Abstract
An information combination of star sensor-based angle measurement and inertial devices is used to improve the accuracy of the autonomous navigation system. The missile-borne environment has high dynamic movement characteristics, and the attitude change will bring the star sensor image movement which affects the angular accuracy of the star sensor, thereby reducing navigation accuracy. This paper studies the effect of the attitude of the carrier on the angular measurement of the star sensor, and proposes the accuracy compensation method based on the angular acceleration measurement, thereby improving the angular accuracy of highly dynamics missile-borne star sensors.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Xing, F., You, Z.: Principle and Implementation of APS CMOS Star Tracker, 1st edn. National Defense Industry Press, Beijing (2017)
Wang, H., Luo, C.: Analysis of dynamic angle measurement of missile borne star sensor. Mod. Defence Technol. 38(1), 37–41 (2010)
Guo, H., Deng, N.: Effect of dynamic factor on measuring star by star sensor. Aerosp. Control 26(6), 38–41 (2008)
Li, X., Zhao, H.: Analysis of star image centroid accuracy of an APS star sensor in rotation. Aerosp. Control Appl. 35(4), 11–16 (2009)
Zhao, S., Wang, Y.: Compensation method of dynamic angle measurement for missile-borne star sensor. Mod. Defence Technol. 38(5), 41–44 (2010)
Gong, D., Wu, Y.: An attempt at improving dynamic performance of star tracker by motion compensation. Aerosp. Control Appl. 35(6), 19–23 (2009)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2022 The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Wu, B., Guo, Z., Ji, D., Chen, F., Liu, Q. (2022). Compensation Method of Dynamic Angle Measurement for Missile-Borne Star Sensor. In: Yan, L., Duan, H., Yu, X. (eds) Advances in Guidance, Navigation and Control . Lecture Notes in Electrical Engineering, vol 644. Springer, Singapore. https://doi.org/10.1007/978-981-15-8155-7_362
Download citation
DOI: https://doi.org/10.1007/978-981-15-8155-7_362
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-15-8154-0
Online ISBN: 978-981-15-8155-7
eBook Packages: Intelligent Technologies and RoboticsIntelligent Technologies and Robotics (R0)