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2022 | OriginalPaper | Chapter

5. Spacecraft Attitude Determination

Authors : Yongchun Xie, Yongjun Lei, Jianxin Guo, Bin Meng

Published in: Spacecraft Dynamics and Control

Publisher: Springer Singapore

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Abstract

The main task in the attitude determination of a spacecraft is to accurately estimate the spacecraft’s attitude and angular velocity by gathering data with attitude sensors.

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previous chapter Spacecraft Attitude Kinematics and Dynamics
next chapter Spacecraft Attitude Control
Literature
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Lv Z, Lei Y (2013) Satellite attitude measurement and determination. National Defense Industry Press, Beijing
2.
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Xiong K, Tang L, Lei Y (2011) Multiple model Kalman filter for attitude determination of precision pointing spacecraft. Acta Astronaut 68:843–852
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Lei Y (2017) Relative alignment error calibration method for star sensors of spacecraft in orbit. Aerosp Control Appl 43(6):1–7
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Liu Y, Chen Y (2003) Star-sensor measurement model and its application to the spacecraft attitude determination system. J Astronaut 24(2):163–167
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Pittelkau ME (2017) Survey of calibration algorithms for spacecraft attitude sensors and gyros. AAS 07–295
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Lei Y, Tian K, Zong H et al (2014) A post-event attitude determination method based on calibration of low-frequency errors of star sensor. In: Proceedings of the 2014 Symposium on inertial technology by the professional group on inertial of the sciences and technology committee of the china aerospace science and technology corporation. Beijing
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Tian K, Zong H, Lei Y (2014) A calibration method for low-frequency errors of star sensor based on gyro constant drift estimation. In: Proceedings of the 16th national conference on space and moving body control technology, pp 162–166
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Lei Y, Li M (2018) Spinning angle velocity determination for in-orbit satellites with attitude anomaly. Aerosp Control Appl 44(1): 15–20
Metadata
Title
Spacecraft Attitude Determination
Authors
Yongchun Xie
Yongjun Lei
Jianxin Guo
Bin Meng
Copyright Year
2022
Publisher
Springer Singapore
Book
Spacecraft Dynamics and Control

Print ISBN: 978-981-336-447-9

Electronic ISBN: 978-981-336-448-6

Copyright Year: 2022

DOI
https://doi.org/10.1007/978-981-33-6448-6_5

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