A METHOD OF DETERMINING THE INITIAL ATTITUDE ANGLES FOR THE STRAPDOWN INERTIAL NAVIGATION SYSTEM IN GYROCOMPASS MODE ON THE MOTOR VEHICLES

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Authors

  • Vu Hai Ha (Corresponding Author) Institute of Military Technical Automation/Academy of Military Science and Technology

Keywords:

Alignment; SINS; IMU; Euler angles; Gyrocompass.

Abstract

For the strapdown inertial navigation system, determining the exact angle of the initial attitudes plays an extremely important role, directly affecting the later navigation process of the system. The paper deals with the initial alignment determination algorithm including true NORTH for the SINS on non-moving objects in gyrocompass mode. The algorithm is carried out in two stages: determining the preliminary initial posture and determining the correct initial posture based on the state vectors of the IMU inertial measurement unit. The results obtained proved the accuracy of the algorithm.

References

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Published

15-12-2020

How to Cite

Vũ Hải Hà. “A METHOD OF DETERMINING THE INITIAL ATTITUDE ANGLES FOR THE STRAPDOWN INERTIAL NAVIGATION SYSTEM IN GYROCOMPASS MODE ON THE MOTOR VEHICLES”. Journal of Military Science and Technology, no. csce4, Dec. 2020, pp. 72-79, https://ojs.jmst.info/index.php/jmst/article/view/326.