electronics, 65, 4, pp. 3550-3558, (2018)
  • [5] ZHA F, CHANG L B, HE H Y., Comprehensive error compensation for dual-axis rotational inertial navigation system, IEEE Sensors Journal, 20, 7, pp. 3788-3802, (2020)
  • [6] LIU Z J, WANG L, LI K, Et al., Analysis and improvement of attitude output accuracy in tri-axis rotational inertial navigation system, IEEE Sensors Journal, 20, 11, pp. 6091-6100, (2020)
  • [7] FENG P D., On hybrid inertial navigation systems, Journal of Chinese Inertial Technology, 24, 3, pp. 281-284, (2016)
  • [8] LI K, GAO P Y., Research on self-calibration technique for hybrid inertial navigation system, Chinese Journal of Scientific Instrument, 40, 4, pp. 9-17, (2019)
  • [9] CHENG J H, MOU H J, SUN X Y, Et al., Dual-axis rotational modulation method based on SINS tetrahedron redundancy configuration, Systems Engineering and Electronics, 39, 8, pp. 1801-1807, (2017)
  • [10] YUAN B L., Research on rotating inertial navigation system with four-frequency differential laser gyroscope, (2007)