In-Orbit Magnetic Disturbance Estimation and Compensation Using UKF in Nano-Satellite Mission-Reference-Cited by-同舟云学术

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In-Orbit Magnetic Disturbance Estimation and Compensation Using UKF in Nano-Satellite Mission

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
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Author:

Inamori Takaya¹

Affiliation:

1. University of Tokyo

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-5905

Reference14 articles.

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

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2. Adaptive Tuning of the Unscented Kalman Filter for Satellite Attitude Estimation;Journal of Aerospace Engineering;2015-05

3. Investigation of Estimation Methods for Time-varying Residual Magnetic Moment;Procedia Engineering;2015

4. Multiple-Model Adaptive Estimation of Time-Varying Residual Magnetic Moment for Small Satellites;Advances in Aerospace Guidance, Navigation and Control;2015

5. Robust Kalman filtering for small satellite attitude estimation in the presence of measurement faults;European Journal of Control;2014-03

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